##### Element Performance Inspection (EPI) Data Collection Tool

**1.1.1 Aircraft Airworthiness (AW)**

# 

# ELEMENT SUMMARY INFORMATION

**Purpose of this Element** (certificate holder's responsibility):

+-----------------------------------------------------------------------+
| -   To ensure each aircraft released to service is in airworthy       |
|     condition and meets the applicable airworthiness requirements of  |
|     14 CFR, including those related to identification and equipment.  |
+-----------------------------------------------------------------------+

**Objective** (FAA oversight):

+-----------------------------------------------------------------------+
| -   To determine the effectiveness of the certificate holder\'s       |
|     procedures in meeting the desired output of the process.          |
|                                                                       |
| -   To determine if the certificate holder follows its procedures,    |
|     controls, process measurements, and interfaces for the Aircraft   |
|     Airworthiness process.                                            |
|                                                                       |
| -   To determine if there were any changes in the personnel           |
|     identified by the certificate holder as having responsibility     |
|     and/or authority for the Aircraft Airworthiness process.          |
+-----------------------------------------------------------------------+

**Specific Instructions**:

+-----------------------------------------------------------------------+
| -   To accomplish this EPI, the inspector must inspect the            |
|     certificate holder\'s aircraft, powerplants, and appliances       |
|     during in-service operation. Further, the inspector will observe  |
|     overhaul, \"heavy maintenance,\" intermediate level maintenance,  |
|     periodic service and maintenance, preventive maintenance, and     |
|     repair/alteration activities. The purpose of the inspection and   |
|     observation is to determine the airworthiness condition (visual   |
|     inspection, safe for flight) and airworthiness status include     |
|     installed powerplants, and appliances at various maintenance and  |
|     operational locations, to discern the airworthiness condition and |
|     status of the certificate holder\'s aircraft.                     |
+-----------------------------------------------------------------------+

**Related EPIs**:

+-----------------------------------------------------------------------+
| -   1.1.2 Appropriate Operational Equipment (AW)                      |
|                                                                       |
| -   1.3.3 Maintenance Facility / Main Maintenance Base (AW)           |
|                                                                       |
| -   1.3.19 Lower Landing Minimums (LLM) (AW)                          |
|                                                                       |
| -   1.3.25 Cargo Handling Equipment, Systems and Appliances (AW)      |
|                                                                       |
| -   5.1.1 Line Stations (AW)                                          |
+-----------------------------------------------------------------------+

# 

# SUPPLEMENTAL INFORMATION

**Specific Regulatory Requirements (SRRs)**:

+-----------------------------------------------------------------------+
| -   SRRs:                                                             |
+=======================================================================+
| > 119.43(b)                                                           |
| >                                                                     |
| > 119.43(b)(1)                                                        |
| >                                                                     |
| > 119.43(b)(2)                                                        |
| >                                                                     |
| > 119.43(c)                                                           |
| >                                                                     |
| > 119.9(b)                                                            |
| >                                                                     |
| > 121.135(a)(1)                                                       |
| >                                                                     |
| > 121.135(b)(1)                                                       |
| >                                                                     |
| > 121.135(b)(16)                                                      |
| >                                                                     |
| > 121.135(b)(2)                                                       |
| >                                                                     |
| > 121.135(b)(3)                                                       |
| >                                                                     |
| > 121.137(a)                                                          |
| >                                                                     |
| > 121.141(a)                                                          |
| >                                                                     |
| > 121.141(b)                                                          |
| >                                                                     |
| > 121.141(b)(1)                                                       |
| >                                                                     |
| > 121.141(b)(2)                                                       |
| >                                                                     |
| > 121.153(a)(1)                                                       |
| >                                                                     |
| > 121.153(a)(2)                                                       |
| >                                                                     |
| > 121.211(b)                                                          |
| >                                                                     |
| > 121.215                                                             |
| >                                                                     |
| > 121.217                                                             |
| >                                                                     |
| > 121.219                                                             |
| >                                                                     |
| > 121.221(f)(5)                                                       |
| >                                                                     |
| > 121.239                                                             |
| >                                                                     |
| > 121.239(a)(1)                                                       |
| >                                                                     |
| > 121.239(a)(2)                                                       |
| >                                                                     |
| > 121.239(a)(3)                                                       |
| >                                                                     |
| > 121.239(b)                                                          |
| >                                                                     |
| > 121.241                                                             |
| >                                                                     |
| > 121.243                                                             |
| >                                                                     |
| > 121.245                                                             |
| >                                                                     |
| > 121.247                                                             |
| >                                                                     |
| > 121.249                                                             |
| >                                                                     |
| > 121.251                                                             |
| >                                                                     |
| > 121.253(a)                                                          |
| >                                                                     |
| > 121.253(b)                                                          |
| >                                                                     |
| > 121.255                                                             |
| >                                                                     |
| > 121.257                                                             |
| >                                                                     |
| > 121.259                                                             |
| >                                                                     |
| > 121.261                                                             |
| >                                                                     |
| > 121.263                                                             |
| >                                                                     |
| > 121.265                                                             |
| >                                                                     |
| > 121.267                                                             |
| >                                                                     |
| > 121.269                                                             |
| >                                                                     |
| > 121.271(a)                                                          |
| >                                                                     |
| > 121.271(b)                                                          |
| >                                                                     |
| > 121.273                                                             |
| >                                                                     |
| > 121.275                                                             |
| >                                                                     |
| > 121.277(a)                                                          |
| >                                                                     |
| > 121.277(b)                                                          |
| >                                                                     |
| > 121.279(b)                                                          |
| >                                                                     |
| > 121.281                                                             |
| >                                                                     |
| > 121.283                                                             |
| >                                                                     |
| > 121.285                                                             |
| >                                                                     |
| > 121.285(b)(1)                                                       |
| >                                                                     |
| > 121.285(b)(2)                                                       |
| >                                                                     |
| > 121.285(b)(3)                                                       |
| >                                                                     |
| > 121.285(b)(4)                                                       |
| >                                                                     |
| > 121.285(b)(5)                                                       |
| >                                                                     |
| > 121.285(b)(6)                                                       |
| >                                                                     |
| > 121.285(b)(7)                                                       |
| >                                                                     |
| > 121.285(b)(8)                                                       |
| >                                                                     |
| > 121.285(c)                                                          |
| >                                                                     |
| > 121.289(a)(1)                                                       |
| >                                                                     |
| > 121.289(a)(2)                                                       |
| >                                                                     |
| > 121.293                                                             |
| >                                                                     |
| > 121.303(b)                                                          |
| >                                                                     |
| > 121.303(c)                                                          |
| >                                                                     |
| > 121.305(b)                                                          |
| >                                                                     |
| > 121.305(c)                                                          |
| >                                                                     |
| > 121.305(d)                                                          |
| >                                                                     |
| > 121.305(e)                                                          |
| >                                                                     |
| > 121.305(f)                                                          |
| >                                                                     |
| > 121.305(g)                                                          |
| >                                                                     |
| > 121.305(h)                                                          |
| >                                                                     |
| > 121.305(i)                                                          |
| >                                                                     |
| > 121.305(j)                                                          |
| >                                                                     |
| > 121.305(j)(1)                                                       |
| >                                                                     |
| > 121.305(j)(2)                                                       |
| >                                                                     |
| > 121.305(j)(3)                                                       |
| >                                                                     |
| > 121.305(j)(4)                                                       |
| >                                                                     |
| > 121.306(c)                                                          |
| >                                                                     |
| > 121.307(a)                                                          |
| >                                                                     |
| > 121.307(b)                                                          |
| >                                                                     |
| > 121.307(c)                                                          |
| >                                                                     |
| > 121.307(d)                                                          |
| >                                                                     |
| > 121.307(e)                                                          |
| >                                                                     |
| > 121.307(f)                                                          |
| >                                                                     |
| > 121.307(g)                                                          |
| >                                                                     |
| > 121.307(h)                                                          |
| >                                                                     |
| > 121.307(i)                                                          |
| >                                                                     |
| > 121.307(j)                                                          |
| >                                                                     |
| > 121.307(k)                                                          |
| >                                                                     |
| > 121.307(l)(1)                                                       |
| >                                                                     |
| > 121.308(a)                                                          |
| >                                                                     |
| > 121.308(b)                                                          |
| >                                                                     |
| > 121.308(d)                                                          |
| >                                                                     |
| > 121.309(b)(1)                                                       |
| >                                                                     |
| > 121.309(b)(2)                                                       |
| >                                                                     |
| > 121.309(b)(3)                                                       |
| >                                                                     |
| > 121.309(b)(4)                                                       |
| >                                                                     |
| > 121.309(c)(1)                                                       |
| >                                                                     |
| > 121.309(c)(2)                                                       |
| >                                                                     |
| > 121.309(c)(3)                                                       |
| >                                                                     |
| > 121.309(c)(4)                                                       |
| >                                                                     |
| > 121.309(c)(5)                                                       |
| >                                                                     |
| > 121.309(c)(5)(i)                                                    |
| >                                                                     |
| > 121.309(c)(5)(ii)                                                   |
| >                                                                     |
| > 121.309(c)(5)(iii)                                                  |
| >                                                                     |
| > 121.309(c)(6)                                                       |
| >                                                                     |
| > 121.309(c)(7)                                                       |
| >                                                                     |
| > 121.309(e)                                                          |
| >                                                                     |
| > 121.309(f)(1)                                                       |
| >                                                                     |
| > 121.309(f)(2)                                                       |
| >                                                                     |
| > 121.310                                                             |
| >                                                                     |
| > 121.310(a)                                                          |
| >                                                                     |
| > 121.310(b)(1)                                                       |
| >                                                                     |
| > 121.310(b)(1)(i)                                                    |
| >                                                                     |
| > 121.310(b)(1)(ii)                                                   |
| >                                                                     |
| > 121.310(b)(1)(iii)                                                  |
| >                                                                     |
| > 121.310(b)(2)(i)                                                    |
| >                                                                     |
| > 121.310(b)(2)(ii)                                                   |
| >                                                                     |
| > 121.310(b)(2)(iii)                                                  |
| >                                                                     |
| > 121.310(c)                                                          |
| >                                                                     |
| > 121.310(c)(1)                                                       |
| >                                                                     |
| > 121.310(c)(2)                                                       |
| >                                                                     |
| > 121.310(c)(3)                                                       |
| >                                                                     |
| > 121.310(d)                                                          |
| >                                                                     |
| > 121.310(d)(1)(i)                                                    |
| >                                                                     |
| > 121.310(d)(1)(ii)                                                   |
| >                                                                     |
| > 121.310(d)(1)(iii)                                                  |
| >                                                                     |
| > 121.310(d)(3)                                                       |
| >                                                                     |
| > 121.310(d)(4)                                                       |
| >                                                                     |
| > 121.310(e)(1)                                                       |
| >                                                                     |
| > 121.310(e)(1)(i)                                                    |
| >                                                                     |
| > 121.310(e)(1)(ii)                                                   |
| >                                                                     |
| > 121.310(e)(2)                                                       |
| >                                                                     |
| > 121.310(f)                                                          |
| >                                                                     |
| > 121.310(f)(1)                                                       |
| >                                                                     |
| > 121.310(f)(2)                                                       |
| >                                                                     |
| > 121.310(f)(3)                                                       |
| >                                                                     |
| > 121.310(f)(3)(i)                                                    |
| >                                                                     |
| > 121.310(f)(3)(ii)                                                   |
| >                                                                     |
| > 121.310(f)(3)(iii)                                                  |
| >                                                                     |
| > 121.310(f)(4)                                                       |
| >                                                                     |
| > 121.310(f)(5)                                                       |
| >                                                                     |
| > 121.310(f)(6)                                                       |
| >                                                                     |
| > 121.310(f)(7)                                                       |
| >                                                                     |
| > 121.310(g)                                                          |
| >                                                                     |
| > 121.310(g)(1)                                                       |
| >                                                                     |
| > 121.310(g)(2)                                                       |
| >                                                                     |
| > 121.310(g)(3)                                                       |
| >                                                                     |
| > 121.310(h)(1)                                                       |
| >                                                                     |
| > 121.310(h)(1)(i)                                                    |
| >                                                                     |
| > 121.310(h)(1)(ii)                                                   |
| >                                                                     |
| > 121.310(h)(2)                                                       |
| >                                                                     |
| > 121.310(h)(2)(i)                                                    |
| >                                                                     |
| > 121.310(h)(2)(ii)                                                   |
| >                                                                     |
| > 121.310(i)                                                          |
| >                                                                     |
| > 121.310(j)                                                          |
| >                                                                     |
| > 121.310(k)                                                          |
| >                                                                     |
| > 121.310(k)(1)                                                       |
| >                                                                     |
| > 121.310(k)(2)                                                       |
| >                                                                     |
| > 121.310(n)                                                          |
| >                                                                     |
| > 121.311(a)(2)                                                       |
| >                                                                     |
| > 121.311(d)                                                          |
| >                                                                     |
| > 121.311(f)                                                          |
| >                                                                     |
| > 121.311(g)                                                          |
| >                                                                     |
| > 121.312(a)                                                          |
| >                                                                     |
| > 121.312(a)(1)(i)                                                    |
| >                                                                     |
| > 121.312(a)(1)(ii)                                                   |
| >                                                                     |
| > 121.312(a)(2)                                                       |
| >                                                                     |
| > 121.312(a)(2)(i)                                                    |
| >                                                                     |
| > 121.312(a)(2)(ii)                                                   |
| >                                                                     |
| > 121.312(a)(3)                                                       |
| >                                                                     |
| > 121.312(a)(3)(i)                                                    |
| >                                                                     |
| > 121.312(a)(3)(ii)                                                   |
| >                                                                     |
| > 121.312(a)(5)                                                       |
| >                                                                     |
| > 121.312(b)                                                          |
| >                                                                     |
| > 121.312(b)(1)                                                       |
| >                                                                     |
| > 121.312(c)                                                          |
| >                                                                     |
| > 121.312(d)                                                          |
| >                                                                     |
| > 121.312(e)                                                          |
| >                                                                     |
| > 121.312(e)(1)                                                       |
| >                                                                     |
| > 121.312(e)(1)(i)                                                    |
| >                                                                     |
| > 121.312(e)(1)(ii)                                                   |
| >                                                                     |
| > 121.312(e)(2)                                                       |
| >                                                                     |
| > 121.312(e)(3)                                                       |
| >                                                                     |
| > 121.313(a)                                                          |
| >                                                                     |
| > 121.313(b)                                                          |
| >                                                                     |
| > 121.313(c)                                                          |
| >                                                                     |
| > 121.313(d)                                                          |
| >                                                                     |
| > 121.313(e)                                                          |
| >                                                                     |
| > 121.313(f)                                                          |
| >                                                                     |
| > 121.313(g)                                                          |
| >                                                                     |
| > 121.313(h)                                                          |
| >                                                                     |
| > 121.313(i)                                                          |
| >                                                                     |
| > 121.313(j)(1)                                                       |
| >                                                                     |
| > 121.313(j)(2)                                                       |
| >                                                                     |
| > 121.314                                                             |
| >                                                                     |
| > 121.314(a)(1)                                                       |
| >                                                                     |
| > 121.314(a)(2)                                                       |
| >                                                                     |
| > 121.314(a)(3)                                                       |
| >                                                                     |
| > 121.314(c)                                                          |
| >                                                                     |
| > 121.315(a)                                                          |
| >                                                                     |
| > 121.315(c)                                                          |
| >                                                                     |
| > 121.316                                                             |
| >                                                                     |
| > 121.317(a)                                                          |
| >                                                                     |
| > 121.317(d)                                                          |
| >                                                                     |
| > 121.317(e)                                                          |
| >                                                                     |
| > 121.318(a)                                                          |
| >                                                                     |
| > 121.319                                                             |
| >                                                                     |
| > 121.323(a)                                                          |
| >                                                                     |
| > 121.323(b)                                                          |
| >                                                                     |
| > 121.323(c)                                                          |
| >                                                                     |
| > 121.323(d)                                                          |
| >                                                                     |
| > 121.323(e)                                                          |
| >                                                                     |
| > 121.325(a)                                                          |
| >                                                                     |
| > 121.325(b)                                                          |
| >                                                                     |
| > 121.325(c)                                                          |
| >                                                                     |
| > 121.327(c)(2)                                                       |
| >                                                                     |
| > 121.327(c)(3)                                                       |
| >                                                                     |
| > 121.329(a)                                                          |
| >                                                                     |
| > 121.329(a)(1)                                                       |
| >                                                                     |
| > 121.329(a)(2)                                                       |
| >                                                                     |
| > 121.329(a)(3)                                                       |
| >                                                                     |
| > 121.329(a)(4)                                                       |
| >                                                                     |
| > 121.331(a)                                                          |
| >                                                                     |
| > 121.331(b)                                                          |
| >                                                                     |
| > 121.331(c)(1)                                                       |
| >                                                                     |
| > 121.331(c)(2)(i)                                                    |
| >                                                                     |
| > 121.331(c)(2)(ii)                                                   |
| >                                                                     |
| > 121.331(c)(2)(iii)                                                  |
| >                                                                     |
| > 121.333(a)                                                          |
| >                                                                     |
| > 121.333(b)                                                          |
| >                                                                     |
| > 121.333(c)(1)                                                       |
| >                                                                     |
| > 121.333(d)                                                          |
| >                                                                     |
| > 121.333(e)                                                          |
| >                                                                     |
| > 121.335(a)                                                          |
| >                                                                     |
| > 121.335(b)                                                          |
| >                                                                     |
| > 121.337(a)                                                          |
| >                                                                     |
| > 121.337(b)                                                          |
| >                                                                     |
| > 121.337(b)(2)                                                       |
| >                                                                     |
| > 121.337(b)(9)(i)                                                    |
| >                                                                     |
| > 121.337(b)(9)(ii)                                                   |
| >                                                                     |
| > 121.337(b)(9)(iii)                                                  |
| >                                                                     |
| > 121.342                                                             |
| >                                                                     |
| > 121.343(a)(1)thru(6)                                                |
| >                                                                     |
| > 121.343(b)                                                          |
| >                                                                     |
| > 121.343(c)                                                          |
| >                                                                     |
| > 121.343(d)                                                          |
| >                                                                     |
| > 121.343(e)                                                          |
| >                                                                     |
| > 121.343(f)                                                          |
| >                                                                     |
| > 121.343(g)                                                          |
| >                                                                     |
| > 121.343(j)                                                          |
| >                                                                     |
| > 121.343(k)                                                          |
| >                                                                     |
| > 121.344(a)                                                          |
| >                                                                     |
| > 121.344(c)(1)                                                       |
| >                                                                     |
| > 121.344(c)(2)                                                       |
| >                                                                     |
| > 121.344(d)                                                          |
| >                                                                     |
| > 121.344(e)                                                          |
| >                                                                     |
| > 121.344(f)                                                          |
| >                                                                     |
| > 121.344(g)                                                          |
| >                                                                     |
| > 121.344(j)                                                          |
| >                                                                     |
| > 121.344a(a)(2)                                                      |
| >                                                                     |
| > 121.344a(b)(1)                                                      |
| >                                                                     |
| > 121.344a(b)(2)                                                      |
| >                                                                     |
| > 121.344a(c)                                                         |
| >                                                                     |
| > 121.344a(d)                                                         |
| >                                                                     |
| > 121.345(a)                                                          |
| >                                                                     |
| > 121.345(b)                                                          |
| >                                                                     |
| > 121.345(c)(1)(i)                                                    |
| >                                                                     |
| > 121.345(c)(1)(ii)                                                   |
| >                                                                     |
| > 121.345(c)(2)                                                       |
| >                                                                     |
| > 121.347(a)(1)                                                       |
| >                                                                     |
| > 121.347(a)(2)                                                       |
| >                                                                     |
| > 121.347(a)(3)                                                       |
| >                                                                     |
| > 121.347(b)                                                          |
| >                                                                     |
| > 121.349(a)                                                          |
| >                                                                     |
| > 121.349(b)                                                          |
| >                                                                     |
| > 121.349(c)                                                          |
| >                                                                     |
| > 121.349(e)                                                          |
| >                                                                     |
| > 121.351(a)                                                          |
| >                                                                     |
| > 121.354(a)                                                          |
| >                                                                     |
| > 121.354(b)                                                          |
| >                                                                     |
| > 121.355(a)(1)                                                       |
| >                                                                     |
| > 121.355(a)(2)                                                       |
| >                                                                     |
| > 121.356                                                             |
| >                                                                     |
| > 121.357(a)                                                          |
| >                                                                     |
| > 121.358(a)                                                          |
| >                                                                     |
| > 121.358(b)(1)(i)                                                    |
| >                                                                     |
| > 121.358(b)(1)(ii)                                                   |
| >                                                                     |
| > 121.358(b)(1)(iii)                                                  |
| >                                                                     |
| > 121.358(b)(1)(iv)                                                   |
| >                                                                     |
| > 121.358(b)(1)(ix)                                                   |
| >                                                                     |
| > 121.358(b)(1)(v)                                                    |
| >                                                                     |
| > 121.358(b)(1)(vi)                                                   |
| >                                                                     |
| > 121.358(b)(1)(vii)                                                  |
| >                                                                     |
| > 121.358(b)(1)(viii)                                                 |
| >                                                                     |
| > 121.358(b)(1)(x)                                                    |
| >                                                                     |
| > 121.358(b)(2)                                                       |
| >                                                                     |
| > 121.359(a)                                                          |
| >                                                                     |
| > 121.359(c)(2)(i)                                                    |
| >                                                                     |
| > 121.359(c)(2)(ii)                                                   |
| >                                                                     |
| > 121.359(c)(2)(iii)                                                  |
| >                                                                     |
| > 121.359(d)                                                          |
| >                                                                     |
| > 121.359(d)(1)                                                       |
| >                                                                     |
| > 121.359(d)(2)                                                       |
| >                                                                     |
| > 121.359(e)                                                          |
| >                                                                     |
| > 121.359(e)(1)                                                       |
| >                                                                     |
| > 121.359(e)(2)                                                       |
| >                                                                     |
| > 121.367                                                             |
| >                                                                     |
| > 121.367(a)                                                          |
| >                                                                     |
| > 121.370(a)                                                          |
| >                                                                     |
| > 121.380(a)(1)                                                       |
| >                                                                     |
| > 121.380(a)(2)(i)                                                    |
| >                                                                     |
| > 121.380(a)(2)(ii)                                                   |
| >                                                                     |
| > 121.380(a)(2)(iii)                                                  |
| >                                                                     |
| > 121.380(a)(2)(iv)                                                   |
| >                                                                     |
| > 121.380(a)(2)(v)                                                    |
| >                                                                     |
| > 121.380(a)(2)(vi)                                                   |
| >                                                                     |
| > 121.380(a)(2)(vii)                                                  |
| >                                                                     |
| > 121.380(c)(1)                                                       |
| >                                                                     |
| > 121.571(b)(1)                                                       |
| >                                                                     |
| > 121.571(b)(2)                                                       |
| >                                                                     |
| > 121.571(b)(3)                                                       |
| >                                                                     |
| > 121.576                                                             |
| >                                                                     |
| > 121.578(b)(1)                                                       |
| >                                                                     |
| > 121.578(b)(2)                                                       |
| >                                                                     |
| > 121.583(a)                                                          |
| >                                                                     |
| > 121.583(b)(1)                                                       |
| >                                                                     |
| > 121.583(b)(2)                                                       |
| >                                                                     |
| > 121.583(b)(3)                                                       |
| >                                                                     |
| > 121.585(d)                                                          |
| >                                                                     |
| > 121.585(d)(1)                                                       |
| >                                                                     |
| > 121.585(d)(10)                                                      |
| >                                                                     |
| > 121.585(d)(2)                                                       |
| >                                                                     |
| > 121.585(d)(3)                                                       |
| >                                                                     |
| > 121.585(d)(4)                                                       |
| >                                                                     |
| > 121.585(d)(5)                                                       |
| >                                                                     |
| > 121.585(d)(6)                                                       |
| >                                                                     |
| > 121.585(d)(7)                                                       |
| >                                                                     |
| > 121.585(d)(8)                                                       |
| >                                                                     |
| > 121.585(d)(9)                                                       |
| >                                                                     |
| > 121.589(c)                                                          |
| >                                                                     |
| > 121.589(f)                                                          |
| >                                                                     |
| > 121.803(a)                                                          |
| >                                                                     |
| > 121.803(c)(1)                                                       |
| >                                                                     |
| > 121.803(c)(2)                                                       |
| >                                                                     |
| > 121.803(c)(4)                                                       |
| >                                                                     |
| > 21.183(c)                                                           |
| >                                                                     |
| > 21.183(d)(1)                                                        |
| >                                                                     |
| > 21.41                                                               |
| >                                                                     |
| > 25.1303(b)(3)                                                       |
| >                                                                     |
| > 25.1303(c)(1)                                                       |
| >                                                                     |
| > 25.1307(d)                                                          |
| >                                                                     |
| > 25.1307(e)                                                          |
| >                                                                     |
| > 25.1326(b)(1)                                                       |
| >                                                                     |
| > 25.1326(b)(2)                                                       |
| >                                                                     |
| > 25.1459(a)                                                          |
| >                                                                     |
| > 25.1459(b)                                                          |
| >                                                                     |
| > 25.1459(c)                                                          |
| >                                                                     |
| > 25.1459(d)                                                          |
| >                                                                     |
| > 25.1459(d)(1)                                                       |
| >                                                                     |
| > 25.1459(d)(2)                                                       |
| >                                                                     |
| > 25.1459(e)                                                          |
| >                                                                     |
| > 25.1529                                                             |
| >                                                                     |
| > 25.1541(a)(1)                                                       |
| >                                                                     |
| > 25.1541(a)(2)                                                       |
| >                                                                     |
| > 25.1541(b)(1)                                                       |
| >                                                                     |
| > 25.1541(b)(2)                                                       |
| >                                                                     |
| > 25.1549(a)                                                          |
| >                                                                     |
| > 25.1549(b)                                                          |
| >                                                                     |
| > 25.1549(c)                                                          |
| >                                                                     |
| > 25.1549(d)                                                          |
| >                                                                     |
| > 25.2(a)                                                             |
| >                                                                     |
| > 25.785(g)                                                           |
| >                                                                     |
| > 25.785(h)                                                           |
| >                                                                     |
| > 25.789(b)                                                           |
| >                                                                     |
| > 25.791(a)                                                           |
| >                                                                     |
| > 25.791(c)                                                           |
| >                                                                     |
| > 25.791(d)                                                           |
| >                                                                     |
| > 25.811(d)(1)                                                        |
| >                                                                     |
| > 25.811(d)(2)                                                        |
| >                                                                     |
| > 25.812(b)(1)(i)                                                     |
| >                                                                     |
| > 25.812(b)(1)(ii)                                                    |
| >                                                                     |
| > 25.812(f)(2)                                                        |
| >                                                                     |
| > 25.853(a)                                                           |
| >                                                                     |
| > 25.853(d)(1)                                                        |
| >                                                                     |
| > 25.853(d)(3)                                                        |
| >                                                                     |
| > 25.857(e)(4)                                                        |
| >                                                                     |
| > 25.857(e)(5)                                                        |
| >                                                                     |
| > 25.963(e)(1)                                                        |
| >                                                                     |
| > 25.963(e)(2)                                                        |
| >                                                                     |
| > 25 App..H25.1(b)                                                    |
| >                                                                     |
| > 39.17                                                               |
| >                                                                     |
| > 39.19                                                               |
| >                                                                     |
| > 45.11(a)                                                            |
| >                                                                     |
| > 45.11(b)                                                            |
| >                                                                     |
| > 45.11(d)                                                            |
| >                                                                     |
| > 45.13(b)                                                            |
| >                                                                     |
| > 45.25                                                               |
| >                                                                     |
| > 45.29                                                               |
| >                                                                     |
| > 91.171(a)(1)                                                        |
| >                                                                     |
| > 91.171(a)(2)                                                        |
| >                                                                     |
| > 91.171(b)                                                           |
| >                                                                     |
| > 91.171(c)                                                           |
| >                                                                     |
| > 91.171(d)                                                           |
| >                                                                     |
| > 91.203(a)(1)                                                        |
| >                                                                     |
| > 91.203(a)(2)                                                        |
| >                                                                     |
| > 91.217(b)                                                           |
| >                                                                     |
| > 91.217(c)                                                           |
| >                                                                     |
| > 91.219(a)                                                           |
| >                                                                     |
| > 91.413(a)                                                           |
| >                                                                     |
| > 91.413(b)                                                           |
| >                                                                     |
| > 91.603                                                              |
| >                                                                     |
| > 91.607                                                              |
| >                                                                     |
| > 91.609(a)                                                           |
| >                                                                     |
| > 91.705(a)(1)                                                        |
| >                                                                     |
| > 91.853                                                              |
| >                                                                     |
| > 91.9(a)                                                             |
| >                                                                     |
| > 91.9(c)                                                             |
| >                                                                     |
| > 91 App..GSection 2(b)(1)                                            |
| >                                                                     |
| > 91 App..GSection 2(b)(2)                                            |
| >                                                                     |
| > B.036c(1)                                                           |
| >                                                                     |
| > D.072(c)                                                            |
| >                                                                     |
| > D.072(d)                                                            |
+-----------------------------------------------------------------------+

**Related CFRs & FAA Policy/Guidance**:

+-----------------------------------------------------------------------+
| -   Related CFRs:                                                     |
+=======================================================================+
| > Intentionally left blank                                            |
+-----------------------------------------------------------------------+

+-----------------------------------------------------------------------+
| -   FAA Policy/Guidance:                                              |
+=======================================================================+
| > FAA Order 8900.1, Volume 3, Ch 36, Sec 1                            |
| >                                                                     |
| > FAA Order 8900.1, Volume 3, Ch 43, Sec 1                            |
| >                                                                     |
| > FAA Order 8900.1, Volume 3, Ch 47, Sec 1                            |
| >                                                                     |
| > FAA Order 8900.1, Volume 4, Ch 4, Sec 1                             |
| >                                                                     |
| > FAA Order 8900.1, Volume 6, Ch 2, Sec 39                            |
| >                                                                     |
| > FAA Order 8900.1, Volume 6, Ch 11, Sec 14                           |
| >                                                                     |
| > AC 20-131A, Change 1                                                |
| >                                                                     |
| > AC 25-7A                                                            |
| >                                                                     |
| > AC 25-10                                                            |
| >                                                                     |
| > AC 25-15                                                            |
| >                                                                     |
| > AC 25-18                                                            |
| >                                                                     |
| > AC 43-4A                                                            |
| >                                                                     |
| > AC 20-42C                                                           |
| >                                                                     |
| > AC 25-18                                                            |
| >                                                                     |
| > AC 120-27E                                                          |
| >                                                                     |
| > AC 120-77                                                           |
| >                                                                     |
| > AC 120-73                                                           |
| >                                                                     |
| > AC 25-1329-1B                                                       |
| >                                                                     |
| > AD 90-25-03                                                         |
| >                                                                     |
| > AD 92-22-08 R1                                                      |
| >                                                                     |
| > AD 94-18-02                                                         |
+-----------------------------------------------------------------------+

+---+-------------------------------------------------------------------+
| * |                                                                   |
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| . |                                                                   |
+---+-------------------------------------------------------------------+
| # |                                                                   |
| # |                                                                   |
|   |                                                                   |
| T |                                                                   |
| a |                                                                   |
| s |                                                                   |
| k |                                                                   |
| s |                                                                   |
+---+-------------------------------------------------------------------+
|   | To meet this objective, the inspector must accomplish the         |
|   | following tasks:                                                  |
+---+-------------------------------------------------------------------+
| 1 | Review the information listed in the Supplemental Information     |
| \ | section of this DCT.                                              |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 2 | Review the certificate holder\'s policies, procedures,            |
| \ | instructions, and information for the Aircraft Airworthiness      |
| . | process.                                                          |
+---+-------------------------------------------------------------------+
| 3 | Review the last accomplished safety attribute inspection (SAI)    |
| \ | for this element with emphasis on the controls, process           |
| . | measurements, and interface attribute section responses.          |
+---+-------------------------------------------------------------------+
| 4 | Observe the certificate holder\'s Aircraft Airworthiness process  |
| \ | to gain an understanding of the procedures, instructions, and     |
| . | information.                                                      |
+---+-------------------------------------------------------------------+
| 5 | Discuss the Aircraft Airworthiness process with the personnel     |
| \ | (other than management) who perform the duties and                |
| . | responsibilities required by the (program/process).               |
+---+-------------------------------------------------------------------+

+---+------------------------------------------------------+-----------+
| # |                                                      |           |
| # |                                                      |           |
|   |                                                      |           |
| Q |                                                      |           |
| u |                                                      |           |
| e |                                                      |           |
| s |                                                      |           |
| t |                                                      |           |
| i |                                                      |           |
| o |                                                      |           |
| n |                                                      |           |
| s |                                                      |           |
+---+------------------------------------------------------+-----------+
|   | To meet this objective, the inspector must answer    |           |
|   | the following questions:                             |           |
+---+------------------------------------------------------+-----------+
| 1 | Determine whether the following performance measures |           |
| \ | were met:                                            |           |
| . |                                                      |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s aircraft meet the      | Yes       |
| . | requirements of the certificate holder\'s inspection |           |
| 1 | program and the program covering other maintenance,  | No,       |
| . | preventive maintenance, and alterations? **     **   | Explain   |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the aircraft, that it is has the       |           |
|   | proper registration certificate.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 2\. Check, at the aircraft, if the proper            |           |
|   | registration certificate is not on board, a FAA form |           |
|   | 8050-1, Application for Certificate of Registration  |           |
|   | has been completed.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 3\. Check, at the aircraft, that it carries an       |           |
|   | appropriate current airworthiness certificate.       |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 4\. Check, at the aircraft, (if required by          |           |
|   | procedures) for a current and approved Flight Manual |           |
|   | for that type of aircraft being operated.            |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(1); 121.141(a)                 |           |
|   |                                                      |           |
|   | 5\. Check, at the Technical Publications Library for |           |
|   | a current and approved Flight Manual for each type   |           |
|   | of aircraft being operated.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(1); 121.141(a)                 |           |
|   |                                                      |           |
|   | 6\. Check that the Certificate Holder has a current, |           |
|   | approved flight manual for that aircraft in          |           |
|   | accordance with the Certificate Holder\'s design.    |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.141(b)                 |           |
|   |                                                      |           |
|   | 7\. Check that the Certificate Holder who has        |           |
|   | prepared a manual that contains the information      |           |
|   | required from the applicable flight manual, that     |           |
|   | this information is clearly identified as flight     |           |
|   | manual requirements in accordance with the           |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.133(a); 121.135(a)(1); 121.141(b)     |           |
|   |                                                      |           |
|   | 8\. Check that the Certificate Holder\'s approved    |           |
|   | Minimum Equipment list is specific for that          |           |
|   | airplane.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.628(a)(1)              |           |
|   |                                                      |           |
|   | 9\. Check that the Certificate Holder\'s approved    |           |
|   | Weight and Balance manual was appropriate for the    |           |
|   | make model and series of the aircraft concerned.     |           |
|   |                                                      |           |
|   | *Sources:* FAA Order 8900.1, Vol 03, Ch 047, Para    |           |
|   | 3-3988.                                              |           |
|   |                                                      |           |
|   | 10\. Check, at the technical publications library,   |           |
|   | that the Certificate Holders manual, who was         |           |
|   | required by 14 CFR Part 121.391 to provide flight    |           |
|   | attendants, contains descriptions or diagrams,       |           |
|   | specific to each type/model of aircraft for Flight   |           |
|   | Attendants to perform their duties and               |           |
|   | responsibilities with a high degree of safety.       |           |
|   |                                                      |           |
|   | *Sources:* FAA Order 8900.1, Vol 03, Ch 032, Sec     |           |
|   | 013, Para 3-3426B, Fig 3-124.                        |           |
|   |                                                      |           |
|   | 11\. Check, at the aircraft, that there was a        |           |
|   | placard or marking stating any limitations on        |           |
|   | contents, including weight in each baggage and cargo |           |
|   | compartment, and each ballast location in accordance |           |
|   | with the Certificate Holder\'s design.               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1); 25.1557(a);       |           |
|   | 91.9(b)(2)                                           |           |
|   |                                                      |           |
|   | 12\. Check, at the aircraft, that there was a        |           |
|   | placard or marking with the word \"fuel\" at each    |           |
|   | fuel filler openings, at or near the filler cover,   |           |
|   | in accordance with the Certificate Holder\'s design. |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1); 25.1557(b)(1)(i); |           |
|   | 91.9(b)(2)                                           |           |
|   |                                                      |           |
|   | 13\. Check, at the reciprocating engine powered      |           |
|   | aircraft, that there was a placard or marking        |           |
|   | containing the minimum fuel grade, at or near the    |           |
|   | filler cover in accordance with the Certificate      |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1);                   |           |
|   | 25.1557(b)(1)(ii); 91.9(b)(2)                        |           |
|   |                                                      |           |
|   | 14\. Check, at the turbine engine powered aircraft,  |           |
|   | that there was a placard or marking containing the   |           |
|   | permissible fuel designations, at or near the filler |           |
|   | cover in accordance with the Certificate Holder\'s   |           |
|   | design.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1);                   |           |
|   | 25.1557(b)(1)(iii); 91.9(b)(2)                       |           |
|   |                                                      |           |
|   | 15\. Check, at the aircraft with a pressure fueling  |           |
|   | system, that there was a placard or marking          |           |
|   | containing the maximum permissible fueling supply    |           |
|   | pressure and the maximum permissible defueling       |           |
|   | pressure in accordance with the Certificate          |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1);                   |           |
|   | 25.1557(b)(1)(iv); 91.9(b)(2)                        |           |
|   |                                                      |           |
|   | 16\. Check, at the aircraft, that there was a        |           |
|   | marking or placard containing the word \"oil\" at or |           |
|   | near the oil filler cover in accordance with the     |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1); 25.1557(b)(2);    |           |
|   | 91.9(b)(2)                                           |           |
|   |                                                      |           |
|   | 17\. Check, at the aircraft, that there was a        |           |
|   | marking or placard identifying the required fluid at |           |
|   | or near augmentation fluid filler openings in        |           |
|   | accordance with the Certificate Holder\'s design.    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1); 25.1557(b)(3);    |           |
|   | 91.9(b)(2)                                           |           |
|   |                                                      |           |
|   | 18\. Check, at the turbine engine powered, transport |           |
|   | category aircraft, that all fuel tank covers located |           |
|   | in an area where experience or analysis indicates a  |           |
|   | strike was likely are impact resistant.              |           |
|   |                                                      |           |
|   | *Sources:* 121.316; 121.367; 25.963(e)(1)            |           |
|   |                                                      |           |
|   | 19\. Check that the Certificate Holder\'s inspection |           |
|   | program and a program covering other maintenance,    |           |
|   | preventive maintenance, and alterations ensures that |           |
|   | each passenger emergency exit on the side of the     |           |
|   | fuselage, has the means of opening that exit from    |           |
|   | the outside marked on the outside of the airplane.   |           |
|   |                                                      |           |
|   | *Sources:* 121.310(g); 121.367                       |           |
|   |                                                      |           |
|   | 20\. Check that the Certificate Holder\'s inspection |           |
|   | program and a program covering other maintenance,    |           |
|   | preventive maintenance, and alterations ensures that |           |
|   | there was a 2-inch colored band, readily             |           |
|   | distinguishable from the surrounding fuselage area   |           |
|   | by contrast in color, outlining each passenger       |           |
|   | emergency exit on the side of the fuselage.          |           |
|   |                                                      |           |
|   | *Sources:* 121.310(g); 121.367                       |           |
|   |                                                      |           |
|   | 21\. Check, at the aircraft, that each passenger     |           |
|   | emergency exit that is not on the side of the        |           |
|   | fuselage has the external means of opening and       |           |
|   | applicable instructions marked conspicuously in red  |           |
|   | or, if red was inconspicuous against the background  |           |
|   | color, in bright chrome yellow.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.310(g)(3); 121.367                    |           |
|   |                                                      |           |
|   | 22\. Check,at the all cargo aircraft with a class E  |           |
|   | cargo compartment, that required crew emergency      |           |
|   | exits are accessible under all cargo loading         |           |
|   | conditions in accordance with the Certificate        |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.221(f)(5); 121.367                    |           |
|   |                                                      |           |
|   | 23\. Check, at the aircraft with a passenger seating |           |
|   | configuration of 10 to 19 seats, that there was at   |           |
|   | least one Type III or larger exit in each side of    |           |
|   | the fuselage.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(g)(3)                     |           |
|   |                                                      |           |
|   | 24\. Check, at the aircraft with a passenger seating |           |
|   | configuration of 20 to 40 seats, that there was at   |           |
|   | least two exits, one of which must be a Type II or   |           |
|   | larger exit, in each side of the fuselage.           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(g)(4)                     |           |
|   |                                                      |           |
|   | 25\. Check, at the aircraft with a passenger seating |           |
|   | configuration of 41 to 110 seats, that there was at  |           |
|   | least two exits, one of which must be a Type I or    |           |
|   | larger exit, in each side of the fuselage.           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(g)(5)                     |           |
|   |                                                      |           |
|   | 26\. Check, at the aircraft with a passenger seating |           |
|   | configuration of more than 110 seats, that there was |           |
|   | at least two Type I or larger exits in each side of  |           |
|   | the fuselage.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(g)(6)                     |           |
|   |                                                      |           |
|   | 27\. Check, at the aircraft with all type III exits, |           |
|   | that combined maximum number of passenger seats was  |           |
|   | not more than 70.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(g)(7)                     |           |
|   |                                                      |           |
|   | 28\. Check, at the aircraft with two type III exits  |           |
|   | in each side of the fuselage that are separated by   |           |
|   | fewer than three passenger seat rows, that combined  |           |
|   | maximum number of passenger seats was not more than  |           |
|   | 65.                                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(g)(7)                     |           |
|   |                                                      |           |
|   | 29\. Check, at the aircraft, that there was a means  |           |
|   | to lock and safeguard each external door against     |           |
|   | opening in flight.                                   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.783(b)                        |           |
|   |                                                      |           |
|   | 30\. Check, at the aircraft with inward opening      |           |
|   | doors, that there was a means to prevent occupants   |           |
|   | from crowding against the door to an extent that     |           |
|   | would interfere with the opening of the door.        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.783(b)                        |           |
|   |                                                      |           |
|   | 31\. Check, at the aircraft with external doors      |           |
|   | including passenger, crew, service, and cargo doors, |           |
|   | for which the initial opening movement was not       |           |
|   | inward, that that there was a provision for direct   |           |
|   | visual inspection of the locking mechanism to        |           |
|   | determine they are fully closed and locked.          |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.783(e)                        |           |
|   |                                                      |           |
|   | 32\. Check, at the aircraft, that external doors     |           |
|   | have provisions to prevent the initiation of         |           |
|   | pressurization of the airplane to an unsafe level if |           |
|   | the door was not fully closed and locked.            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.783(f)                        |           |
|   |                                                      |           |
|   | 33\. Check, at the aircraft electrical/electronics   |           |
|   | compartments, that each item of installed equipment  |           |
|   | was labeled as to its identification, function, or   |           |
|   | operating limitations, or any applicable combination |           |
|   | of these factors.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1301(b)                       |           |
|   |                                                      |           |
|   | 34\. Check, at the aircraft electrical/electronics   |           |
|   | compartments, that cables are grouped, routed, and   |           |
|   | spaced so that damage to essential circuits will be  |           |
|   | minimized if there are faults in heavy               |           |
|   | current-carrying cables.                             |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1353(b)                       |           |
|   |                                                      |           |
|   | 35\. Check, at the aircraft electrical/electronics   |           |
|   | compartments, that main power cables (including      |           |
|   | generator cables) in the fuselage are isolated from  |           |
|   | flammable fluid lines or are shrouded by means of    |           |
|   | electrically insulated, flexible conduit, or         |           |
|   | equivalent, which was in addition to the normal      |           |
|   | cable insulation.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.869(a)(3)(i);                 |           |
|   | 25.869(a)(3)(ii)                                     |           |
|   |                                                      |           |
|   | 36\. Check, at the aircraft, that there was a means  |           |
|   | for indicating the adequacy of the power being       |           |
|   | supplied to required flight instruments.             |           |
|   |                                                      |           |
|   | *Sources:* 121.313(d); 121.367                       |           |
|   |                                                      |           |
|   | 37\. Check, at the passenger or combination          |           |
|   | cargo/passenger (combi) airplane, that has a         |           |
|   | passenger seat configuration, excluding any pilot    |           |
|   | seat, of 10 to 30 seats, that it was equipped with   |           |
|   | an approved traffic alert and collision avoidance    |           |
|   | system.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.356(b); 121.367                       |           |
|   |                                                      |           |
|   | 38\. Check, at the aircraft that has TCAS II         |           |
|   | installed, that the TCAS II meets TSO C-119b,        |           |
|   | (version 7.0) or later version.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.356(d); 121.367                       |           |
|   |                                                      |           |
|   | 39\. Check, at the transport category airplane       |           |
|   | (except c-46 type airplanes), that it was equipped   |           |
|   | with approved airborne weather radar.                |           |
|   |                                                      |           |
|   | *Sources:* 121.357(a); 121.367                       |           |
|   |                                                      |           |
|   | 40\. Check, the nontransport category airplane,      |           |
|   | certificated after December 31, 1964, that it was    |           |
|   | equipped with approved airborne weather radar.       |           |
|   |                                                      |           |
|   | *Sources:* 121.357(a); 121.367                       |           |
|   |                                                      |           |
|   | 41\. Check, at the turbine-engine powered airplane,  |           |
|   | manufactured after January 2, 1991, that it was      |           |
|   | equipped with either an approved airborne windshear  |           |
|   | warning and flight guidance system, an approved      |           |
|   | airborne detection and avoidance system, or an       |           |
|   | approved combination of these systems.               |           |
|   |                                                      |           |
|   | *Sources:* 121.358(a); 121.367                       |           |
|   |                                                      |           |
|   | 42\. Check, at the A-300-600 airplane, manufactured  |           |
|   | before January 3, 1991, that it was equipped with    |           |
|   | either an approved airborne windshear warning and    |           |
|   | flight guidance system, an approved airborne         |           |
|   | detection and avoidance system, or an approved       |           |
|   | combination of these systems.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(i); 121.367                 |           |
|   |                                                      |           |
|   | 43\. Check, at the A-310 airplane, manufactured      |           |
|   | before January 3, 1991, that it was equipped with    |           |
|   | either an approved airborne windshear warning and    |           |
|   | flight guidance system, an approved airborne         |           |
|   | detection and avoidance system, or an approved       |           |
|   | combination of these systems.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(ii); 121.367                |           |
|   |                                                      |           |
|   | 44\. Check, at the A-320 airplane, manufactured      |           |
|   | before January 3, 1991, that it was equipped with    |           |
|   | either an approved airborne windshear warning and    |           |
|   | flight guidance system, an approved airborne         |           |
|   | detection and avoidance system, or an approved       |           |
|   | combination of these systems.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(iii); 121.367               |           |
|   |                                                      |           |
|   | 45\. Check, at the B-737-300, 400, or 500 series     |           |
|   | airplane, manufactured before January 3, 1991, that  |           |
|   | it was equipped with either an approved airborne     |           |
|   | windshear warning and flight guidance system, an     |           |
|   | approved airborne detection and avoidance system, or |           |
|   | an approved combination of these systems.            |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(iv); 121.367                |           |
|   |                                                      |           |
|   | 46\. Check, at the B-747-400 airplane, manufactured  |           |
|   | before January 3, 1991, that it was equipped with    |           |
|   | either an approved airborne windshear warning and    |           |
|   | flight guidance system, an approved airborne         |           |
|   | detection and avoidance system, or an approved       |           |
|   | combination of these systems.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(v); 121.367                 |           |
|   |                                                      |           |
|   | 47\. Check, at the B-757 airplane, manufactured      |           |
|   | before January 3, 1991, that it was equipped with    |           |
|   | either an approved airborne windshear warning and    |           |
|   | flight guidance system, an approved airborne         |           |
|   | detection and avoidance system, or an approved       |           |
|   | combination of these systems.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(vi); 121.367                |           |
|   |                                                      |           |
|   | 48\. Check, at the B-767 airplane, manufactured      |           |
|   | before January 3, 1991, that it was equipped with    |           |
|   | either an approved airborne windshear warning and    |           |
|   | flight guidance system, an approved airborne         |           |
|   | detection and avoidance system, or an approved       |           |
|   | combination of these systems.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(vii); 121.367               |           |
|   |                                                      |           |
|   | 49\. Check, at the F-100 airplane, manufactured      |           |
|   | before January 3, 1991, that it was equipped with    |           |
|   | either an approved airborne windshear warning and    |           |
|   | flight guidance system, an approved airborne         |           |
|   | detection and avoidance system, or an approved       |           |
|   | combination of these systems.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(viii); 121.367              |           |
|   |                                                      |           |
|   | 50\. Check, at the MD-11 airplane, manufactured      |           |
|   | before January 3, 1991, that it was equipped with    |           |
|   | either an approved airborne windshear warning and    |           |
|   | flight guidance system, an approved airborne         |           |
|   | detection and avoidance system, or an approved       |           |
|   | combination of these systems.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(ix); 121.367                |           |
|   |                                                      |           |
|   | 51\. Check, at the MD-80 series airplane,            |           |
|   | manufactured before January 3, 1991, that it was     |           |
|   | equipped with either an approved airborne windshear  |           |
|   | warning and flight guidance system, an approved      |           |
|   | airborne detection and avoidance system, or an       |           |
|   | approved combination of these systems.               |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(1)(x); 121.367                 |           |
|   |                                                      |           |
|   | 52\. Check, at the turbine-engine powered airplane,  |           |
|   | manufactured before January 3, 1991, that it was     |           |
|   | equipped with an approved airborne windshear warning |           |
|   | system, an approved airborne windshear detection and |           |
|   | avoidance system, or an approved combination of      |           |
|   | these systems.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.358(b)(2); 121.367                    |           |
|   |                                                      |           |
|   | 53\. Check, at the turbine-engine powered airplane,  |           |
|   | that it was equipped with a ground proximity warning |           |
|   | system that meets the performance and environmental  |           |
|   | standards of TSO-C92.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.360(a); 121.367                       |           |
|   |                                                      |           |
|   | 54\. Check, at the turbine-powered airplane, that it |           |
|   | was equipped with a ground proximity warning/glide   |           |
|   | slope deviation alerting system that meets the       |           |
|   | performance and environmental standards contained in |           |
|   | TSO-C92a or TSO-C92b or incorporates TSO-approved    |           |
|   | ground proximity warning-glide slope deviation       |           |
|   | alerting equipment.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.360(e); 121.367                       |           |
|   |                                                      |           |
|   | 55\. Check, at the turbojet-powered engine powered   |           |
|   | airplane, that it was equipped with an approved      |           |
|   | altitude alerting system or device.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 91.219(a)                        |           |
|   |                                                      |           |
|   | 56\. Check, at the turbine engine powered airplane,  |           |
|   | manufactured after March 29, 2002, that it was       |           |
|   | equipped with an approved terrain awareness and      |           |
|   | warning system that meets the requirements for Class |           |
|   | A equipment in Technical Standard Order (TSO)-C151   |           |
|   | and an approved terrain situational awareness        |           |
|   | display.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.354(a); 121.367                       |           |
|   |                                                      |           |
|   | 57\. Check, at the aircraft, that it was equipped    |           |
|   | with a takeoff warning system that provides to the   |           |
|   | pilots an aural warning that was automatically       |           |
|   | activated during the initial portion of the takeoff  |           |
|   | roll if the wing flaps or leading edge devices are   |           |
|   | not within the approved range of takeoff positions.  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.703(a)(1)                     |           |
|   |                                                      |           |
|   | 58\. Check, at the aircraft, that it was equipped    |           |
|   | with a takeoff warning system that provides to the   |           |
|   | pilots an aural warning that was automatically       |           |
|   | activated during the initial portion of the takeoff  |           |
|   | roll if the wing spoilers (except lateral control    |           |
|   | spoilers meeting the requirements of Sec. 25.671),   |           |
|   | speed brakes, or longitudinal trim devices are in a  |           |
|   | position that would not allow a safe takeoff.        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.703(a)(2)                     |           |
|   |                                                      |           |
|   | 59\. Check, at the nontransport category airplane    |           |
|   | manufactured after December 20, 1999, that a takeoff |           |
|   | warning system was installed that provides to the    |           |
|   | pilots an aural warning that was automatically       |           |
|   | activated during the initial portion of the takeoff  |           |
|   | roll if the wing flaps or leading edge devices are   |           |
|   | not within the approved range of takeoff positions.  |           |
|   |                                                      |           |
|   | *Sources:* 121.293; 121.367; 25.703(a)(1)            |           |
|   |                                                      |           |
|   | 60\. Check, at the aircraft with an established      |           |
|   | approach wing-flap position, that the airplane has a |           |
|   | landing gear aural warning device that functions     |           |
|   | continuously whenever the wing flaps are extended    |           |
|   | beyond the maximum certificated approach climb       |           |
|   | configuration position in the Airplane Flight Manual |           |
|   | and the landing gear was not fully extended and      |           |
|   | locked.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.289(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 61\. Check, at the aircraft that it was operated     |           |
|   | with an established approach wing-flap position,     |           |
|   | that it has a landing gear aural warning device that |           |
|   | functions continuously whenever the wing flaps are   |           |
|   | extended beyond the position at which landing gear   |           |
|   | extension was normally performed and the landing     |           |
|   | gear was not fully extended and locked.              |           |
|   |                                                      |           |
|   | *Sources:* 121.289(a)(2); 121.367                    |           |
|   |                                                      |           |
|   | 62\. Check, at the aircraft that it was operated in  |           |
|   | airspace designated as Minimum Navigation            |           |
|   | Performance Specifications (MNPS) airspace, that it  |           |
|   | has approved navigation performance capability that  |           |
|   | complies with the requirements of appendix C of 14   |           |
|   | CFR part 91.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 91.705(a)(1)                     |           |
|   |                                                      |           |
|   | 63\. Check, at the aircraft, that it was operated in |           |
|   | airspace designated as Required Navigation           |           |
|   | Performance 10 (RNP-10) airspace using two           |           |
|   | independent inertial navigation systems (INS), that  |           |
|   | the navigation system was installed and operational. |           |
|   |                                                      |           |
|   | *Sources:* 121.367; B.036Class II Navigation         |           |
|   |                                                      |           |
|   | 64\. Check, at the aircraft, that it was operated in |           |
|   | airspace designated as Required Navigation           |           |
|   | Performance 10 (RNP-10) airspace using two flight    |           |
|   | management system/navigation sensor combinations (or |           |
|   | equivalent) that the navigation system was installed |           |
|   | and operational.                                     |           |
|   |                                                      |           |
|   | *Sources:* 121.367; B.036Class II Navigation         |           |
|   |                                                      |           |
|   | 65\. Check, at the aircraft, that it was operated in |           |
|   | airspace designated as Required Navigation           |           |
|   | Performance 10 (RNP-10) airspace using two           |           |
|   | independent approved GPS navigation systems          |           |
|   | acceptable for primary means of Class II navigation  |           |
|   | in oceanic and remote areas, that the navigation     |           |
|   | system was installed and operational.                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; B.036Class II Navigation         |           |
|   |                                                      |           |
|   | 66\. Check, at the aircraft, that it was operated in |           |
|   | airspace designated as Required Navigation           |           |
|   | Performance 10 (RNP-10) airspace using inertial      |           |
|   | navigation systems that use a mixed position         |           |
|   | solution (e.g., triple mix) that the navigation      |           |
|   | system was installed and operational.                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; B.036Class II Navigation         |           |
|   |                                                      |           |
|   | 67\. Check, at the aircraft, that the cockpit seat   |           |
|   | cushions meet the applicable flammability            |           |
|   | requirements under which the airplane was type       |           |
|   | certificated.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.312(d); 121.367                       |           |
|   |                                                      |           |
|   | 68\. Check, at the aircraft tin which the proximity  |           |
|   | of passenger emergency exits to the flightcrew area  |           |
|   | does not offer a convenient and readily accessible   |           |
|   | means of evacuation of the flightcrew, that exits of |           |
|   | sufficient size, are located in the flightcrew area  |           |
|   | so as to permit rapid evacuation by the crew.        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(j)                        |           |
|   |                                                      |           |
|   | 69\. Check, at the aircraft having a passenger       |           |
|   | seating capacity greater than 20, that exit of       |           |
|   | sufficient size, are located in the flightcrew area  |           |
|   | so as to permit rapid evacuation by the crew.        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(j)                        |           |
|   |                                                      |           |
|   | 70\. Check, at the aircraft, that a movable door on  |           |
|   | each side of the fuselage or top hatch in the        |           |
|   | external walls of the fuselage was provided allowing |           |
|   | unobstructed opening to the outside for flightcrew   |           |
|   | emergency exit.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(j); 25.809(a)             |           |
|   |                                                      |           |
|   | 71\. Check, at the aircraft, that a seat was         |           |
|   | available on the flight deck for occupancy by the    |           |
|   | Administrator while conducting en route inspections. |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.581(a)                 |           |
|   |                                                      |           |
|   | 72\. Check, at the aircraft, that specified markings |           |
|   | and placards are displayed in conspicuous places     |           |
|   | that may not be easily erased, disfigured, or        |           |
|   | obscured.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1); 25.1541(b)(1);    |           |
|   | 25.1541(b)(2)                                        |           |
|   |                                                      |           |
|   | 73\. Check, at the aircraft, that was type           |           |
|   | certificated under Aero Bulletin 7A or Part 04 of    |           |
|   | the Civil Air Regulations in effect before November  |           |
|   | 1, 1946, that each compartment used by the crew or   |           |
|   | passengers was at least flash resistant.             |           |
|   |                                                      |           |
|   | *Sources:* 121.211(b); 121.215(a); 121.215(b);       |           |
|   | 121.367                                              |           |
|   |                                                      |           |
|   | 74\. Check, at the aircraft, that was type           |           |
|   | certificated under Aero Bulletin 7A or Part 04 of    |           |
|   | the Civil Air Regulations in effect before November  |           |
|   | 1, 1946 that the wall and ceiling linings and the    |           |
|   | covering of upholstering, floors, and furnishings of |           |
|   | each compartment used by the crew or passengers was  |           |
|   | flame resistant.                                     |           |
|   |                                                      |           |
|   | *Sources:* 121.211(b); 121.215(c); 121.367           |           |
|   |                                                      |           |
|   | 75\. Check, at a transport category airplane with    |           |
|   | passenger seating capacity of 20 or more             |           |
|   | manufactured after August 19, 1988, that all         |           |
|   | interior materials in each compartment used by the   |           |
|   | crewmembers and passengers, has met the test         |           |
|   | requirements of parts IV and V of Appendix F of FAR  |           |
|   | part 25, or other approved equivalent method.        |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(1)(i); 121.367; 25.853(d)      |           |
|   |                                                      |           |
|   | 76\. Check, at a nontransport category airplane type |           |
|   | certificated before January 1, 1965, manufactured    |           |
|   | after August 19, 1988, with passenger seating        |           |
|   | capacity of 20 or more, that all interior materials  |           |
|   | in each compartment used by the crewmembers and      |           |
|   | passengers, has met the test requirements of parts   |           |
|   | IV and V of Appendix F of FAR part 25, or other      |           |
|   | approved equivalent method.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(1)(i); 121.367; 25.853(d)      |           |
|   |                                                      |           |
|   | 77\. Check, at a transport category airplane type    |           |
|   | certificated before January 1, 1965, manufactured    |           |
|   | after August 19, 1990, with passenger seating        |           |
|   | capacity of 20 or more, that all interior materials  |           |
|   | in each compartment used by the crewmembers and      |           |
|   | passengers has met the test requirements of parts IV |           |
|   | and V of Appendix F of FAR part 25, or other         |           |
|   | approved equivalent method.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(1)(ii); 121.367; 25.853(d)     |           |
|   |                                                      |           |
|   | 78\. Check, at a nontransport category airplane type |           |
|   | certificated before January 1, 1965, manufactured    |           |
|   | after August 19, 1990, with passenger seating        |           |
|   | capacity of 20 or more that all interior materials   |           |
|   | in each compartment used by the crewmembers and      |           |
|   | passengers has met the test requirements of parts IV |           |
|   | and V of Appendix F of FAR part 25, or other         |           |
|   | approved equivalent method.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(1)(ii); 121.367; 25.853(d)     |           |
|   |                                                      |           |
|   | 79\. Check, at a transport category airplane for     |           |
|   | which application for type certificate was filed     |           |
|   | prior to May 1, 1972, that, if there was a           |           |
|   | substantially complete replacement of the cabin      |           |
|   | interior on or after May 1, 1972, that all interior  |           |
|   | materials in each compartment continues to comply    |           |
|   | with the provisions of Sec. 25.853.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(2)(i); 121.367                 |           |
|   |                                                      |           |
|   | 80\. Check, at a nontransport category airplane for  |           |
|   | which application for type certificate was filed     |           |
|   | prior to May 1, 1972, that, if there was a           |           |
|   | substantially complete replacement of the cabin      |           |
|   | interior on or after May 1, 1972, that all interior  |           |
|   | materials in each compartment continues to comply    |           |
|   | with the provisions of Sec. 25.853.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(2)(i); 121.367                 |           |
|   |                                                      |           |
|   | 81\. Check, at a transport category airplane for     |           |
|   | which the application for type certificate was filed |           |
|   | on or after May 1, 1972 that, if there was a         |           |
|   | substantially complete replacement of the cabin      |           |
|   | interior on or after August 20, 1990, all interior   |           |
|   | materials in each compartment continues to comply    |           |
|   | with the material requirements under which the       |           |
|   | airplane was type certificated, regardless of        |           |
|   | passenger capacity.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(2)(ii); 121.367                |           |
|   |                                                      |           |
|   | 82\. Check, at a nontransport category airplane for  |           |
|   | which the application for type certificate was filed |           |
|   | on or after May 1, 1972, that, if there was a        |           |
|   | substantially complete replacement of the cabin      |           |
|   | interior on or after August 20, 1990, all interior   |           |
|   | materials in each compartment continues to comply    |           |
|   | with the material requirements under which the       |           |
|   | airplane was type certificated, regardless of        |           |
|   | passenger capacity.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(2)(ii); 121.367                |           |
|   |                                                      |           |
|   | 83\. Check, at a transport category airplane, type   |           |
|   | certificated after January 1, 1958 with a seating    |           |
|   | capacity of 20 or more, that, if there was a         |           |
|   | substantially complete replacement of the cabin      |           |
|   | interior components identified in Sec. 25.853(d), on |           |
|   | or after March 6, 1995, all interior materials in    |           |
|   | each compartment continues to comply with the heat   |           |
|   | release rate testing provisions of Sec. 25.853(d).   |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(3)(i); 121.367                 |           |
|   |                                                      |           |
|   | 84\. Check, at a nontransport category airplane,     |           |
|   | type certificated after January 1, 1958 with a       |           |
|   | seating capacity of 20 or more that, if there was a  |           |
|   | substantially complete replacement of the cabin      |           |
|   | interior components identified in Sec. 25.853(d), on |           |
|   | or after March 6, 1995, all interior materials in    |           |
|   | each compartment continues to comply with the heat   |           |
|   | release rate testing provisions of Sec. 25.853(d).   |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(3)(i); 121.367                 |           |
|   |                                                      |           |
|   | 85\. Check, at a transport category airplane type    |           |
|   | certificated before January 1, 1965, with a seating  |           |
|   | capacity of 20 or more that, if there was a          |           |
|   | substantially complete replacement of the cabin      |           |
|   | interior components identified in Sec. 25.853(d), on |           |
|   | or after August 20, 1990 all interior materials in   |           |
|   | each compartment continues to comply with the heat   |           |
|   | release rate and smoke testing provisions of Sec.    |           |
|   | 25.853(d).                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(3)(ii); 121.367; 25.853(d)     |           |
|   |                                                      |           |
|   | 86\. Check, at a nontransport category airplane type |           |
|   | certificated before January 1, 1965, with a seating  |           |
|   | capacity of 20 or more, that, if there was a         |           |
|   | substantially complete replacement of the cabin      |           |
|   | interior components identified in Sec. 25.853(d), on |           |
|   | or after August 20, 1990 all interior materials in   |           |
|   | each compartment continues to comply with the heat   |           |
|   | release rate and smoke testing provisions of Sec.    |           |
|   | 25.853(d).                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(3)(ii); 121.367; 25.853(d)     |           |
|   |                                                      |           |
|   | 87\. Check, at a transport category airplane type    |           |
|   | certificated after January 1, 1958, that seat        |           |
|   | cushions, except those on flight crewmember seats,   |           |
|   | in each compartment occupied by crew or passengers,  |           |
|   | continues to meet the test requirements of part II   |           |
|   | of FAR 25, Appendix F or other equivalent methods.   |           |
|   |                                                      |           |
|   | *Sources:* 121.312(b)(1); 121.367; 25.853(c)         |           |
|   |                                                      |           |
|   | 88\. Check at the aircraft that, printed cards       |           |
|   | supplementing the oral briefing pertinent only to    |           |
|   | that type and model airplane, are in convenient      |           |
|   | locations for each passengers use, containing        |           |
|   | diagrams of, and methods of operating, the emergency |           |
|   | exits.                                               |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(10); 121.571(b)(1);            |           |
|   | 121.571(b)(2)                                        |           |
|   |                                                      |           |
|   | 89\. Check at the aircraft that, printed cards       |           |
|   | supplementing the oral briefing pertinent only to    |           |
|   | that type and model airplane, are in convenient      |           |
|   | locations for each passengers use, containing        |           |
|   | instructions necessary for use of emergency          |           |
|   | equipment.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(10); 121.571(b)(1);            |           |
|   | 121.571(b)(2)                                        |           |
|   |                                                      |           |
|   | 90\. Check at the aircraft that, in the event of an  |           |
|   | emergency, information cards at each exit seat       |           |
|   | includes information in the language in which the    |           |
|   | crew briefings and oral commands are given to locate |           |
|   | the emergency exit, are presented.                   |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(1)  |           |
|   |                                                      |           |
|   | 91\. Check at the aircraft that, in the event of an  |           |
|   | emergency, information cards at each exit seat       |           |
|   | includes information in the language in which the    |           |
|   | crew briefings and oral commands are given, to       |           |
|   | recognize the emergency exit opening mechanism at    |           |
|   | each exit.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(2)  |           |
|   |                                                      |           |
|   | 92\. Check at the aircraft that, in the event of an  |           |
|   | emergency, information cards at each exit seat       |           |
|   | includes information in the language in which the    |           |
|   | crew briefings and oral commands are given, to       |           |
|   | comprehend the instructions for operating the        |           |
|   | emergency exit.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(3)  |           |
|   |                                                      |           |
|   | 93\. Check at the aircraft that, in the event of an  |           |
|   | emergency, information cards at each exit seat       |           |
|   | includes information in the language in which the    |           |
|   | crew briefings and oral commands are given, to       |           |
|   | operate the emergency exit.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(4)  |           |
|   |                                                      |           |
|   | 94\. Check at the aircraft that, in the event of an  |           |
|   | emergency, information cards at each exit seat       |           |
|   | includes information in the language in which the    |           |
|   | crew briefings and oral commands are given, to       |           |
|   | assess whether opening the emergency exit will       |           |
|   | increase the hazards to which passengers may be      |           |
|   | exposed.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(5)  |           |
|   |                                                      |           |
|   | 95\. Check at the aircraft that, in the event of an  |           |
|   | emergency, information cards at each exit seat       |           |
|   | includes information in the language in which the    |           |
|   | crew briefings and oral commands are given, to       |           |
|   | follow oral directions and hand signals given by a   |           |
|   | crewmember.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(6)  |           |
|   |                                                      |           |
|   | 96\. Check at the aircraft that, information cards   |           |
|   | are made available which include information, in the |           |
|   | event of an emergency, to stow or secure the         |           |
|   | emergency exit door so that it will not impede use   |           |
|   | of the exit.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(7)  |           |
|   |                                                      |           |
|   | 97\. Check at the aircraft that, information cards   |           |
|   | are made available which include information, in the |           |
|   | event of an emergency, to assess the condition of an |           |
|   | escape slide, activate the slide, and stabilize the  |           |
|   | slide after deployment to assist others in getting   |           |
|   | off the slide.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(8)  |           |
|   |                                                      |           |
|   | 98\. Check at the aircraft that, information cards   |           |
|   | are made available which include information, in the |           |
|   | event of an emergency, to pass expeditiously through |           |
|   | the emergency exit.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(9)  |           |
|   |                                                      |           |
|   | 99\. Check at the aircraft that, information cards   |           |
|   | are made available which include information, in the |           |
|   | event of an emergency, for passengers to assess,     |           |
|   | select, and follow a safe path away from the         |           |
|   | emergency exit.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.571(b); 121.585(d)(10) |           |
|   |                                                      |           |
|   | 100\. Check at the aircraft that, there was a sign   |           |
|   | or placard installed in each lavatory that reads:    |           |
|   | \"Federal law provides for a penalty of up to        |           |
|   | \$2,000 for tampering with the smoke detector        |           |
|   | installed in this lavatory\".                        |           |
|   |                                                      |           |
|   | *Sources:* 121.317(e); 121.367                       |           |
|   |                                                      |           |
|   | 101\. Check at the aircraft that, all floor surface  |           |
|   | areas, which are likely to become wet in service,    |           |
|   | have slip resistant properties.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.793                           |           |
|   |                                                      |           |
|   | 102\. Check at the aircraft that, was type           |           |
|   | certificated under Aero Bulletin 7A or Part 04 of    |           |
|   | the Civil Air Regulations in effect before November  |           |
|   | 1, 1946, that each compartment where smoking was to  |           |
|   | be allowed it was equipped with self-contained ash   |           |
|   | trays that are completely removable.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.211(b); 121.215(d); 121.367           |           |
|   |                                                      |           |
|   | 103\. Check at the aircraft that, lavatories have    |           |
|   | self-contained, removable ashtrays located           |           |
|   | conspicuously on or near the entry side of each      |           |
|   | lavatory door. One ashtray may serve more than one   |           |
|   | lavatory door if the ashtray can be seen readily     |           |
|   | from the cabin side of each lavatory served.         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(g)                        |           |
|   |                                                      |           |
|   | 104\. Check at the aircraft that, was type           |           |
|   | certificated under Aero Bulletin 7A or Part 04 of    |           |
|   | the Civil Air Regulations in effect before November  |           |
|   | 1, 1946, that each receptacle used for towels,       |           |
|   | papers, and waste was of fire-resistant material.    |           |
|   |                                                      |           |
|   | *Sources:* 121.211(b); 121.215(e); 121.367           |           |
|   |                                                      |           |
|   | 105\. Check at the aircraft that, was type           |           |
|   | certificated under Aero Bulletin 7A or Part 04 of    |           |
|   | the Civil Air Regulations in effect before November  |           |
|   | 1, 1946, that each receptacle used for towels,       |           |
|   | papers, and waste has a cover or other means of      |           |
|   | containing possible fires started in the             |           |
|   | receptacles.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.211(b); 121.215(e); 121.367           |           |
|   |                                                      |           |
|   | 106\. Check at the aircraft that, a placard was      |           |
|   | located on or adjacent to the door of each           |           |
|   | receptacle used for the disposal of flammable waste  |           |
|   | materials to indicate that use of the receptacle for |           |
|   | disposal of cigarettes, etc., was prohibited.        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.791(c)                        |           |
|   |                                                      |           |
|   | 107\. Check at the aircraft that, there was a door   |           |
|   | between the passenger and pilot compartments (i.e.,  |           |
|   | flightdeck door), with a locking means to prevent    |           |
|   | passengers from opening it without the pilot\'s      |           |
|   | permission.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.313(f); 121.367                       |           |
|   |                                                      |           |
|   | 108\. Check at the aircraft that was equipped with a |           |
|   | crew rest area having separate entries from the      |           |
|   | flightdeck and the passenger compartment that there  |           |
|   | was a door between the crew rest area and the        |           |
|   | passenger compartment, with a locking means to       |           |
|   | prevent passengers from opening it without the       |           |
|   | pilot\'s permission.                                 |           |
|   |                                                      |           |
|   | *Sources:* 121.313(f); 121.367                       |           |
|   |                                                      |           |
|   | 109\. Check at the aircraft that, the flight deck    |           |
|   | door will resist forcible intrusion by unauthorized  |           |
|   | persons and be capable of withstanding impacts of    |           |
|   | 300 Joules (221.3 foot-pounds) at the critical       |           |
|   | locations on the door, as well as a 250 pound (1113  |           |
|   | Newtons) constant tensile load on the knob or        |           |
|   | handle.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.313(j)(1); 121.367; 25.795(a)(1)      |           |
|   |                                                      |           |
|   | 110\. Check at the aircraft that, the flight deck    |           |
|   | door will resist penetration by small arms fire and  |           |
|   | fragmentation devices to a level equivalent to level |           |
|   | IIIa of the National Institute of Justice Standard   |           |
|   | (NIJ) 0101.04.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.313(j)(1); 121.367; 25.795(a)(2)      |           |
|   |                                                      |           |
|   | 111\. Check at the aircraft, with a lockable door    |           |
|   | installed between the pilot compartment and the      |           |
|   | passenger compartment, and a maximum passenger       |           |
|   | seating configuration of more than 20 seats, that    |           |
|   | the emergency exit configuration was designed so     |           |
|   | that neither crewmembers nor passengers require use  |           |
|   | of the flightdeck door in order to reach the         |           |
|   | emergency exits provided for them.                   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.772(a)                        |           |
|   |                                                      |           |
|   | 112\. Check at the aircraft, that was type           |           |
|   | certificated under Aero Bulletin 7A or Part 04 of    |           |
|   | the Civil Air Regulations in effect before November  |           |
|   | 1, 1946, that where internal doors are equipped with |           |
|   | louvers or other ventilating means, there was a      |           |
|   | means, convenient to the crew, for closing the flow  |           |
|   | of air through the door when necessary.              |           |
|   |                                                      |           |
|   | *Sources:* 121.211(b); 121.217; 121.367              |           |
|   |                                                      |           |
|   | 113\. Check at the aircraft, that was type           |           |
|   | certificated under Aero Bulletin 7A or Part 04 of    |           |
|   | the Civil Air Regulations in effect before November  |           |
|   | 1, 1946, that there was suitable ventilation in each |           |
|   | passenger or crew compartment.                       |           |
|   |                                                      |           |
|   | *Sources:* 121.211(b); 121.219; 121.367              |           |
|   |                                                      |           |
|   | 114\. Check at the aircraft, in the passenger        |           |
|   | compartment, that cargo was carried in an approved   |           |
|   | cargo bin that was not installed in a position that  |           |
|   | restricts access to or use of any required emergency |           |
|   | exit, or of the aisle in the passenger compartment.  |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(5); 121.367                    |           |
|   |                                                      |           |
|   | 115\. Check at the aircraft, that a cargo stowage    |           |
|   | compartment was placarded for its maximum weight and |           |
|   | providing proper restraint for all baggage or cargo  |           |
|   | stowed within, and in a manner that does not hinder  |           |
|   | the possible use of any emergency equipment was      |           |
|   | provided for each article of baggage to be stowed.   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.589(c)(1)                    |           |
|   |                                                      |           |
|   | 116\. Check at the aircraft, that each passenger     |           |
|   | seat, under which baggage was to be stowed, was      |           |
|   | fitted with a means to prevent articles of baggage   |           |
|   | stowed under it from sliding forward.                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.589(f)                       |           |
|   |                                                      |           |
|   | 117\. Check at the aircraft, that each aisle seat    |           |
|   | was fitted with a means to prevent articles of       |           |
|   | baggage stowed under it from sliding sideward into   |           |
|   | the aisle.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.589(f)                       |           |
|   |                                                      |           |
|   | 118\. Check at an aircraft that each crew and        |           |
|   | passenger area has an emergency means to allow rapid |           |
|   | evacuation in crash landings, with the landing gear  |           |
|   | extended as well as with the landing gear retracted, |           |
|   | considering the possibility of the airplane being on |           |
|   | fire.                                                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.803(a)                        |           |
|   |                                                      |           |
|   | 119\. Check at an aircraft with a service            |           |
|   | compartment located below the main deck, which may   |           |
|   | be occupied during taxi or flight but not during     |           |
|   | takeoff or landing, that there was at least two      |           |
|   | emergency evacuation routes, one at each end of each |           |
|   | lower deck service compartment or two having         |           |
|   | sufficient separation within each compartment, which |           |
|   | could be used by each occupant of the lower deck     |           |
|   | service compartment and to rapidly evacuate to the   |           |
|   | main deck under normal and emergency lighting        |           |
|   | conditions.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.819(a)                        |           |
|   |                                                      |           |
|   | 120\. Check at an aircraft with a service            |           |
|   | compartment located below the main deck, which may   |           |
|   | be occupied during taxi or flight but not during     |           |
|   | takeoff or landing, that there are at least two      |           |
|   | emergency evacuation routes that provide for the     |           |
|   | evacuation of incapacitated persons, with            |           |
|   | assistance.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.819(a)                        |           |
|   |                                                      |           |
|   | 121\. Check at an aircraft with a service            |           |
|   | compartment located below the main deck, which may   |           |
|   | be occupied during taxi or flight but not during     |           |
|   | takeoff or landing, that there are at least two      |           |
|   | emergency evacuation routes that are not dependent   |           |
|   | on any powered device.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.819(a)                        |           |
|   |                                                      |           |
|   | 122\. Check at an aircraft with a service            |           |
|   | compartment located below the main deck, which may   |           |
|   | be occupied during taxi or flight but not during     |           |
|   | takeoff or landing, that in the event the            |           |
|   | airplane\'s main power system or compartment main    |           |
|   | lighting system should fail, emergency illumination  |           |
|   | for each lower deck service compartment was          |           |
|   | automatically provided.                              |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.819(a)                        |           |
|   |                                                      |           |
|   | 123\. Check at an aircraft with a service            |           |
|   | compartment located below the main deck, which may   |           |
|   | be occupied during taxi or flight but not during     |           |
|   | takeoff or landing, that there was an aural          |           |
|   | emergency alarm system, audible during normal and    |           |
|   | emergency conditions, to enable crewmembers on the   |           |
|   | flight deck and at each required floor level         |           |
|   | emergency exit to alert occupants of each lower deck |           |
|   | service compartment of an emergency situation.       |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.819(c)                        |           |
|   |                                                      |           |
|   | 124\. Check at the aircraft, that when oxygen is     |           |
|   | supplied to both crew and passengers, the            |           |
|   | distribution system is designed for either a source  |           |
|   | of supply for the flight crew on duty and a separate |           |
|   | source for the passengers and other crewmembers; or  |           |
|   | a common source of supply with means to separately   |           |
|   | reserve the minimum supply required by the flight    |           |
|   | crew on duty.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1445(a)(1); 25.1445(a)(2)     |           |
|   |                                                      |           |
|   | 125\. Check at the aircraft,, if oxygen dispensing   |           |
|   | units are installed, there was an individual         |           |
|   | dispensing unit for each occupant for whom           |           |
|   | supplemental oxygen is to be supplied, designed to   |           |
|   | cover the nose and mouth and was equipped with a     |           |
|   | suitable means to retain the unit in position on the |           |
|   | face.                                                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1447(a)                       |           |
|   |                                                      |           |
|   | 126\. Check at an aircraft, that operates up to and  |           |
|   | including 25,000 feet, that an oxygen supply         |           |
|   | terminal and unit of oxygen dispensing equipment for |           |
|   | the immediate use of oxygen by each crewmember was   |           |
|   | within easy reach of that crewmember.                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1447(b)                       |           |
|   |                                                      |           |
|   | 127\. Check at an aircraft that operates above       |           |
|   | 25,000 feet that there is an oxygen-dispensing unit  |           |
|   | connected to oxygen supply terminals immediately     |           |
|   | available to each occupant, wherever seated.         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1447(c)(1)                    |           |
|   |                                                      |           |
|   | 128\. Check at an aircraft that operates above       |           |
|   | 25,000 feet, that there was at least two oxygen      |           |
|   | dispensing units connected to oxygen terminals in    |           |
|   | each lavatory.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1447(c)(1)                    |           |
|   |                                                      |           |
|   | 129\. Check at an aircraft that operates above       |           |
|   | 25,000 feet, that the total number of dispensing     |           |
|   | units and outlets in the cabin exceeds the number of |           |
|   | seats by at least 10 percent and the extra units are |           |
|   | as uniformly distributed throughout the cabin as     |           |
|   | practicable.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1447(c)(1)                    |           |
|   |                                                      |           |
|   | 130\. Check at an aircraft that operates above       |           |
|   | 30,000 feet, has an inspection program and program   |           |
|   | covering other maintenance, preventive maintenance   |           |
|   | and alterations that ensures that the crew is        |           |
|   | provided with a manual means of making the           |           |
|   | dispensing units immediately available in the event  |           |
|   | of failure of the automatic system.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1447(c)(1)                    |           |
|   |                                                      |           |
|   | 131\. Check at the aircraft, that there is a means   |           |
|   | to allow the crew to determine whether oxygen is     |           |
|   | being delivered to the dispensing equipment.         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1449                          |           |
|   |                                                      |           |
|   | 132\. Check at the aircraft, that oxygen pressure    |           |
|   | tanks, and lines between tanks and the shutoff       |           |
|   | means, are protected from unsafe temperatures; and   |           |
|   | located where the probability and hazards of rupture |           |
|   | in a crash landing are minimized.                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1453(a); 25.1453(b)           |           |
|   |                                                      |           |
|   | 133\. Check at the aircraft, that each projecting    |           |
|   | object that would injure persons seated or moving    |           |
|   | about the airplane in normal flight must be padded.  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.785(k)                        |           |
|   |                                                      |           |
|   | 134\. Check at an aircraft that operates on a flight |           |
|   | on which smoking is prohibited that there is at      |           |
|   | least one placard so stating that is legible to each |           |
|   | person seated in the cabin.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.791(a)                        |           |
|   |                                                      |           |
|   | 135\. Check at an aircraft that operates on a flight |           |
|   | on which smoking is to be allowed, and if the crew   |           |
|   | compartment is separated from the passenger          |           |
|   | compartment, that there was at least one sign,       |           |
|   | operable by a member of the flightcrew, legible      |           |
|   | under all probable conditions of cabin illumination  |           |
|   | to each person seated in the cabin, notifying when   |           |
|   | smoking is prohibited.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.791(a)                        |           |
|   |                                                      |           |
|   | 136\. Check at the aircraft, that there is a         |           |
|   | placard, located on or adjacent to the door of each  |           |
|   | receptacle used for the disposal of flammable waste  |           |
|   | materials, to indicate that use of the receptacle    |           |
|   | for disposal of cigarettes, etc., is prohibited.     |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.791(c)                        |           |
|   |                                                      |           |
|   | 137\. Check at the aircraft, that lavatories have    |           |
|   | \"No Smoking\" or \"No Smoking in Lavatory\"         |           |
|   | placards conspicuously located on or adjacent to     |           |
|   | each side of the entry door.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.791(d)                        |           |
|   |                                                      |           |
|   | 138\. Check at an aircraft that operates with a      |           |
|   | maximum passenger-seating configuration of more than |           |
|   | 20 seats, that the emergency exit configuration was  |           |
|   | designed so that neither crewmembers nor passengers  |           |
|   | require use of the flightdeck door in order to reach |           |
|   | the emergency exits provided for them.               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.772(a)                        |           |
|   |                                                      |           |
|   | 139\. Check at the aircraft, that a means is         |           |
|   | provided to enable flight crewmembers to directly    |           |
|   | enter the passenger compartment from the pilot       |           |
|   | compartment if the cockpit door becomes jammed.      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.772(b)                        |           |
|   |                                                      |           |
|   | 140\. Check at the aircraft, that there is an        |           |
|   | emergency means to enable a flight attendant to      |           |
|   | enter the pilot compartment in the event that the    |           |
|   | flightcrew becomes incapacitated.                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.772(c)                        |           |
|   |                                                      |           |
|   | 141\. Check at the aircraft, that each item of       |           |
|   | installed equipment is labeled as to its             |           |
|   | identification, function, or operating limitations,  |           |
|   | or any applicable combination of these factors.      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1301(b)                       |           |
|   |                                                      |           |
|   | 142\. Check at the aircraft, that each baggage and   |           |
|   | cargo compartment, except underseat compartments     |           |
|   | designed for the storage of carry-on articles        |           |
|   | weighing not more than 20 pounds, and each ballast   |           |
|   | location must have a placard stating any limitations |           |
|   | on contents, including weight, that are necessary    |           |
|   | under the loading requirements.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1557(a)                       |           |
|   |                                                      |           |
|   | 143\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed prior |           |
|   | to May 1, 1972, that the airplane is equipped with   |           |
|   | exterior lighting that is operable manually from a   |           |
|   | point in the passenger compartment that is readily   |           |
|   | accessible to a normal flight attendant seat.        |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367; 25.812(f)(1)   |           |
|   |                                                      |           |
|   | 144\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed prior |           |
|   | to May 1, 1972, the aircraft is equipped with        |           |
|   | exterior lighting that is a flight crew warning      |           |
|   | light, which illuminates when power is on in the     |           |
|   | airplane and the emergency lighting control device   |           |
|   | is not armed.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367; 25.812(f)(2)   |           |
|   |                                                      |           |
|   | 145\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed prior |           |
|   | to May 1, 1972, that the aircraft is equipped with   |           |
|   | exterior emergency lighting at each overwing         |           |
|   | emergency exit the illumination with not less than   |           |
|   | 0.03 foot-candle (measured normal to the direction   |           |
|   | of the incident light) on a 2-square-foot area where |           |
|   | an evacuee is likely to make his first step outside  |           |
|   | the cabin.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367;                |           |
|   | 25.812(g)(1)(i)                                      |           |
|   |                                                      |           |
|   | 146\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed prior |           |
|   | to May 1, 1972, that the aircraft is equipped with   |           |
|   | exterior emergency lighting at each overwing         |           |
|   | emergency exit the illumination with not less than   |           |
|   | 0.05 foot-candle (measured normal to the direction   |           |
|   | of incident light) along the 30 percent of the       |           |
|   | slip-resistant portion of the escape route required  |           |
|   | in 25.810(c) that is farthest from the exit for the  |           |
|   | minimum required width of the escape route.          |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367;                |           |
|   | 25.812(g)(1)(ii)                                     |           |
|   |                                                      |           |
|   | 147\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed prior |           |
|   | to May 1, 1972, that each airplane is equipped with  |           |
|   | exterior emergency lighting at each overwing         |           |
|   | emergency exit the illumination with not less than   |           |
|   | 0.03 foot-candle on the ground surface with the      |           |
|   | landing gear extended (measured normal to the        |           |
|   | direction of the incident light) where an evacuee    |           |
|   | using the established escape route would normally    |           |
|   | make first contact with the ground.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367;                |           |
|   | 25.812(g)(1)(iii)                                    |           |
|   |                                                      |           |
|   | 148\. Check at a transport category aircraft,        |           |
|   | manufactured on or after November 27, 1990, with a   |           |
|   | seating capacity of more than 19 passengers, that it |           |
|   | was equipped with a public address system which is   |           |
|   | approved in accordance with 14 CFR 21.305 and is     |           |
|   | designed so that no unused, unstowed microphone will |           |
|   | render the system inoperative.                       |           |
|   |                                                      |           |
|   | *Sources:* 121.318(b); 121.318(g); 121.367;          |           |
|   | 25.1423(d)                                           |           |
|   |                                                      |           |
|   | 149\. Check at the aircraft, that the airplane       |           |
|   | contains the specified markings and placards.        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1)                    |           |
|   |                                                      |           |
|   | 150\. Check at the aircraft, that each marking and   |           |
|   | placard may not be easily erased, disfigured, or     |           |
|   | obscured.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(b)(2)                    |           |
|   |                                                      |           |
|   | 151\. Check at the aircraft, that each baggage and   |           |
|   | cargo compartment, except underseat compartments     |           |
|   | designed for the storage of carry-on articles        |           |
|   | weighing not more than 20 pounds, and each ballast   |           |
|   | location must have a placard stating any limitations |           |
|   | on contents, including weight, that are necessary    |           |
|   | under the loading requirements.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1557(a)                       |           |
|   |                                                      |           |
|   | 152\. Check at the aircraft, that where internal     |           |
|   | doors are equipped with louvers or other ventilating |           |
|   | means, there must be a means convenient to the crew  |           |
|   | for closing the flow of air through the door when    |           |
|   | necessary.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.367                                   |           |
|   |                                                      |           |
|   | 153\. Check at the aircraft, that each passenger or  |           |
|   | crew compartment is suitably ventilated. Carbon      |           |
|   | monoxide concentration may not be more than one part |           |
|   | in 20,000 parts of air, and fuel fumes may not be    |           |
|   | present.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.367                                   |           |
|   |                                                      |           |
|   | 154\. Check at an aircraft, with a passenger         |           |
|   | capacity of 20 or more, that each compartment        |           |
|   | occupied by the crew or passengers, interior ceiling |           |
|   | and wall panels, other than lighting lenses and      |           |
|   | windows meet the test requirements of parts IV and V |           |
|   | of appendix F 14 CFR Part 25, or other approved      |           |
|   | equivalent method.                                   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(d)(1)                     |           |
|   |                                                      |           |
|   | 155\. Check at the aircraft, that if smoking is to   |           |
|   | be allowed in any other compartment occupied by the  |           |
|   | crew or passengers, an adequate number of            |           |
|   | self-contained, removable ashtrays are provided for  |           |
|   | all seated occupants.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(f)                        |           |
|   |                                                      |           |
|   | 156\. Check at the aircraft, that lavatories have    |           |
|   | self-contained, removable ashtrays located           |           |
|   | conspicuously on or near the entry side of each      |           |
|   | lavatory door, except that one ashtray may serve     |           |
|   | more than one lavatory door if the ashtray can be    |           |
|   | seen readily from the cabin side of each lavatory    |           |
|   | served.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(g)                        |           |
|   |                                                      |           |
|   | 157\. Check at the aircraft, that each receptacle    |           |
|   | used for the disposal of flammable waste material    |           |
|   | was fully enclosed, constructed of at least fire     |           |
|   | resistant materials, and will contain fires likely   |           |
|   | to occur in it under normal use.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.215(e); 121.367                       |           |
|   |                                                      |           |
|   | 158\. Check at the aircraft, that for each cargo and |           |
|   | baggage compartment not occupied by crew or          |           |
|   | passengers, no compartment contains any controls,    |           |
|   | wiring, lines, equipment, or accessories whose       |           |
|   | damage or failure would affect safe operation,       |           |
|   | unless those items are protected so that they cannot |           |
|   | be damaged by the movement of cargo in the           |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 159\. Check at the aircraft, that for each cargo and |           |
|   | baggage compartment not occupied by crew or          |           |
|   | passengers, no compartment contains any controls,    |           |
|   | wiring, lines, equipment, or accessories whose       |           |
|   | damage or failure would affect safe operation,       |           |
|   | unless those items are protected so that their       |           |
|   | breakage or failure will not create a fire hazard.   |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 160\. Check that the Certificate Holder\'s           |           |
|   | inspection program and program covering other        |           |
|   | maintenance preventive maintenance and alterations   |           |
|   | ensures that for each cargo and baggage compartment  |           |
|   | not occupied by crew or passengers, there was a      |           |
|   | means to prevent cargo or baggage from interfering   |           |
|   | with the functioning of the fire protective features |           |
|   | of the compartment.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(2); 121.367                    |           |
|   |                                                      |           |
|   | 161\. Check at the aircraft, that for each cargo and |           |
|   | baggage compartment not occupied by crew or          |           |
|   | passengers, sources of heat within the compartment   |           |
|   | are shielded and insulated to prevent igniting the   |           |
|   | cargo or baggage.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(g)                        |           |
|   |                                                      |           |
|   | 162\. Check at the aircraft, that each emergency     |           |
|   | exit, including a flight crew emergency exit, is a   |           |
|   | movable door or hatch in the external walls of the   |           |
|   | fuselage, allowing unobstructed opening to the       |           |
|   | outside, capable of being opened from the inside and |           |
|   | the outside with the airplane in the normal ground   |           |
|   | attitude.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.809(a); 25.809(b)(1)          |           |
|   |                                                      |           |
|   | 163\. Check at an aircraft, with a class E cargo     |           |
|   | compartment that the required crew emergency exits   |           |
|   | are accessible under any cargo loading condition.    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.857(e)(5)                     |           |
|   |                                                      |           |
|   | 164\. Check at the aircraft, that a means is         |           |
|   | provided to prevent each item of mass (that is part  |           |
|   | of the airplane type design) in a passenger or crew  |           |
|   | compartment or galley from becoming a hazard by      |           |
|   | shifting under the appropriate maximum load factors  |           |
|   | corresponding to the specified flight and ground     |           |
|   | load conditions, and to the emergency landing        |           |
|   | conditions of 14 CFR 25.561(b).                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.789(a)                        |           |
|   |                                                      |           |
|   | 165\. Check at the aircraft, that in the event of    |           |
|   | any probable failure conditions of any system which  |           |
|   | would adversely affect the ventilating air, the      |           |
|   | ventilation system is designed to provide each       |           |
|   | occupant with an airflow containing at least 0.55    |           |
|   | pounds of fresh air per minute to enable the         |           |
|   | crewmembers to perform their duties without undue    |           |
|   | discomfort or fatigue and to provide reasonable      |           |
|   | passenger comfort.                                   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.831(a)                        |           |
|   |                                                      |           |
|   | 166\. Check at the aircraft, that a means was        |           |
|   | provided to enable the occupants of the flight crew  |           |
|   | compartment to control the temperature and quantity  |           |
|   | of ventilating air supplied to their compartment     |           |
|   | independently of the temperature and quantity of air |           |
|   | supplied to other compartments and areas.            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.831(e)(1)                     |           |
|   |                                                      |           |
|   | 167\. Check at the aircraft, that a means was        |           |
|   | provided to enable the occupants of the crewmember   |           |
|   | compartments and areas, other than the flight crew   |           |
|   | compartment, to control the temperature and quantity |           |
|   | of ventilating air supplied to their compartment     |           |
|   | independently of the temperature and quantity of air |           |
|   | supplied to other compartments and areas.            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.831(e)(2)                     |           |
|   |                                                      |           |
|   | 168\. Check at the aircraft, that each lamp is       |           |
|   | installed so as to prevent contact between lamp bulb |           |
|   | and cargo.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.787(c)                        |           |
|   |                                                      |           |
|   | 169\. Check at the aircraft, that each hand fire     |           |
|   | extinguisher for use in each Class B cargo           |           |
|   | compartment was clearly identified and clearly       |           |
|   | marked to indicate its method of operation.          |           |
|   |                                                      |           |
|   | *Sources:* 121.221(c)(2); 121.309(b)(1); 121.367     |           |
|   |                                                      |           |
|   | 170\. Check at the aircraft, that in each cargo and  |           |
|   | baggage compartment not occupied by crew or          |           |
|   | passengers, sources of heat within the compartment   |           |
|   | must be shielded and insulated to prevent igniting   |           |
|   | the cargo or baggage.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(g)                        |           |
|   |                                                      |           |
|   | 171\. Check at an aircraft that was converted from a |           |
|   | passenger to a Class E cargo compartment that an     |           |
|   | Airplane Flight Manual was furnished, containing the |           |
|   | weight distribution limitations, either in the       |           |
|   | Airplane Flight Manual or in a separate weight and   |           |
|   | balance control and loading document that is         |           |
|   | incorporated by reference in the Airplane Flight     |           |
|   | Manual, including condition of the airplane and the  |           |
|   | items included in the empty weight.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(26); 25.1581(a)(1);            |           |
|   | 25.1583(c)(1)                                        |           |
|   |                                                      |           |
|   | 172\. Check at an aircraft that was converted from a |           |
|   | passenger to a Class E cargo compartment that an     |           |
|   | Airplane Flight Manual was furnished, containing the |           |
|   | weight distribution limitations, either in the       |           |
|   | Airplane Flight Manual or in a separate weight and   |           |
|   | balance control and loading document that is         |           |
|   | incorporated by reference in the Airplane Flight     |           |
|   | Manual, including loading instructions necessary to  |           |
|   | ensure loading of the airplane within the weight and |           |
|   | center of gravity limits, and to maintain the        |           |
|   | loading within these limits in flight.               |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(26); 25.1583(c)(2)             |           |
|   |                                                      |           |
|   | 173\. Check at an aircraft that was converted from a |           |
|   | passenger to a Class E cargo compartment that an     |           |
|   | Airplane Flight Manual was furnished, containing the |           |
|   | weight distribution limitations, either in the       |           |
|   | Airplane Flight Manual or in a separate weight and   |           |
|   | balance control and loading document that is         |           |
|   | incorporated by reference in the Airplane Flight     |           |
|   | Manual including, if certification for more than one |           |
|   | center of gravity range is requested, the            |           |
|   | appropriate limitations, with regard to weight and   |           |
|   | loading procedures, for each separate center of      |           |
|   | gravity range.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(26); 25.1583(c)(3)             |           |
|   |                                                      |           |
|   | 174\. Check at an aircraft that was converted from a |           |
|   | passenger to a Class E cargo compartment that an     |           |
|   | Airplane Flight Manual was furnished, containing     |           |
|   | other information that is necessary for safe         |           |
|   | operation because of design, operating, or handling  |           |
|   | characteristics.                                     |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(26); 25.1581(a)(2)             |           |
|   |                                                      |           |
|   | 175\. Check, at the certificate holding district     |           |
|   | office, that the operator who conducts domestic,     |           |
|   | flag or commuter operations, sent a copy of the      |           |
|   | record (current list of each aircraft that it        |           |
|   | operates) and each change to the certificate-holding |           |
|   | district office in accordance with its design.       |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.685                    |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s engines and parts      | Yes       |
| . | thereof meet the requirements of the certificate     |           |
| 2 | holder\'s inspection program and the program         | No,       |
| . | covering other maintenance, preventive maintenance,  | Explain   |
|   | and alterations? **     **                           |           |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the aircraft, that engines are         |           |
|   | identified by means of a fireproof plate attached to |           |
|   | the engine marked on it by etching, stamping,        |           |
|   | engraving, or other approved method of fireproof     |           |
|   | marking, at an accessible location in such a manner  |           |
|   | that it will not likely be defaced or removed during |           |
|   | normal service or lost or destroyed in an accident,  |           |
|   | that has (3) Builder\'s serial number.               |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(a); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5); 45.13(a)(6)                |           |
|   |                                                      |           |
|   | 2\. Check, at the aircraft, that engines are         |           |
|   | identified by means of a fireproof plate attached to |           |
|   | the engine marked on it by etching, stamping,        |           |
|   | engraving, or other approved method of fireproof     |           |
|   | marking, at an accessible location in such a manner  |           |
|   | that it will not likely be defaced or removed during |           |
|   | normal service or lost or destroyed in an accident,  |           |
|   | that has (4) Type certificate number, if any.        |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(a); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5); 45.13(a)(6)                |           |
|   |                                                      |           |
|   | 3\. Check, at the aircraft, that engines are         |           |
|   | identified by means of a fireproof plate attached to |           |
|   | the engine marked on it by etching, stamping,        |           |
|   | engraving, or other approved method of fireproof     |           |
|   | marking, at an accessible location in such a manner  |           |
|   | that it will not likely be defaced or removed during |           |
|   | normal service or lost or destroyed in an accident,  |           |
|   | that has (5) Production certificate number, if any.  |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(a); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5); 45.13(a)(6)                |           |
|   |                                                      |           |
|   | 4\. Check, at the aircraft, that engines are         |           |
|   | identified by means of a fireproof plate attached to |           |
|   | the engine marked on it by etching, stamping,        |           |
|   | engraving, or other approved method of fireproof     |           |
|   | marking, at an accessible location in such a manner  |           |
|   | that it will not likely be defaced or removed during |           |
|   | normal service or lost or destroyed in an accident,  |           |
|   | that has (6) For aircraft engines, the established   |           |
|   | rating.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(a); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5); 45.13(a)(6)                |           |
|   |                                                      |           |
|   | 5\. Check, at the aircraft, that it was in           |           |
|   | compliance Stage 3 noise level requirements in       |           |
|   | accordance with the Certificate Holder\'s design.    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 91.853                           |           |
|   |                                                      |           |
|   | 6\. Check, at the aircraft engines, that no signs of |           |
|   | loose/missing equipment, improper installation,      |           |
|   | leakage or other indications of defect exist.        |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(16); 121.367; 121.369(b)       |           |
|   |                                                      |           |
|   | 7\. Check, at the aircraft APU, that no signs of     |           |
|   | loose/missing equipment, improper installation,      |           |
|   | leakage or other indications of defect exist.        |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(16); 121.367; 121.369(b)       |           |
|   |                                                      |           |
|   | 8\. Check, at the aircraft engine nacelles and APU   |           |
|   | compartments, that no signs of loose/missing         |           |
|   | equipment, corrosion and other indications of defect |           |
|   | exist.                                               |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(16); 121.367; 121.369(b)       |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s propellers and parts   | Yes       |
| . | thereof meet the requirements of the certificate     |           |
| 3 | holder\'s inspection program and the program         | No,       |
| . | covering other maintenance, preventive maintenance,  | Explain   |
|   | and alterations? **     **                           |           |
|   |                                                      | Not       |
|   | *Related Performance JTIs:*                          | A         |
|   |                                                      | pplicable |
|   | 1\. Check, at the aircraft, that propellers,         |           |
|   | propeller blades, or propeller hubs produced under   |           |
|   | the terms of a type or production certificate are    |           |
|   | identified by means of a plate, stamping, engraving, |           |
|   | etching, or other approved method of fireproof       |           |
|   | identification that is placed on it on a             |           |
|   | non-critical surface, that will not be likely to be  |           |
|   | defaced or removed during normal service or lost or  |           |
|   | destroyed in an accident that has (1)Builder\'s      |           |
|   | name.                                                |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(b); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5)                             |           |
|   |                                                      |           |
|   | 2\. Check, at the aircraft, that propellers,         |           |
|   | propeller blades, or propeller hubs produced under   |           |
|   | the terms of a type or production certificate are    |           |
|   | identified by means of a plate, stamping, engraving, |           |
|   | etching, or other approved method of fireproof       |           |
|   | identification that is placed on it on a             |           |
|   | non-critical surface, that will not be likely to be  |           |
|   | defaced or removed during normal service or lost or  |           |
|   | destroyed in an accident that has (2) Model          |           |
|   | designation.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(b); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5)                             |           |
|   |                                                      |           |
|   | 3\. Check, at the aircraft, that propellers,         |           |
|   | propeller blades, or propeller hubs produced under   |           |
|   | the terms of a type or production certificate are    |           |
|   | identified by means of a plate, stamping, engraving, |           |
|   | etching, or other approved method of fireproof       |           |
|   | identification that is placed on it on a             |           |
|   | non-critical surface, that will not be likely to be  |           |
|   | defaced or removed during normal service or lost or  |           |
|   | destroyed in an accident that has (3) Builder\'s     |           |
|   | serial number.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(b); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5)                             |           |
|   |                                                      |           |
|   | 4\. Check, at the aircraft, that propellers,         |           |
|   | propeller blades, or propeller hubs produced under   |           |
|   | the terms of a type or production certificate are    |           |
|   | identified by means of a plate, stamping, engraving, |           |
|   | etching, or other approved method of fireproof       |           |
|   | identification that is placed on it on a             |           |
|   | non-critical surface, that will not be likely to be  |           |
|   | defaced or removed during normal service or lost or  |           |
|   | destroyed in an accident that has (4) Type           |           |
|   | certificate number, if any.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(b); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5)                             |           |
|   |                                                      |           |
|   | 5\. Check, at the aircraft, that propellers,         |           |
|   | propeller blades, or propeller hubs produced under   |           |
|   | the terms of a type or production certificate are    |           |
|   | identified by means of a plate, stamping, engraving, |           |
|   | etching, or other approved method of fireproof       |           |
|   | identification that is placed on it on a             |           |
|   | non-critical surface, that will not be likely to be  |           |
|   | defaced or removed during normal service or lost or  |           |
|   | destroyed in an accident that has (5) Production     |           |
|   | certificate number, if any.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(b); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5)                             |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s appliances and parts   | Yes       |
| . | thereof meet the requirements of the certificate     |           |
| 4 | holder\'s inspection program and the program         | No,       |
| . | covering other maintenance, preventive maintenance,  | Explain   |
|   | and alterations? **     **                           |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s emergency equipment    | Yes       |
| . | and parts thereof meet the requirements of the       |           |
| 5 | certificate holder\'s inspection program and the     | No,       |
| . | program covering other maintenance, preventive       | Explain   |
|   | maintenance, and alterations? **     **              |           |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the technical publications library,    |           |
|   | that the Certificate Holder\'s manual, who was       |           |
|   | required by 121.391 to provide flight attendants,    |           |
|   | contains the location of any items of equipment      |           |
|   | which vary from one aircraft to another and that the |           |
|   | N-numbers are provided for that specific equipment.  |           |
|   |                                                      |           |
|   | *Sources:* FAA Order 8900.1, Vol 03, Ch 032, Sec     |           |
|   | 013, Para 3-3426B, Fig 3-124.                        |           |
|   |                                                      |           |
|   | 2\. Check, at the aircraft, that each item of        |           |
|   | emergency and flotation equipment was inspected      |           |
|   | regularly in accordance with inspection periods      |           |
|   | established in the operations specifications.        |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.367                    |           |
|   |                                                      |           |
|   | 3\. Check, at the aircraft, that each item of        |           |
|   | emergency and flotation equipment was readily        |           |
|   | accessible to the crew.                              |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(2); 121.367                    |           |
|   |                                                      |           |
|   | 4\. Check, at the aircraft, that each item of        |           |
|   | emergency and flotation equipment was clearly        |           |
|   | identified.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.367                    |           |
|   |                                                      |           |
|   | 5\. Check, at the aircraft, that each item of        |           |
|   | emergency and flotation equipment was clearly marked |           |
|   | to indicate its method of operation.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.367                    |           |
|   |                                                      |           |
|   | 6\. Check, at the aircraft that carries emergency    |           |
|   | and flotation equipment in a compartment or          |           |
|   | container, that the compartment or container was     |           |
|   | marked as to contents.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 7\. Check, at the aircraft that carries emergency    |           |
|   | and flotation equipment in a compartment or          |           |
|   | container, that the compartment or container was     |           |
|   | marked as to date of last inspection.                |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 8\. Check, at the aircraft, that at least one hand   |           |
|   | fire extinguisher of an approved type, containing    |           |
|   | the type and quantity of extinguishing agent         |           |
|   | suitable for the kinds of fires likely to occur in   |           |
|   | the compartment, was conveniently located on the     |           |
|   | flight deck for use by the flightcrew.               |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(1); 121.309(c)(4); 121.367     |           |
|   |                                                      |           |
|   | 9\. Check, at the aircraft, it was furnished with    |           |
|   | protective breathing equipment that will protect the |           |
|   | flightcrew from the effects of smoke, carbon dioxide |           |
|   | or other harmful gases or an oxygen deficient        |           |
|   | environment caused by other than an airplane         |           |
|   | depressurization.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.337(a); 121.337(b)(1); 121.367        |           |
|   |                                                      |           |
|   | 10\. Check, at the aircraft, that protective         |           |
|   | breathing equipment was easily accessible and        |           |
|   | conveniently located on the flight deck for          |           |
|   | immediate use by crewmembers in combating fires.     |           |
|   |                                                      |           |
|   | *Sources:* 121.337(a); 121.337(b)(9)(ii); 121.367    |           |
|   |                                                      |           |
|   | 11\. Check, at the aircraft, that protective         |           |
|   | breathing equipment was inspected regularly in       |           |
|   | accordance with inspection guidelines and the        |           |
|   | inspection periods established by the equipment      |           |
|   | manufacturer.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.337(a); 121.337(b)(2); 121.367        |           |
|   |                                                      |           |
|   | 12\. Check, at the turbine engine powered airplane,  |           |
|   | that operates at flight altitudes above flight level |           |
|   | 250, that it has an oxygen mask, so designed that it |           |
|   | can be rapidly placed on his face from its ready     |           |
|   | position, properly secured, sealed, and supplying    |           |
|   | oxygen upon demand for each flight crewmember on     |           |
|   | flight deck duty.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.333(a); 121.333(c)(1); 121.367        |           |
|   |                                                      |           |
|   | 13\. Check, at the turbine engine powered airplane,  |           |
|   | that operates at flight altitudes above flight level |           |
|   | 250, that it has an oxygen mask, so designed that    |           |
|   | after being placed on the face it does not prevent   |           |
|   | immediate communication between the flight           |           |
|   | crewmember and other crewmembers over the airplane   |           |
|   | intercommunication system for each flight crewmember |           |
|   | on flight deck duty.                                 |           |
|   |                                                      |           |
|   | *Sources:* 121.333(a); 121.333(c)(1); 121.367        |           |
|   |                                                      |           |
|   | 14\. Check, at the transport category airplane that  |           |
|   | was type certificated after January 1, 1958, that it |           |
|   | was equipped at each flight deck station with a      |           |
|   | combined safety belt and shoulder harness consisting |           |
|   | of a combined safety belt and shoulder harness with  |           |
|   | a single-point release that permits the flight deck  |           |
|   | occupant, when seated with the restraint system      |           |
|   | fastened, to perform all of the occupant\'s          |           |
|   | necessary flight deck functions.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.311(f); 121.367; 25.785(g)            |           |
|   |                                                      |           |
|   | 15\. Check, at the transport category airplane that  |           |
|   | was type certificated after January 1, 1958, that    |           |
|   | each safety belt and shoulder harness on the flight  |           |
|   | deck has a means to secure each combined restraint   |           |
|   | system when not in use to prevent interference with  |           |
|   | the operation of the airplane and with rapid egress  |           |
|   | in an emergency.                                     |           |
|   |                                                      |           |
|   | *Sources:* 121.311(f); 121.367; 25.785(g)            |           |
|   |                                                      |           |
|   | 16\. Check, at the aircraft, that it has an approved |           |
|   | cockpit check procedure for each type of aircraft,   |           |
|   | designed so that a flight crewmember will not need   |           |
|   | to rely upon his memory for items to be checked,     |           |
|   | that includes each item necessary for flight         |           |
|   | crewmembers to check for safety before starting      |           |
|   | engines, taking off, or landing, and in engine and   |           |
|   | systems emergencies in accordance with the           |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.315(a); 121.315(b)     |           |
|   |                                                      |           |
|   | 17\. Check, at the aircraft, that it has an approved |           |
|   | cockpit check procedure for each type of aircraft,   |           |
|   | that was readily usable in the cockpit of each       |           |
|   | aircraft and the flight crew shall follow them when  |           |
|   | operating the aircraft in accordance with the        |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.315(a); 121.315(c)     |           |
|   |                                                      |           |
|   | 18\. Check at the aircraft, that each item of        |           |
|   | emergency equipment was inspected regularly, in      |           |
|   | accordance with inspection periods established in    |           |
|   | the operations specifications, to ensure its         |           |
|   | condition for continued serviceability and immediate |           |
|   | readiness to perform its intended emergency          |           |
|   | purposes.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.367                    |           |
|   |                                                      |           |
|   | 19\. Check at the aircraft, that each item of        |           |
|   | flotation equipment was inspected regularly in       |           |
|   | accordance with inspection periods established in    |           |
|   | the operations specifications to ensure its          |           |
|   | condition for continued serviceability and immediate |           |
|   | readiness to perform its intended emergency          |           |
|   | purposes.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.367                    |           |
|   |                                                      |           |
|   | 20\. Check at the aircraft, that each item of        |           |
|   | emergency equipment was readily accessible to the    |           |
|   | crew and, with regard to equipment located in the    |           |
|   | passenger compartment, to passengers.                |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(2); 121.367                    |           |
|   |                                                      |           |
|   | 21\. Check at the aircraft, that each item of        |           |
|   | flotation equipment was readily accessible to the    |           |
|   | crew and, with regard to equipment located in the    |           |
|   | passenger compartment, to passengers.                |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(2); 121.367                    |           |
|   |                                                      |           |
|   | 22\. Check at the aircraft, that each item of        |           |
|   | emergency equipment was clearly identified and       |           |
|   | clearly marked to indicate its method of operation.  |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.367                    |           |
|   |                                                      |           |
|   | 23\. Check at the aircraft, that each item of        |           |
|   | flotation equipment was clearly identified and       |           |
|   | clearly marked to indicate its method of operation.  |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.367                    |           |
|   |                                                      |           |
|   | 24\. Check at the aircraft, that each item of        |           |
|   | emergency equipment, when carried in a compartment   |           |
|   | or container, was carried in a compartment or        |           |
|   | container marked as to contents.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 25\. Check at the aircraft, that each item of        |           |
|   | emergency equipment, when carried in a compartment   |           |
|   | or container, the compartment or container, or the   |           |
|   | item itself, was marked as to date of last           |           |
|   | inspection.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 26\. Check at the aircraft, that each item of        |           |
|   | flotation equipment, when carried in a compartment   |           |
|   | or container, was carried in a compartment or        |           |
|   | container marked as to contents.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 27\. Check at the aircraft, that each item of        |           |
|   | emergency equipment, when carried in a compartment   |           |
|   | or container, the compartment or container, or the   |           |
|   | item itself, was marked as to date of last           |           |
|   | inspection.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 28\. Check at the aircraft, that hand fire           |           |
|   | extinguishers of an approved type, designed to       |           |
|   | minimize the hazard of toxic gas concentrations, are |           |
|   | provided for use in passenger compartments, with the |           |
|   | type and quantity of extinguishing agent suitable    |           |
|   | for the kinds of fires likely to occur in the        |           |
|   | compartment where the extinguisher was intended to   |           |
|   | be used.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(1); 121.367                    |           |
|   |                                                      |           |
|   | 29\. Check at an aircraft, with passenger seats      |           |
|   | accommodating more than 6 but fewer than 31          |           |
|   | passengers, that at least one hand fire extinguisher |           |
|   | is conveniently located in passenger compartment.    |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(5)(i); 121.367                 |           |
|   |                                                      |           |
|   | 30\. Check at an aircraft, with passenger seats      |           |
|   | accommodating more than 30 but fewer than 61         |           |
|   | passengers, that at least two hand fire              |           |
|   | extinguishers that are conveniently located and      |           |
|   | uniformly distributed throughout each compartment.   |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(5)(ii); 121.367                |           |
|   |                                                      |           |
|   | 31\. Check at an aircraft, with passenger seats      |           |
|   | accommodating 61 through 200 passengers, that at     |           |
|   | least three hand fire extinguishers that are         |           |
|   | conveniently located and uniformly distributed       |           |
|   | throughout each compartment.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(5)(iii); 121.367               |           |
|   |                                                      |           |
|   | 32\. Check at an aircraft, with passenger seats      |           |
|   | accommodating 201 through 300 passengers, that at    |           |
|   | least four hand fire extinguishers that are          |           |
|   | conveniently located and uniformly distributed       |           |
|   | throughout each compartment.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(5)(iii); 121.367               |           |
|   |                                                      |           |
|   | 33\. Check at an aircraft, with passenger seats      |           |
|   | accommodating 301 through 400 passengers, that at    |           |
|   | least five hand fire extinguishers that are          |           |
|   | conveniently located and uniformly distributed       |           |
|   | throughout each compartment.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(5)(iii); 121.367               |           |
|   |                                                      |           |
|   | 34\. Check at an aircraft, with passenger seats      |           |
|   | accommodating 401 through 500 passengers, that at    |           |
|   | least six hand fire extinguishers that are           |           |
|   | conveniently located and uniformly distributed       |           |
|   | throughout each compartment.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(5)(iii); 121.367               |           |
|   |                                                      |           |
|   | 35\. Check at an aircraft, with passenger seats      |           |
|   | accommodating 501 through 600 passengers, that at    |           |
|   | least seven hand fire extinguishers that are         |           |
|   | conveniently located and uniformly distributed       |           |
|   | throughout each compartment.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(5)(iii); 121.367               |           |
|   |                                                      |           |
|   | 36\. Check at an aircraft, with passenger seats      |           |
|   | accommodating 601 or more passengers, that at least  |           |
|   | eight hand fire extinguishers that are conveniently  |           |
|   | located and uniformly distributed throughout each    |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(5)(iii); 121.367               |           |
|   |                                                      |           |
|   | 37\. Check at the aircraft, that at least two of the |           |
|   | required hand fire extinguisher installed in         |           |
|   | passenger-carrying airplanes contain Halon 1211      |           |
|   | (bromochlorofluoromethane) or equivalent as the      |           |
|   | extinguishing agent.                                 |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(7); 121.367                    |           |
|   |                                                      |           |
|   | 38\. Check at the aircraft, that at least one hand   |           |
|   | fire extinguisher in the passenger compartment       |           |
|   | contains Halon 1211 or equivalent.                   |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(7); 121.367                    |           |
|   |                                                      |           |
|   | 39\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher was clearly identified and clearly      |           |
|   | marked to indicate its method of operation.          |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.309(c)(7); 121.367     |           |
|   |                                                      |           |
|   | 40\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher when carried in a compartment or        |           |
|   | container, the compartment or container, was marked  |           |
|   | as to contents.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(c)(7); 121.367     |           |
|   |                                                      |           |
|   | 41\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher when carried in a compartment or        |           |
|   | container, the compartment or container or the fire  |           |
|   | extinguisher itself was marked as to date of last    |           |
|   | inspection.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(c)(7); 121.367     |           |
|   |                                                      |           |
|   | 42\. Check at an aircraft, with a class E cargo      |           |
|   | compartment, that at least one hand fire             |           |
|   | extinguisher, of an approved type, with the type and |           |
|   | quantity of extinguishing agent suitable for the     |           |
|   | kinds of fires likely to occur in the compartment is |           |
|   | conveniently located and accessible to crewmembers   |           |
|   | during flight for use in each class E compartment.   |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(1); 121.309(c)(2); 121.367     |           |
|   |                                                      |           |
|   | 43\. Check at an aircraft, with a class E cargo      |           |
|   | compartment, that each hand fire extinguisher, for   |           |
|   | use in each class E cargo compartment, was clearly   |           |
|   | identified and clearly marked to indicate its method |           |
|   | of operation.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.309(c)(2); 121.367     |           |
|   |                                                      |           |
|   | 44\. Check at an aircraft, with a class E cargo      |           |
|   | compartment, that each hand fire extinguisher for    |           |
|   | use in each class E cargo compartment, when carried  |           |
|   | in a compartment or container, was carried in a      |           |
|   | compartment or container marked as to contents.      |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(c)(2); 121.367     |           |
|   |                                                      |           |
|   | 45\. Check at an aircraft, with a class E cargo      |           |
|   | compartment, that each hand fire extinguisher for    |           |
|   | use in each class E cargo compartment, when carried  |           |
|   | in a compartment or container, the compartment or    |           |
|   | container, or the fire extinguisher itself, was      |           |
|   | marked as to date of last inspection.                |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(c)(2); 121.367     |           |
|   |                                                      |           |
|   | 46\. Check at the aircraft, that at least one hand   |           |
|   | fire extinguisher, of an approved type, with the     |           |
|   | type and quantity of extinguishing agent suitable    |           |
|   | for the kinds of fires likely to occur, was          |           |
|   | conveniently located for use in each galley, located |           |
|   | in a compartment other than a passenger, cargo, or   |           |
|   | crew compartment.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(1); 121.309(c)(3); 121.367     |           |
|   |                                                      |           |
|   | 47\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher for use in each galley located in a     |           |
|   | compartment other than a passenger, cargo, or crew   |           |
|   | compartment, was clearly identified and clearly      |           |
|   | marked to indicate its method of operation.          |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.309(c)(3); 121.367     |           |
|   |                                                      |           |
|   | 48\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher, for use in each galley located in a    |           |
|   | compartment other than a passenger, cargo, or crew   |           |
|   | compartment, when carried in a compartment or        |           |
|   | container, the compartment or container was marked   |           |
|   | as to contents.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(c)(3); 121.367     |           |
|   |                                                      |           |
|   | 49\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher, for use in each galley located in a    |           |
|   | compartment other than a passenger, cargo, or crew   |           |
|   | compartment, when carried in a compartment or        |           |
|   | container, compartment or container, or the fire     |           |
|   | extinguisher itself, was marked as to date of last   |           |
|   | inspection.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(c)(3); 121.367     |           |
|   |                                                      |           |
|   | 50\. Check at the aircraft, that, for those cases    |           |
|   | where a galley was located in a passenger            |           |
|   | compartment, at least one hand fire extinguisher, of |           |
|   | an approved type, with the type and quantity of      |           |
|   | extinguishing agent suitable for the kinds of fires  |           |
|   | likely to occur, designed to minimize the hazard of  |           |
|   | toxic gas concentrations, was conveniently located   |           |
|   | and easily accessible for use in the galley.         |           |
|   |                                                      |           |
|   | *Sources:* 121.309(c)(1); 121.309(c)(6); 121.367     |           |
|   |                                                      |           |
|   | 51\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher for use in each galley that was located |           |
|   | in a passenger compartment was clearly identified    |           |
|   | and clearly marked to indicate its method of         |           |
|   | operation.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.309(c)(6); 121.367     |           |
|   |                                                      |           |
|   | 52\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher, for use in each galley that was        |           |
|   | located in a passenger compartment, when carried in  |           |
|   | a compartment or container, the compartment or       |           |
|   | container was marked as to contents.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(c)(6); 121.367     |           |
|   |                                                      |           |
|   | 53\. Check at the aircraft, that each hand fire      |           |
|   | extinguisher, for use in each galley that was        |           |
|   | located in a passenger compartment, when carried in  |           |
|   | a compartment or container, the compartment or       |           |
|   | container, or the fire extinguisher itself, was      |           |
|   | marked as to date of last inspection.                |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(c)(6); 121.367     |           |
|   |                                                      |           |
|   | 54\. Check at an aircraft, with up to 50 passenger   |           |
|   | seats, that the aircraft has at least 1 approved     |           |
|   | first-aid kit.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121 App..A; 121.309(d)(1)(i); 121.367     |           |
|   |                                                      |           |
|   | 55\. Check at an aircraft with 51 to 150 passenger   |           |
|   | seats, that the aircraft has at least 2 approved     |           |
|   | first-aid kits, distributed as evenly as practicable |           |
|   | throughout the aircraft, readily accessible to the   |           |
|   | cabin flight attendants.                             |           |
|   |                                                      |           |
|   | *Sources:* 121 App..A; 121 App..A; 121.309(d)(1)(i); |           |
|   | 121.367                                              |           |
|   |                                                      |           |
|   | 56\. Check at an aircraft with 151 to 250 passenger  |           |
|   | seats, that the aircraft has at least 3 approved     |           |
|   | first-aid kits, distributed as evenly as practicable |           |
|   | throughout the aircraft, readily accessible to the   |           |
|   | cabin flight attendants.                             |           |
|   |                                                      |           |
|   | *Sources:* 121 App..A; 121 App..A; 121.309(d)(1)(i); |           |
|   | 121.367                                              |           |
|   |                                                      |           |
|   | 57\. Check at an aircraft with more than 250         |           |
|   | passenger seats, that the aircraft has at least 4    |           |
|   | approved first-aid kits, distributed as evenly as    |           |
|   | practicable throughout the aircraft, readily         |           |
|   | accessible to the cabin flight attendants.           |           |
|   |                                                      |           |
|   | *Sources:* 121 App..A; 121 App..A; 121.309(d)(1)(i); |           |
|   | 121.367                                              |           |
|   |                                                      |           |
|   | 58\. Check at the aircraft that each first-aid kit   |           |
|   | was clearly identified.                              |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.309(d)(1)(i); 121.367  |           |
|   |                                                      |           |
|   | 59\. Check at the aircraft that each first-aid kit,  |           |
|   | when carried in a compartment or container, the      |           |
|   | compartment or container was marked as to contents.  |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(d)(1)(i); 121.367  |           |
|   |                                                      |           |
|   | 60\. Check at the aircraft that each first-aid kit,  |           |
|   | when carried in a compartment or container, the      |           |
|   | compartment or container was marked as to date of    |           |
|   | last inspection.                                     |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(d)(1)(i); 121.367  |           |
|   |                                                      |           |
|   | 61\. Check at the aircraft, which requires a flight  |           |
|   | attendant, that each airplane was equipped with an   |           |
|   | emergency medical kit.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.309(d)(1)(ii); 121.367                |           |
|   |                                                      |           |
|   | 62\. Check at the aircraft, that each emergency      |           |
|   | medical kit was clearly identified.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.309(d)(1)(ii); 121.367 |           |
|   |                                                      |           |
|   | 63\. Check at the aircraft, that each emergency      |           |
|   | medical kit, when carried in a compartment or        |           |
|   | container, was carried in a compartment or container |           |
|   | that was marked as to contents.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(d)(1)(ii); 121.367 |           |
|   |                                                      |           |
|   | 64\. Check at the aircraft, that each emergency      |           |
|   | medical kit, when carried in a compartment or        |           |
|   | container, was carried in a compartment or container |           |
|   | that was marked as to date of last inspection.       |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(d)(1)(ii); 121.367 |           |
|   |                                                      |           |
|   | 65\. Check at the aircraft, that pairs of protective |           |
|   | latex gloves, or equivalent nonpermeable gloves,     |           |
|   | equal in number to the number of first aid kits on   |           |
|   | board the aircraft are distributed as evenly as      |           |
|   | practicable throughout the cabin of the aircraft.    |           |
|   |                                                      |           |
|   | *Sources:* 121.309(d)(2); 121.367                    |           |
|   |                                                      |           |
|   | 66\. Check at an aircraft with a service compartment |           |
|   | located below the main deck, which may be occupied   |           |
|   | during taxi or flight but not during takeoff or      |           |
|   | landing, that each powered lift system installed     |           |
|   | between a lower deck service compartment and the     |           |
|   | main deck for the carriage of persons or equipment,  |           |
|   | or both, has a hatch capable of being used for       |           |
|   | evacuating persons from the lift that was operable   |           |
|   | from inside and outside the lift without tools, with |           |
|   | the lift in any position.                            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.819(g)(3)                     |           |
|   |                                                      |           |
|   | 67\. Check at an aircraft with an emergency exit     |           |
|   | (other than over-the-wing) that was more than 6 feet |           |
|   | from the ground, with the airplane on the ground and |           |
|   | the landing gear extended, that there was an         |           |
|   | approved means to assist the occupants in descending |           |
|   | to the ground.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.310(a); 121.367                       |           |
|   |                                                      |           |
|   | 68\. Check at the aircraft, that each approved means |           |
|   | to assist the occupants in descending to the ground  |           |
|   | was inspected regularly in accordance with           |           |
|   | inspection periods established in the operations     |           |
|   | specifications to ensure its condition for continued |           |
|   | serviceability and immediate readiness to perform    |           |
|   | its intended emergency purposes.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.310(a); 121.367        |           |
|   |                                                      |           |
|   | 69\. Check at the aircraft, that each approved means |           |
|   | to assist the occupants in descending to the ground  |           |
|   | was clearly identified and clearly marked to         |           |
|   | indicate its method of operation.                    |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.310(a); 121.367        |           |
|   |                                                      |           |
|   | 70\. Check at the aircraft, that each approved means |           |
|   | to assist the occupants in descending to the ground, |           |
|   | when carried in a compartment or container, the      |           |
|   | compartment or container was marked as to contents.  |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.310(a); 121.367        |           |
|   |                                                      |           |
|   | 71\. Check at the aircraft, that each approved means |           |
|   | used to assist the occupants in descending to the    |           |
|   | ground, when carried in a compartment or container,  |           |
|   | the compartment or container or the item itself, was |           |
|   | marked as to date of last inspection.                |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.310(a); 121.367        |           |
|   |                                                      |           |
|   | 72\. Check at the aircraft, that the location of     |           |
|   | each passenger emergency exit was indicated by a     |           |
|   | passenger emergency exit locator sign above the      |           |
|   | aisle (or aisles) near each passenger emergency      |           |
|   | exit, or at another overhead location if it was more |           |
|   | practical because of low headroom.                   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.811(d)(1)                     |           |
|   |                                                      |           |
|   | 73\. Check at the aircraft, that the location of     |           |
|   | each passenger emergency exit marking sign was next  |           |
|   | to each passenger emergency exit, except that one    |           |
|   | sign may serve two such exits if they both can be    |           |
|   | seen readily.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.811(d)(2)                     |           |
|   |                                                      |           |
|   | 74\. Check at the aircraft, that each passenger      |           |
|   | emergency exit, its means of access, and its means   |           |
|   | of opening are conspicuously marked.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.310(b)(1); 121.367                    |           |
|   |                                                      |           |
|   | 75\. Check at the aircraft, that the identity and    |           |
|   | location of each passenger emergency exit was        |           |
|   | recognizable from a distance equal to the width of   |           |
|   | the cabin.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.310(b)(1); 121.367                    |           |
|   |                                                      |           |
|   | 76\. Check at the aircraft, that a sign visible to   |           |
|   | occupants approaching along the main passenger aisle |           |
|   | indicates the location of each passenger emergency   |           |
|   | exit.                                                |           |
|   |                                                      |           |
|   | *Sources:* 121.310(b)(1); 121.367                    |           |
|   |                                                      |           |
|   | 77\. Check at the aircraft, that there was a         |           |
|   | locating sign above the aisle near each              |           |
|   | over-the-wing passenger emergency exit, or at        |           |
|   | another ceiling location if it was more practical    |           |
|   | because of low headroom.                             |           |
|   |                                                      |           |
|   | *Sources:* 121.310(b)(1)(i); 121.367                 |           |
|   |                                                      |           |
|   | 78\. Check at the aircraft, that on each bulkhead or |           |
|   | divider that prevents fore and aft vision along the  |           |
|   | passenger cabin, there was a sign to indicate        |           |
|   | emergency exits beyond and obscured by the bulkhead  |           |
|   | or divider, except that if this was not possible the |           |
|   | sign may be placed at another appropriate location.  |           |
|   |                                                      |           |
|   | *Sources:* 121.310(b)(1)(iii); 121.367               |           |
|   |                                                      |           |
|   | 79\. Check at an aircraft, with a passenger seating  |           |
|   | configuration, excluding pilot seats, of 10 seats or |           |
|   | more, that each passenger emergency exit locator     |           |
|   | sign required by Sec. 25.811(d)(1) and each          |           |
|   | passenger emergency exit marking sign required by    |           |
|   | Sec. 25.811(d)(2) was internally electrically        |           |
|   | illuminated and has red letters at least 1 inches    |           |
|   | high on an illuminated white background, and has an  |           |
|   | area of at least 21 square inches excluding the      |           |
|   | letters.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.812(b)(1)(i)                  |           |
|   |                                                      |           |
|   | 80\. Check at an aircraft, with a passenger seating  |           |
|   | configuration, excluding pilot seats, of 10 seats or |           |
|   | more, that each passenger emergency exit locator     |           |
|   | sign on each bulkhead or divider, that prevents fore |           |
|   | and aft vision along the passenger cabin to indicate |           |
|   | emergency exits beyond and obscured by the bulkhead  |           |
|   | or divider, is internally electrically illuminated   |           |
|   | or self-illuminated by other than electrical means.  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.811(d)(3); 25.812(b)(1)(ii)   |           |
|   |                                                      |           |
|   | 81\. Check at an aircraft, with a passenger seating  |           |
|   | configuration, excluding pilot seats, of 10 seats or |           |
|   | more, that each passenger emergency exit locator     |           |
|   | sign on each bulkhead or divider, that prevents fore |           |
|   | and aft vision along the passenger cabin to indicate |           |
|   | emergency exits beyond and obscured by the bulkhead  |           |
|   | or divider, has red letters at least 1 inches high   |           |
|   | on a white background having an area of at least 21  |           |
|   | square inches excluding the letters.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.811(d)(3); 25.812(b)(1)(ii)   |           |
|   |                                                      |           |
|   | 82\. Check at a transport category airplane with a   |           |
|   | type certificate that was filed on or after May 1,   |           |
|   | 1972, that each passenger emergency exit marking and |           |
|   | each locating sign was manufactured to meet the      |           |
|   | interior emergency exit marking requirements under   |           |
|   | which the airplane was type certificated.            |           |
|   |                                                      |           |
|   | *Sources:* 121.310(b)(2)(ii); 121.367                |           |
|   |                                                      |           |
|   | 83\. Check at a nontransport category turbopropeller |           |
|   | powered airplane that was type certificated after    |           |
|   | December 31, 1964, that each passenger emergency     |           |
|   | exit marking was manufactured to meet the            |           |
|   | requirements of Sec. 23.811(b).                      |           |
|   |                                                      |           |
|   | *Sources:* 121.310(b)(2)(iii); 121.367               |           |
|   |                                                      |           |
|   | 84\. Check at an aircraft with Type III exits,       |           |
|   | regardless of passenger capacity of the airplane in  |           |
|   | which it was installed, that for each Type III exit  |           |
|   | that there are placards that accurately state or     |           |
|   | illustrate the proper method of opening the exit,    |           |
|   | including the use of handholds.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.813(c)(3)(ii)                 |           |
|   |                                                      |           |
|   | 85\. Check at an aircraft with Type III exits,       |           |
|   | regardless of passenger capacity of the airplane in  |           |
|   | which it was installed, that for each Type III exit  |           |
|   | if the exit was a removable hatch, there are         |           |
|   | placards that state the weight of the hatch and      |           |
|   | indicate an appropriate location to place the hatch  |           |
|   | after removal.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.813(c)(3)(iii)                |           |
|   |                                                      |           |
|   | 86\. Check at a passenger carrying aircraft for      |           |
|   | which the application for the type certificate was   |           |
|   | filed prior to May 1, 1972 that the location of each |           |
|   | passenger emergency exit operating handle, and       |           |
|   | instructions for opening the exit, are shown by a    |           |
|   | marking on or near the exit that was readable from a |           |
|   | distance of 30 inches.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.310(e)(1); 121.367                    |           |
|   |                                                      |           |
|   | 87\. Check at a passenger carrying aircraft for      |           |
|   | which the application for the type certificate was   |           |
|   | filed prior to May 1, 1972, that for each Type I and |           |
|   | Type II emergency exit with a locking mechanism      |           |
|   | released by rotary motion of the handle, the         |           |
|   | instructions for opening was shown by a red arrow    |           |
|   | with a shaft at least three-fourths inch wide and a  |           |
|   | head twice the width of the shaft, extending along   |           |
|   | at least 70 of arc at a radius approximately equal   |           |
|   | to three-fourths of the handle length.               |           |
|   |                                                      |           |
|   | *Sources:* 121.310(e)(1)(i); 121.367                 |           |
|   |                                                      |           |
|   | 88\. Check at a passenger carrying aircraft for      |           |
|   | which the application for the type certificate was   |           |
|   | filed prior to May 1, 1972, that for each Type I and |           |
|   | Type II emergency exit with a locking mechanism      |           |
|   | released by rotary motion of the handle, the         |           |
|   | instructions for opening was shown by the word       |           |
|   | \"open\" in red letters 1 inch high placed           |           |
|   | horizontally near the head of the arrow.             |           |
|   |                                                      |           |
|   | *Sources:* 121.310(e)(1)(ii); 121.367                |           |
|   |                                                      |           |
|   | 89\. Check at a passenger carrying aircraft for      |           |
|   | which the application for the type certificate was   |           |
|   | filed prior to May 1, 1972, that the location of     |           |
|   | each passenger emergency exit operating handle and   |           |
|   | instructions for opening the exit are shown in       |           |
|   | accordance with the requirements under which the     |           |
|   | airplane was type certificated.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.310(e)(2); 121.367                    |           |
|   |                                                      |           |
|   | 90\. Check at a passenger carrying aircraft for      |           |
|   | which the application for the type certificate was   |           |
|   | filed prior to May 1, 1972, that no operating handle |           |
|   | or operating handle cover may continue to be used if |           |
|   | its luminescence (brightness) decreases to below 100 |           |
|   | micro lamberts.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.310(e)(2); 121.367                    |           |
|   |                                                      |           |
|   | 91\. Check at the aircraft, that the location of the |           |
|   | operating handle and instructions for opening exits  |           |
|   | from the inside of the airplane was self-illuminated |           |
|   | with an initial brightness of at least 160 micro     |           |
|   | lamberts, or was conspicuously located and well      |           |
|   | illuminated by the emergency lighting even in        |           |
|   | conditions of occupant crowding at the exit.         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.811(e); 25.811(e)(2)(i);      |           |
|   | 25.811(e)(2)(ii)                                     |           |
|   |                                                      |           |
|   | 92\. Check at a passenger carrying transport         |           |
|   | category aircraft that each passage way between      |           |
|   | individual passenger areas, or leading to a Type I   |           |
|   | or Type II emergency exit, was unobstructed and at   |           |
|   | least 20 inches wide.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.310(f)(1); 121.367                    |           |
|   |                                                      |           |
|   | 93\. Check at a passenger carrying transport         |           |
|   | category aircraft that there was enough space next   |           |
|   | to each Type I or Type II emergency exit to allow a  |           |
|   | crewmember to assist in the evacuation of passengers |           |
|   | without reducing the unobstructed width of the       |           |
|   | passageway below 20 inches.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.310(f)(1); 121.310(f)(2); 121.367     |           |
|   |                                                      |           |
|   | 94\. Check at a passenger carrying transport         |           |
|   | category aircraft that there was access from the     |           |
|   | main aisle to each Type III and Type IV exit which   |           |
|   | was not obstructed by seats, berths, or other        |           |
|   | protrusions in a manner that would reduce the        |           |
|   | effectiveness of the exit.                           |           |
|   |                                                      |           |
|   | *Sources:* 121.310(f)(3); 121.367                    |           |
|   |                                                      |           |
|   | 95\. Check at a passenger carrying transport         |           |
|   | category aircraft that for which the application for |           |
|   | the type certificate was filed prior to May 1, 1972, |           |
|   | that required emergency exit distribution was as     |           |
|   | uniform as practical, taking passenger distribution  |           |
|   | into account.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.310(f)(3)(iii); 121.367;              |           |
|   | 25.813(c)(1)(i)                                      |           |
|   |                                                      |           |
|   | 96\. Check at a passenger carrying transport         |           |
|   | category aircraft, that if it was necessary to pass  |           |
|   | through a passageway between passenger compartments  |           |
|   | to reach any required emergency exit from any seat   |           |
|   | in the passenger cabin, that the passageway was not  |           |
|   | obstructed.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.310(f)(4); 121.367                    |           |
|   |                                                      |           |
|   | 97\. Check at a passenger carrying transport         |           |
|   | category aircraft, that no door was installed in any |           |
|   | partition between passenger compartments.            |           |
|   |                                                      |           |
|   | *Sources:* 121.310(f)(5); 121.367                    |           |
|   |                                                      |           |
|   | 98\. Check at a passenger carrying transport         |           |
|   | category aircraft, that if it was necessary to pass  |           |
|   | through a doorway separating the passenger cabin     |           |
|   | from other areas to reach required emergency exit    |           |
|   | from any passenger seat, the door has a means to     |           |
|   | latch it in open position.                           |           |
|   |                                                      |           |
|   | *Sources:* 121.310(f)(6); 121.367                    |           |
|   |                                                      |           |
|   | 99\. Check at an aircraft having an emergency exit   |           |
|   | configuration installed and authorized for operation |           |
|   | prior to October 16, 1987, that was required to have |           |
|   | more than one passenger emergency exit for each side |           |
|   | of the fuselage, that no passenger emergency exit    |           |
|   | was more than 60 feet from any adjacent passenger    |           |
|   | emergency exit on the same side of the same deck of  |           |
|   | the fuselage, as measured parallel to the            |           |
|   | airplane\'s longitudinal axis between the nearest    |           |
|   | exit edges.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.310(m); 121.367                       |           |
|   |                                                      |           |
|   | 100\. Check at an aircraft that carries cargo in the |           |
|   | passenger compartment in an approved cargo bin that  |           |
|   | the bin was not installed in a position that         |           |
|   | restricts access to or use of any required emergency |           |
|   | exit, or of the aisle in the passenger compartment.  |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(5); 121.367                    |           |
|   |                                                      |           |
|   | 101\. Check at the aircraft, that each passenger     |           |
|   | ventral exit (except the ventral exits on M-404 and  |           |
|   | CV-240 airplanes) meets the requirements of 121.310  |           |
|   | for floor level emergency exits.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.310(i); 121.367                       |           |
|   |                                                      |           |
|   | 102\. Check at the aircraft, that each passenger     |           |
|   | tail cone exit meets the requirements of 121.310 for |           |
|   | floor level emergency exits.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.310(i); 121.367                       |           |
|   |                                                      |           |
|   | 103\. Check at the aircraft, that approved emergency |           |
|   | exits in the passenger compartments that are in      |           |
|   | excess of the minimum number of required emergency   |           |
|   | exits meet all of the applicable provisions of       |           |
|   | 121.310 except paragraphs (f)(1), (2), and (3) and   |           |
|   | are readily accessible.                              |           |
|   |                                                      |           |
|   | *Sources:* 121.310(j); 121.367                       |           |
|   |                                                      |           |
|   | 104\. Check at a large passenger-carrying            |           |
|   | turbojet-powered aircraft, that each ventral exit    |           |
|   | and tailcone exit was designed and constructed so    |           |
|   | that it cannot be opened during flight.              |           |
|   |                                                      |           |
|   | *Sources:* 121.310(k)(1); 121.367                    |           |
|   |                                                      |           |
|   | 105\. Check at the aircraft, that there was an       |           |
|   | approved survival type emergency locator transmitter |           |
|   | for use in one life raft.                            |           |
|   |                                                      |           |
|   | *Sources:* 121.339(a)(4); 121.367; 25.1415(d)        |           |
|   |                                                      |           |
|   | 106\. Check at an aircraft, that conducts flag or    |           |
|   | supplemental operations or a domestic operations     |           |
|   | within the State of Alaska over an uninhabited area  |           |
|   | or any other area that (in its operations            |           |
|   | specifications) the Administrator specifies required |           |
|   | equipment for search and rescue in case of an        |           |
|   | emergency, that each airplane was equipped with an   |           |
|   | approved survival type emergency locator             |           |
|   | transmitter.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.353(b); 121.367                       |           |
|   |                                                      |           |
|   | 107\. Check at an aircraft, that conducts flag or    |           |
|   | supplemental operations or a domestic operations     |           |
|   | within the State Hawaii over an uninhabited area or  |           |
|   | any other area that (in its operations               |           |
|   | specifications) the Administrator specifies required |           |
|   | equipment for search and rescue in case of an        |           |
|   | emergency, that each airplane was equipped with an   |           |
|   | approved survival type emergency locator             |           |
|   | transmitter.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.353(b); 121.367                       |           |
|   |                                                      |           |
|   | 108\. Check at an aircraft, that operates in         |           |
|   | extended overwater operations, that each approved    |           |
|   | survival type emergency locator transmitter was      |           |
|   | inspected regularly in accordance with inspection    |           |
|   | periods established in the operations specifications |           |
|   | to ensure its condition for continued serviceability |           |
|   | and immediate readiness to perform its intended      |           |
|   | emergency purposes.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.339(a)(4); 121.367     |           |
|   |                                                      |           |
|   | 109\. Check at the aircraft, which requires the      |           |
|   | survival type emergency locator transmitter, that it |           |
|   | was easily accessible in the event of a ditching     |           |
|   | without appreciable time for preparatory procedures. |           |
|   |                                                      |           |
|   | *Sources:* 121.339(b); 121.367                       |           |
|   |                                                      |           |
|   | 110\. Check at the aircraft, that required life      |           |
|   | rafts, that they are installed in conspicuously      |           |
|   | marked, approved locations.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.339(b); 121.367                       |           |
|   |                                                      |           |
|   | 111\. Check at the aircraft, that has life           |           |
|   | preservers are installed, that they are in           |           |
|   | conspicuously marked, approved locations.            |           |
|   |                                                      |           |
|   | *Sources:* 121.339(b); 121.367                       |           |
|   |                                                      |           |
|   | 112\. Check at the aircraft, that survival type      |           |
|   | emergency locator transmitters are installed, that   |           |
|   | they are in conspicuously marked, approved           |           |
|   | locations.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.339(b); 121.367                       |           |
|   |                                                      |           |
|   | 113\. Check at an aircraft that operates in extended |           |
|   | overwater operations that the aircraft was equipped  |           |
|   | with a life preserver equipped with an approved      |           |
|   | survivor locator light, for each occupant of the     |           |
|   | airplane.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.339(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 114\. Check at an aircraft, that operates in         |           |
|   | extended overwater operations, that each life        |           |
|   | preserver was inspected regularly in accordance with |           |
|   | inspection periods established in the operations     |           |
|   | specifications to ensure its condition for continued |           |
|   | serviceability and immediate readiness to perform    |           |
|   | its intended emergency purposes.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.339(a)(1); 121.367     |           |
|   |                                                      |           |
|   | 115\. Check at an aircraft that operates in any      |           |
|   | overwater operation, that each airplane was equipped |           |
|   | with life preservers in accordance with Sec.         |           |
|   | 121.339(a) (1) or with an approved flotation means   |           |
|   | for each occupant that was within easy reach of each |           |
|   | seated occupant and was readily removable from the   |           |
|   | airplane.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.340(a); 121.367                       |           |
|   |                                                      |           |
|   | 116\. Check at an aircraft that operates an airplane |           |
|   | in extended overwater operations, that the airplane  |           |
|   | was equipped with enough approved life rafts (each   |           |
|   | equipped with an approved survivor locator light) of |           |
|   | a rated capacity and buoyancy to accommodate the     |           |
|   | occupants of the airplane.                           |           |
|   |                                                      |           |
|   | *Sources:* 121.339(a)(2); 121.367; 25.1415(b)(1)     |           |
|   |                                                      |           |
|   | 117\. Check at an aircraft, that operates an         |           |
|   | airplane in extended overwater operations, that the  |           |
|   | airplane was equipped with either excess rafts or    |           |
|   | rafts of enough buoyancy and seating capacity beyond |           |
|   | the rated capacity of the rafts to accommodate all   |           |
|   | occupants of the airplane in the event of a loss of  |           |
|   | one raft of the largest rated capacity.              |           |
|   |                                                      |           |
|   | *Sources:* 121.339(a)(2); 121.367                    |           |
|   |                                                      |           |
|   | 118\. Check at an aircraft that operates an airplane |           |
|   | in extended overwater operations, that each life     |           |
|   | raft was inspected regularly in accordance with      |           |
|   | inspection periods established in the operations     |           |
|   | specifications to ensure its condition for continued |           |
|   | serviceability and immediate readiness to perform    |           |
|   | its intended emergency purposes.                     |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.339(a)(2); 121.367     |           |
|   |                                                      |           |
|   | 119\. Check at an aircraft that operates an airplane |           |
|   | in extended overwater operations, that the airplane  |           |
|   | was equipped with at least one pyrotechnic signaling |           |
|   | device for each life raft.                           |           |
|   |                                                      |           |
|   | *Sources:* 121.339(a)(3); 121.367                    |           |
|   |                                                      |           |
|   | 120\. Check at an aircraft that operates an airplane |           |
|   | in extended overwater operations, that each          |           |
|   | pyrotechnic signaling device was inspected regularly |           |
|   | in accordance with inspection periods established in |           |
|   | the operations specifications to ensure its          |           |
|   | condition for continued serviceability and immediate |           |
|   | readiness to perform its intended emergency          |           |
|   | purposes.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.339(a)(3); 121.367     |           |
|   |                                                      |           |
|   | 121\. Check at an aircraft, that conducts flag or    |           |
|   | supplemental operations or a domestic operation      |           |
|   | within the State of Alaska over an uninhabited area  |           |
|   | or any other area that (in its operations            |           |
|   | specifications) the Administrator specifies required |           |
|   | equipment for search and rescue in case of an        |           |
|   | emergency, that the airplane was equipped with a     |           |
|   | suitable pyrotechnic signaling device.               |           |
|   |                                                      |           |
|   | *Sources:* 121.353(a); 121.367                       |           |
|   |                                                      |           |
|   | 122\. Check at an aircraft, that conducts flag or    |           |
|   | supplemental operations or a domestic operation      |           |
|   | within the State of Hawaii over an uninhabited area  |           |
|   | or any other area that (in its operations            |           |
|   | specifications) the Administrator specifies required |           |
|   | equipment for search and rescue in case of an        |           |
|   | emergency, that the airplane was equipped with a     |           |
|   | suitable pyrotechnic signaling device.               |           |
|   |                                                      |           |
|   | *Sources:* 121.353(a); 121.367                       |           |
|   |                                                      |           |
|   | 123\. Check at the aircraft, that a survival kit,    |           |
|   | appropriately equipped for the route to be flown,    |           |
|   | was attached to each required life raft.             |           |
|   |                                                      |           |
|   | *Sources:* 121.339(c); 121.367                       |           |
|   |                                                      |           |
|   | 124\. Check at the aircraft, that each survival kit  |           |
|   | was inspected regularly in accordance with           |           |
|   | inspection periods established in the operations     |           |
|   | specifications, to ensure its condition for          |           |
|   | continued serviceability and immediate readiness to  |           |
|   | perform its intended emergency purposes.             |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.339(c); 121.367        |           |
|   |                                                      |           |
|   | 125\. Check at an aircraft, that conducts flag or    |           |
|   | supplemental operation within the State of Alaska    |           |
|   | over an uninhabited area or any other area that (in  |           |
|   | its operations specifications) the Administrator     |           |
|   | specifies required equipment for search and rescue   |           |
|   | in case of an emergency, that the airplane was       |           |
|   | equipped with enough survival kits, appropriately    |           |
|   | equipped for the route to be flown for the number of |           |
|   | occupants of the airplane.                           |           |
|   |                                                      |           |
|   | *Sources:* 121.353(c); 121.367                       |           |
|   |                                                      |           |
|   | 126\. Check at an aircraft, that conducts flag or    |           |
|   | supplemental operation within the State of Hawaii    |           |
|   | over an uninhabited area or any other area that (in  |           |
|   | its operations specifications) the Administrator     |           |
|   | specifies required equipment for search and rescue   |           |
|   | in case of an emergency, that the airplane was       |           |
|   | equipped with enough survival kits, appropriately    |           |
|   | equipped for the route to be flown for the number of |           |
|   | occupants of the airplane.                           |           |
|   |                                                      |           |
|   | *Sources:* 121.353(c); 121.367                       |           |
|   |                                                      |           |
|   | 127\. Check at the aircraft, that approved           |           |
|   | protective breathing equipment (PBE) that supplies   |           |
|   | breathing gas for 15 minutes at a pressure altitude  |           |
|   | of 8,000 feet that protects crewmembers from the     |           |
|   | effects of smoke, carbon dioxide or other harmful    |           |
|   | gases while combating fires were on board the        |           |
|   | airplane.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.337(a); 121.337(b)(1);                |           |
|   | 121.337(b)(7)(i)(B); 121.367                         |           |
|   |                                                      |           |
|   | 128\. Check at the aircraft, that protective         |           |
|   | breathing equipment (PBE) was inspected regularly in |           |
|   | accordance with inspection guidelines and            |           |
|   | established inspection periods.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(2); 121.367                    |           |
|   |                                                      |           |
|   | 129\. Check at the aircraft, that the part of the    |           |
|   | protective breathing equipment protecting the eyes   |           |
|   | does not impair the wearer\'s vision to the extent   |           |
|   | that a crewmember\'s duties cannot be accomplished   |           |
|   | and must allow corrective glasses to be worn without |           |
|   | impairment of vision.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(3); 121.367                    |           |
|   |                                                      |           |
|   | 130\. Check at the aircraft, that protective         |           |
|   | breathing equipment, while in use, allows crewmember |           |
|   | interphone communications between each of two flight |           |
|   | crewmember stations in the pilot compartment and at  |           |
|   | least one normal flight attendant station in each    |           |
|   | passenger compartment.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 131\. Check at the aircraft, that protective         |           |
|   | breathing equipment was provided that, while in use, |           |
|   | allows any crewmember to use the airplane interphone |           |
|   | system at any of the flight attendant stations.      |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(5); 121.367                    |           |
|   |                                                      |           |
|   | 132\. Check at the aircraft, that breathing          |           |
|   | equipment (PBE) is provided, if other than chemical  |           |
|   | oxygen generators, there is a means to allow the     |           |
|   | crew to readily determine, during the equipment      |           |
|   | preflight that the gas supply is fully charged.      |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(7)(iii); 121.367               |           |
|   |                                                      |           |
|   | 133\. Check at the aircraft, that protective         |           |
|   | breathing equipment with a fixed or portable         |           |
|   | breathing gas supply meeting the requirements of     |           |
|   | this section was conveniently located on the flight  |           |
|   | deck and be easily accessible for immediate use by   |           |
|   | each required flight crewmember at his or her        |           |
|   | assigned duty station.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(8); 121.367                    |           |
|   |                                                      |           |
|   | 134\. Check at the aircraft, that one PBE with a     |           |
|   | portable breathing gas supply was accessible and     |           |
|   | conveniently located for immediate use by            |           |
|   | crewmembers in combating fires for each hand fire    |           |
|   | extinguisher for use in a galley, other than a       |           |
|   | galley located in a passenger, cargo, or crew        |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(9)(i); 121.367                 |           |
|   |                                                      |           |
|   | 135\. Check at the aircraft, that one PBE with a     |           |
|   | portable breathing gas supply was accessible and     |           |
|   | conveniently located for immediate use by            |           |
|   | crewmembers in combating fires on the flight deck.   |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(9)(ii); 121.367                |           |
|   |                                                      |           |
|   | 136\. Check at the aircraft, in each passenger       |           |
|   | compartment, that one PBE with a portable breathing  |           |
|   | gas supply was located within 3 feet of each         |           |
|   | required hand fire extinguisher required by 14 CFR   |           |
|   | 121.309.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.337(b)(9)(iii); 121.367               |           |
|   |                                                      |           |
|   | 137\. Checks at the aircraft, that protective        |           |
|   | breathing equipment was installed for the use of     |           |
|   | appropriate crewmembers in each class A, cargo       |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1439(a)                       |           |
|   |                                                      |           |
|   | 138\. Check at the aircraft, that protective         |           |
|   | breathing equipment was installed for the use of     |           |
|   | appropriate crewmembers in each class B, cargo       |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1439(a)                       |           |
|   |                                                      |           |
|   | 139\. Check at the aircraft, that protective         |           |
|   | breathing equipment was installed for the use of     |           |
|   | appropriate crewmembers in each class E, cargo       |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1439(a)                       |           |
|   |                                                      |           |
|   | 140\. Check at the aircraft, that protective         |           |
|   | breathing equipment was installed in each isolated   |           |
|   | separate compartment in the airplane, including      |           |
|   | upper and lower lobe galleys, in which crewmember    |           |
|   | occupancy is permitted during flight for the maximum |           |
|   | number of crewmembers expected to be in the area     |           |
|   | during any operation.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1439(a)                       |           |
|   |                                                      |           |
|   | 141\. Check at a turbine engine powered aircraft     |           |
|   | with a pressurized cabin above flight level 250,     |           |
|   | that each flight crewmember on flight deck duty must |           |
|   | be provided with a quick-donning type oxygen         |           |
|   | dispensing unit connected to an oxygen supply        |           |
|   | terminal so designed that it can be rapidly placed   |           |
|   | on his face from its ready position, properly        |           |
|   | secured, sealed, and supplying oxygen upon demand,   |           |
|   | with one hand, within five seconds and without       |           |
|   | disturbing eyeglasses or causing delay in proceeding |           |
|   | with emergency duties.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.333(a); 121.333(c)(1); 121.367;       |           |
|   | 25.1447(c)(2)(i)                                     |           |
|   |                                                      |           |
|   | 142\. Check at a turbine engine powered aircraft     |           |
|   | with a pressurized cabin above flight level 250,     |           |
|   | that each flight crewmember on flight deck duty is   |           |
|   | provided with a quick-donning type oxygen dispensing |           |
|   | unit connected to an oxygen supply terminal so       |           |
|   | designed that after being placed on the face it does |           |
|   | not prevent immediate communication between the      |           |
|   | flight crewmember and other crewmembers over the     |           |
|   | airplane intercommunication system.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.333(a); 121.333(c)(1); 121.367;       |           |
|   | 25.1447(c)(2)(ii)                                    |           |
|   |                                                      |           |
|   | 143\. Check at the aircraft, that there was a means  |           |
|   | to allow the crew to readily determine, during       |           |
|   | flight, the quantity of oxygen available in each     |           |
|   | source of supply.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1441(c)                       |           |
|   |                                                      |           |
|   | 144\. Check at the aircraft, that there is an        |           |
|   | approved safety belt, equipped with a metal-to-metal |           |
|   | latching device, for separate use by each person on  |           |
|   | board the airplane who has reached his second        |           |
|   | birthday.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.311(a)(2); 121.367; 25.785(i)         |           |
|   |                                                      |           |
|   | 145\. Check at the aircraft, that each sideward      |           |
|   | facing seat was approved.                            |           |
|   |                                                      |           |
|   | *Sources:* 121.311(d); 121.367; 25.785(c)            |           |
|   |                                                      |           |
|   | 146\. Check at the aircraft, that if the seat backs  |           |
|   | do not provide a firm handhold, there was a handgrip |           |
|   | or rail along each aisle to enable persons to steady |           |
|   | themselves while using the aisles in moderately      |           |
|   | rough air.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.785(j)                        |           |
|   |                                                      |           |
|   | 147\. Check at the aircraft, that each item of       |           |
|   | installed equipment is labeled as to its             |           |
|   | identification, function, or operating limitations,  |           |
|   | or any applicable combination of these factors.      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1301(b)                       |           |
|   |                                                      |           |
|   | 148\. Check at the aircraft, that each item of       |           |
|   | installed equipment is installed according to        |           |
|   | limitations specified for that equipment.            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1301(c)                       |           |
|   |                                                      |           |
|   | 149\. Check at the aircraft, that each megaphone is  |           |
|   | clearly identified.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.309(f)(1);             |           |
|   | 121.309(f)(2); 121.367                               |           |
|   |                                                      |           |
|   | 150\. Check at the aircraft, that each megaphone is  |           |
|   | clearly marked to indicate its method of operation.  |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(3); 121.309(f)(1);             |           |
|   | 121.309(f)(2); 121.367                               |           |
|   |                                                      |           |
|   | 151\. Check at the aircraft, that each airplane has  |           |
|   | an emergency lighting system, independent of the     |           |
|   | main lighting system that illuminates each passenger |           |
|   | exit marking and locating sign.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(1); 121.367                    |           |
|   |                                                      |           |
|   | 152\. Check at an aircraft, type certificated after  |           |
|   | January 1, 1958 that the aircraft has an emergency   |           |
|   | lighting system, independent of the main lighting    |           |
|   | system that includes floor proximity emergency       |           |
|   | escape path marking which enables each passenger to  |           |
|   | visually identify the emergency escape path along    |           |
|   | the cabin aisle floor to the first exits or pair of  |           |
|   | exits forward and aft of the seat.                   |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(3); 121.367; 25.812(e)(1)      |           |
|   |                                                      |           |
|   | 153\. Check at an aircraft, type certificated after  |           |
|   | January 1, 1958 that the aircraft has an emergency   |           |
|   | lighting system, independent of the main lighting    |           |
|   | system that includes floor proximity emergency       |           |
|   | escape path marking which enables each passenger to  |           |
|   | readily identify each exit from the emergency escape |           |
|   | path by reference only to markings and visual        |           |
|   | features not more than 4 feet above the cabin floor. |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(3); 121.367; 25.812(e)(2)      |           |
|   |                                                      |           |
|   | 154\. Check at the aircraft, that each emergency     |           |
|   | light is operable manually both from the flightcrew  |           |
|   | station and, for airplanes on which a flight         |           |
|   | attendant is required, from a point in the passenger |           |
|   | compartment that is readily accessible to a normal   |           |
|   | flight attendant seat.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(1); 121.310(d)(1)(i); 121.367  |           |
|   |                                                      |           |
|   | 155\. Check at the aircraft, that each emergency     |           |
|   | light has a means to prevent inadvertent operation   |           |
|   | of the manual controls.                              |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(1); 121.310(d)(1)(ii); 121.367 |           |
|   |                                                      |           |
|   | 156\. Check at the aircraft, that each emergency     |           |
|   | light, when armed or turned on at either station,    |           |
|   | remain lighted or become lighted upon interruption   |           |
|   | of the airplane\'s normal electric power.            |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(1); 121.310(d)(1)(iii);        |           |
|   | 121.367                                              |           |
|   |                                                      |           |
|   | 157\. Check at the aircraft, that each emergency     |           |
|   | light, provides the required level of illumination   |           |
|   | for at least 10 minutes at the critical ambient      |           |
|   | conditions after emergency landing.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(1); 121.310(d)(3); 121.367     |           |
|   |                                                      |           |
|   | 158\. Check at the aircraft, that each emergency     |           |
|   | light, has a cockpit control device that has an      |           |
|   | \"on,\" \"off,\" and \"armed\" position.             |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(1); 121.310(d)(4); 121.367     |           |
|   |                                                      |           |
|   | 159\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed prior |           |
|   | to May 1, 1972, that the airplane is equipped with   |           |
|   | exterior lighting that is operable manually from the |           |
|   | flight crew station.                                 |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367; 25.812(f)(1)   |           |
|   |                                                      |           |
|   | 160\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed prior |           |
|   | to May 1, 1972, that the aircraft, not required by   |           |
|   | 25.809(f) to have descent assist means, is equipped  |           |
|   | with exterior emergency lighting at each             |           |
|   | non-overwing emergency exit, with illumination not   |           |
|   | less than 0.03 foot-candle (measured normal to the   |           |
|   | direction of the incident light) on the ground       |           |
|   | surface with the landing gear extended where an      |           |
|   | evacuee is likely to make his first contact with the |           |
|   | ground outside the cabin.                            |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367;                |           |
|   | 25.812(g)(1)(iii)                                    |           |
|   |                                                      |           |
|   | 161\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed on or |           |
|   | after May 1, 1972, that the aircraft is equipped     |           |
|   | with exterior lighting meeting the exterior          |           |
|   | emergency lighting requirements under which the      |           |
|   | airplane was type certificated.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(ii); 121.367                |           |
|   |                                                      |           |
|   | 162\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed prior |           |
|   | to May 1, 1972, that the aircraft was equipped with  |           |
|   | a slip-resistant escape route established from each  |           |
|   | overwing emergency exit.                             |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(2)(i); 121.367; 25.810(c)      |           |
|   |                                                      |           |
|   | 163\. Check at an aircraft, for which the            |           |
|   | application for the type certificate was filed on or |           |
|   | after May 1, 1972, that each airplane was equipped   |           |
|   | with a slip-resistant escape route meeting the       |           |
|   | requirements under which the airplane was type       |           |
|   | certificated.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(2)(ii); 121.367                |           |
|   |                                                      |           |
|   | 164\. Check at the aircraft, that it was equipped    |           |
|   | with flashlight stowage provisions accessible from   |           |
|   | each flight attendant seat.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.310(i); 121.367                       |           |
|   |                                                      |           |
|   | 165\. Check at an aircraft, with a Class A cargo     |           |
|   | compartment that there was a hand fire extinguisher  |           |
|   | available for each Class A compartment.              |           |
|   |                                                      |           |
|   | *Sources:* 121.221(b)(2); 121.367                    |           |
|   |                                                      |           |
|   | 166\. Check at the aircraft, that each hand fire     |           |
|   | extinguisher for use in each Class A cargo           |           |
|   | compartment was inspected regularly in accordance    |           |
|   | with inspection periods established in the           |           |
|   | operations specifications to ensure its condition    |           |
|   | for continued serviceability and immediate readiness |           |
|   | to perform its intended emergency purposes.          |           |
|   |                                                      |           |
|   | *Sources:* 121.221(b)(2); 121.309(b)(1); 121.367     |           |
|   |                                                      |           |
|   | 167\. Check at the aircraft, that each hand fire     |           |
|   | extinguisher was clearly identified and clearly      |           |
|   | marked to indicate its method of operation.          |           |
|   |                                                      |           |
|   | *Sources:* 121.221(b)(2); 121.309(b)(1); 121.367     |           |
|   |                                                      |           |
|   | 168\. Check at the aircraft, that each class B       |           |
|   | compartment has a separate approved smoke or fire    |           |
|   | detector system to give warning at the pilot or      |           |
|   | flight engineer station.                             |           |
|   |                                                      |           |
|   | *Sources:* 121.221(c)(1); 121.367                    |           |
|   |                                                      |           |
|   | 169\. Check at an aircraft, with a Class B cargo     |           |
|   | compartment that a hand fire extinguisher was        |           |
|   | available for the compartment.                       |           |
|   |                                                      |           |
|   | *Sources:* 121.221(c)(2); 121.367                    |           |
|   |                                                      |           |
|   | 170\. Check at an aircraft, that each hand fire      |           |
|   | extinguisher for use in each Class B cargo           |           |
|   | compartment was inspected regularly in accordance    |           |
|   | with inspection periods established in the           |           |
|   | operations specifications to ensure its condition    |           |
|   | for continued serviceability and immediate readiness |           |
|   | to perform its intended emergency purposes.          |           |
|   |                                                      |           |
|   | *Sources:* 121.221(c)(2); 121.309(b)(1); 121.367     |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s airframe and parts     | Yes       |
| . | thereof meet the requirements of the certificate     |           |
| 6 | holder\'s inspection program and the program         | No,       |
| . | covering other maintenance, preventive maintenance,  | Explain   |
|   | and alterations? **     **                           |           |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number displayed on the aircraft |           |
|   | fuselage exterior, adjacent to and aft of the rear   |           |
|   | most entrance door, or on the fuselage near the tail |           |
|   | surface, in such a manner that it will not likely be |           |
|   | defaced or removed during normal service, that a     |           |
|   | fireproof plate, is secured to an accessible         |           |
|   | exterior or interior location, near an entrance, in  |           |
|   | such a manner that it will not likely be defaced or  |           |
|   | removed during normal service or lost or destroyed   |           |
|   | in an accident, that has (1)Builder\'s name.         |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 2\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number displayed on the aircraft |           |
|   | fuselage exterior, adjacent to and aft of the rear   |           |
|   | most entrance door, or on the fuselage near the tail |           |
|   | surface, in such a manner that it will not likely be |           |
|   | defaced or removed during normal service, that a     |           |
|   | fireproof plate, is secured to an accessible         |           |
|   | exterior or interior location, near an entrance, in  |           |
|   | such a manner that it will not likely be defaced or  |           |
|   | removed during normal service or lost or destroyed   |           |
|   | in an accident, that has (2) Model designation.      |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 3\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number displayed on the aircraft |           |
|   | fuselage exterior, adjacent to and aft of the rear   |           |
|   | most entrance door, or on the fuselage near the tail |           |
|   | surface, in such a manner that it will not likely be |           |
|   | defaced or removed during normal service, that a     |           |
|   | fireproof plate, is secured to an accessible         |           |
|   | exterior or interior location, near an entrance, in  |           |
|   | such a manner that it will not likely be defaced or  |           |
|   | removed during normal service or lost or destroyed   |           |
|   | in an accident, that has (3) Builder\'s serial       |           |
|   | number.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 4\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number displayed on the aircraft |           |
|   | fuselage exterior, adjacent to and aft of the rear   |           |
|   | most entrance door, or on the fuselage near the tail |           |
|   | surface, in such a manner that it will not likely be |           |
|   | defaced or removed during normal service, that a     |           |
|   | fireproof plate, is secured to an accessible         |           |
|   | exterior or interior location, near an entrance, in  |           |
|   | such a manner that it will not likely be defaced or  |           |
|   | removed during normal service or lost or destroyed   |           |
|   | in an accident, that has (4) Type certificate        |           |
|   | number, if any.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 5\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number displayed on the aircraft |           |
|   | fuselage exterior, adjacent to and aft of the rear   |           |
|   | most entrance door, or on the fuselage near the tail |           |
|   | surface, in such a manner that it will not likely be |           |
|   | defaced or removed during normal service, that a     |           |
|   | fireproof plate, is secured to an accessible         |           |
|   | exterior or interior location, near an entrance, in  |           |
|   | such a manner that it will not likely be defaced or  |           |
|   | removed during normal service or lost or destroyed   |           |
|   | in an accident, that has (5) Production certificate  |           |
|   | number, if any                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 6\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number is NOT displayed on the   |           |
|   | aircraft fuselage exterior, that a fireproof plate,  |           |
|   | is secured to an accessible exterior or interior     |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (1)Builder\'s name.                              |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 7\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number is NOT displayed on the   |           |
|   | aircraft fuselage exterior, that a fireproof plate,  |           |
|   | is secured to an accessible exterior or interior     |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (2) Model designation.                           |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 8\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number is NOT displayed on the   |           |
|   | aircraft fuselage exterior, that a fireproof plate,  |           |
|   | is secured to an accessible exterior or interior     |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (3) Builder\'s serial number.                    |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 9\. Check, at the aircraft that was manufactured     |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number is NOT displayed on the   |           |
|   | aircraft fuselage exterior, that a fireproof plate,  |           |
|   | is secured to an accessible exterior or interior     |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (4) Type certificate number, if any.             |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 10\. Check, at the aircraft that was manufactured    |           |
|   | before March 7, 1988, and has the model designation  |           |
|   | and builders serial number is NOT displayed on the   |           |
|   | aircraft fuselage exterior, that a fireproof plate,  |           |
|   | is secured to an accessible exterior or interior     |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (5) Production certificate number, if any        |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 11\. Check, at the aircraft that was manufactured    |           |
|   | after March 7, 1988, that a fireproof plate is       |           |
|   | secured to an accessible exterior or interior        |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (1)Builder\'s name.                              |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 12\. Check, at the aircraft that was manufactured    |           |
|   | after March 7, 1988, that a fireproof plate is       |           |
|   | secured to an accessible exterior or interior        |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (2) Model designation.                           |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 13\. Check, at the aircraft that was manufactured    |           |
|   | after March 7, 1988, that a fireproof plate is       |           |
|   | secured to an accessible exterior or interior        |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (3) Builder\'s serial number.                    |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 14\. Check, at the aircraft that was manufactured    |           |
|   | after March 7, 1988, that a fireproof plate is       |           |
|   | secured to an accessible exterior or interior        |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (4) Type certificate number, if any.             |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 15\. Check, at the aircraft that was manufactured    |           |
|   | after March 7, 1988, that a fireproof plate is       |           |
|   | secured to an accessible exterior or interior        |           |
|   | location, near an entrance, in such a manner that it |           |
|   | will not likely be defaced or removed during normal  |           |
|   | service or lost or destroyed in an accident, that    |           |
|   | has (5) Production certificate number, if any        |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 45.11(a);         |           |
|   | 45.13(a)(1); 45.13(a)(2); 45.13(a)(3); 45.13(a)(4);  |           |
|   | 45.13(a)(5)                                          |           |
|   |                                                      |           |
|   | 16\. Check, at the aircraft, that engines are        |           |
|   | identified by means of a fireproof plate attached to |           |
|   | the engine marked on it by etching, stamping,        |           |
|   | engraving, or other approved method of fireproof     |           |
|   | marking, at an accessible location in such a manner  |           |
|   | that it will not likely be defaced or removed during |           |
|   | normal service or lost or destroyed in an accident,  |           |
|   | that has (1)Builder\'s name.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(a); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5); 45.13(a)(6)                |           |
|   |                                                      |           |
|   | 17\. Check, at the aircraft, that engines are        |           |
|   | identified by means of a fireproof plate attached to |           |
|   | the engine marked on it by etching, stamping,        |           |
|   | engraving, or other approved method of fireproof     |           |
|   | marking, at an accessible location in such a manner  |           |
|   | that it will not likely be defaced or removed during |           |
|   | normal service or lost or destroyed in an accident,  |           |
|   | that has (2) Model designation.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.153(a)(2); 121.367;    |           |
|   | 45.11(a); 45.13(a)(1); 45.13(a)(2); 45.13(a)(3);     |           |
|   | 45.13(a)(4); 45.13(a)(5); 45.13(a)(6)                |           |
|   |                                                      |           |
|   | 18\. Check, at the aircraft, that metallic           |           |
|   | components are bonded properly to the aircraft in    |           |
|   | accordance with the Certificate Holder\'s design.    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.581(b)(1)                     |           |
|   |                                                      |           |
|   | 19\. Check, at the aircraft, that non-metallic       |           |
|   | components are bonded properly to the aircraft in    |           |
|   | accordance with the Certificate Holder\'s design.    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.581(c)(2)                     |           |
|   |                                                      |           |
|   | 20\. Inspect the aircraft for major repairs, and     |           |
|   | verify that the approved data for that repair        |           |
|   | includes damage tolerance in accordance with the     |           |
|   | Certificate Holders design.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(17); 121.367; 25.571(a)(3)     |           |
|   |                                                      |           |
|   | 21\. Check, at the aircraft, that it was equipped    |           |
|   | with heated pitot tubes in accordance with the       |           |
|   | Certificate Holders design.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.323(e); 121.325(a); 121.367           |           |
|   |                                                      |           |
|   | 22\. Check, at the aircraft, that it was equipped    |           |
|   | with an operable pitot heat indication system        |           |
|   | incorporating an amber light that was in clear view  |           |
|   | of a flight crewmember to indicate to the flight     |           |
|   | crew when that pitot heating system was switched     |           |
|   | \"off\".                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.342; 121.367; 25.1326(a);             |           |
|   | 25.1326(b)(1)                                        |           |
|   |                                                      |           |
|   | 23\. Check, at the nontransport category airplane    |           |
|   | type certificated after December 31, 1964, that it   |           |
|   | was equipped with an operable pitot heat indication  |           |
|   | system incorporating an amber light that was in      |           |
|   | clear view of a flight crewmember to indicate to the |           |
|   | flight crew when the pitot heating system was        |           |
|   | switched \"off\".                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.342; 121.367; 25.1326(a);             |           |
|   | 25.1326(b)(1)                                        |           |
|   |                                                      |           |
|   | 24\. Check, at the aircraft, that it was equipped    |           |
|   | with an operable pitot heat indication system        |           |
|   | incorporating an amber light that was in clear view  |           |
|   | of a flight crewmember to indicate to the flight     |           |
|   | crew when that pitot heating system was not          |           |
|   | operating if the pitot heating system was switched   |           |
|   | \"on\" and any pitot tube heating element was        |           |
|   | inoperative.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.342; 121.367; 25.1326(a);             |           |
|   | 25.1326(b)(2)                                        |           |
|   |                                                      |           |
|   | 25\. Check, at the nontransport category airplane    |           |
|   | type certificated after December 31, 1964, that it   |           |
|   | was equipped with an operable pitot heat indication  |           |
|   | system incorporating an amber light that was in      |           |
|   | clear view of a flight crewmember to indicate to the |           |
|   | flight crew when that pitot heating system was not   |           |
|   | operating if the pitot heating system was switched   |           |
|   | \"on\" and any pitot tube heating element was        |           |
|   | inoperative.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.342; 121.367; 25.1326(a);             |           |
|   | 25.1326(b)(2)                                        |           |
|   |                                                      |           |
|   | 26\. Check, at the aircraft, that it was equipped    |           |
|   | with two independent static pressure systems, vented |           |
|   | to the outside atmospheric pressure so that they     |           |
|   | will be least affected by air flow variation or      |           |
|   | moisture or other foreign matter are installed on    |           |
|   | the airplane.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.313(e); 121.367                       |           |
|   |                                                      |           |
|   | 27\. Check, at the aircraft, that it was equipped    |           |
|   | with a means was provided for transferring an        |           |
|   | instrument from its primary operating system to an   |           |
|   | alternate system, the means includes a positive      |           |
|   | positioning control that was marked to indicate      |           |
|   | clearly which system was being used.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.313(e); 121.367                       |           |
|   |                                                      |           |
|   | 28\. Check, at the aircraft, that it was equipped    |           |
|   | with two landing lights.                             |           |
|   |                                                      |           |
|   | *Sources:* 121.323(c); 121.367                       |           |
|   |                                                      |           |
|   | 29\. Check, at the nontransport category airplane    |           |
|   | type certificated after December 31, 1964, that it   |           |
|   | was equipped with at least one landing light.        |           |
|   |                                                      |           |
|   | *Sources:* 121.323(c); 121.367                       |           |
|   |                                                      |           |
|   | 30\. Check, at the aircraft that was operated at     |           |
|   | night, that it was equipped position lights.         |           |
|   |                                                      |           |
|   | *Sources:* 121.323(a); 121.367                       |           |
|   |                                                      |           |
|   | 31\. Check, at the aircraft that was operated at     |           |
|   | night, that it was equipped with an anti-collision   |           |
|   | light.                                               |           |
|   |                                                      |           |
|   | *Sources:* 121.323(b); 121.367                       |           |
|   |                                                      |           |
|   | 32\. Check, at the aircraft, that specified markings |           |
|   | and are installed.                                   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1); 25.1541(a)(2)     |           |
|   |                                                      |           |
|   | 33\. Check, at the aircraft, that placards required  |           |
|   | for the safe operation are installed, if there are   |           |
|   | unusual airplane design, operating, or handling      |           |
|   | characteristics, in accordance with the Certificate  |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1); 25.1541(a)(2)     |           |
|   |                                                      |           |
|   | 34\. Check, at the aircraft, that the name of the    |           |
|   | Certificate Holder or operating certificate number   |           |
|   | of the Certificate Holder who was operating the      |           |
|   | aircraft, was legibly displayed on the aircraft and  |           |
|   | was clearly visible and readable from the outside of |           |
|   | the aircraft in accordance with the Certificate      |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 119.9(b); 121.367                         |           |
|   |                                                      |           |
|   | 35\. Check, at the turbine engine powered, transport |           |
|   | category aircraft, that all fuel tank covers located |           |
|   | in an area where experience or analysis indicates a  |           |
|   | strike was likely are fire resistant.                |           |
|   |                                                      |           |
|   | *Sources:* 121.316; 121.367; 25.963(e)(2)            |           |
|   |                                                      |           |
|   | 36\. Check, at the aircraft, that each passenger     |           |
|   | emergency exit on the side of the fuselage, when the |           |
|   | opening means for such an exit was located on only   |           |
|   | one side of the fuselage, has a conspicuous marking  |           |
|   | to that effect provided on the other side.           |           |
|   |                                                      |           |
|   | *Sources:* 121.310(g)(3); 121.367                    |           |
|   |                                                      |           |
|   | 37\. Check,at the all cargo aircraft with a class E  |           |
|   | cargo compartment, that required crew emergency      |           |
|   | exits are accessible under all cargo loading         |           |
|   | conditions in accordance with the Certificate        |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.221(f)(5); 121.367                    |           |
|   |                                                      |           |
|   | 38\. Check, at the passenger-carrying airplane for   |           |
|   | which the application for the type certificate was   |           |
|   | filed prior to May 1, 1972, that it was equipped     |           |
|   | with exterior lighting that was automatically        |           |
|   | activated when the assist means was erected.         |           |
|   |                                                      |           |
|   | *Sources:* 121.310(d)(1)(i); 121.310(h)(1)(i);       |           |
|   | 121.367; 25.812(f)(1)                                |           |
|   |                                                      |           |
|   | 39\. Check, at the passenger-carrying airplane for   |           |
|   | which the application for the type certificate was   |           |
|   | filed prior to May 1, 1972, that it was equipped     |           |
|   | with exterior lighting that was operable manually    |           |
|   | from the flight crew station and from a point in the |           |
|   | passenger compartment that was readily accessible to |           |
|   | a normal flight attendant seat.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.310(d)(1)(i); 121.310(h)(1)(i);       |           |
|   | 121.367; 25.812(f)(1)                                |           |
|   |                                                      |           |
|   | 40\. Check, at the passenger-carrying airplane for   |           |
|   | which the application for the type certificate was   |           |
|   | filed prior to May 1, 1972, that it was equipped     |           |
|   | with exterior lighting that has a flight crew        |           |
|   | warning light which illuminates when power was on in |           |
|   | the airplane and the emergency lighting control      |           |
|   | device was not armed.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367; 25.812(f)(2)   |           |
|   |                                                      |           |
|   | 41\. Check, at the aircraft electrical/electronics   |           |
|   | compartments, that no signs of poor condition,       |           |
|   | loose/missing equipment, fluid contamination or      |           |
|   | other indications of defects exist.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.369(b)                       |           |
|   |                                                      |           |
|   | 42\. Check, at the aircraft interior, that the       |           |
|   | forward and rear pressure bulkhead and under floor   |           |
|   | areas are in good condition and exhibit no evidence  |           |
|   | of damage, corrosion, fluid leaks.                   |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(16); 121.367; 121.369(b)       |           |
|   |                                                      |           |
|   | 43\. Check at the aircraft interior, forward and     |           |
|   | rear pressure bulkhead and under floor areas, for    |           |
|   | security of attachment and corrosion prevention      |           |
|   | treatment application.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(16); 121.367; 121.369(b)       |           |
|   |                                                      |           |
|   | 44\. Check, at the aircraft flight deck for          |           |
|   | condition, loose/missing equipment, deterioration,   |           |
|   | breakage, leakage, corrosion, and evidence of        |           |
|   | defects in windshields, windows, paneling, flooring, |           |
|   | controls, lighting, and wiring installations.        |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(16); 121.367; 121.369(b)       |           |
|   |                                                      |           |
|   | 45\. Check, at the aircraft flight deck for          |           |
|   | equipment condition, proper installation, and        |           |
|   | identification.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.153(a)(2); 121.367; 121.369(b)        |           |
|   |                                                      |           |
|   | 46\. Check, at the aircraft operated at night, that  |           |
|   | instrument lights provide sufficient illumination to |           |
|   | make each instrument, switch and other device        |           |
|   | necessary for safe operation easily readable.        |           |
|   |                                                      |           |
|   | *Sources:* 121.323(d); 121.367                       |           |
|   |                                                      |           |
|   | 47\. Check, at the aircraft operated at night, that  |           |
|   | instrument lights are installed so that their direct |           |
|   | rays are shielded from the pilot\'s eyes.            |           |
|   |                                                      |           |
|   | *Sources:* 121.323(d); 121.367                       |           |
|   |                                                      |           |
|   | 48\. Check, at the aircraft operated at night, that  |           |
|   | instrument lights are installed so that no           |           |
|   | objectionable reflections are visible to the pilot.  |           |
|   |                                                      |           |
|   | *Sources:* 121.323(d); 121.367                       |           |
|   |                                                      |           |
|   | 49\. Check, at the aircraft operated at night, that  |           |
|   | there was a means of controlling the intensity of    |           |
|   | illumination of instrument lights unless it was      |           |
|   | shown that non\--dimming instrument lights are       |           |
|   | satisfactory.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.323(d); 121.367                       |           |
|   |                                                      |           |
|   | 50\. Check, at the aircraft operated in IFR over the |           |
|   | top conditions, that instrument lights provide       |           |
|   | sufficient illumination to make each instrument,     |           |
|   | switch and other device necessary for safe operation |           |
|   | easily readable.                                     |           |
|   |                                                      |           |
|   | *Sources:* 121.325(c); 121.367                       |           |
|   |                                                      |           |
|   | 51\. Check, at the aircraft operated in IFR over the |           |
|   | top conditions, that instrument lights are installed |           |
|   | so that no objectionable reflections are visible to  |           |
|   | the pilot.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.325(c); 121.367                       |           |
|   |                                                      |           |
|   | 52\. Check, at the aircraft operated in IFR over the |           |
|   | top conditions, that there was a means of            |           |
|   | controlling the intensity of illumination of         |           |
|   | instrument lights unless it was shown that           |           |
|   | non-dimming instrument lights are satisfactory.      |           |
|   |                                                      |           |
|   | *Sources:* 121.325(c); 121.367                       |           |
|   |                                                      |           |
|   | 53\. Check at the aircraft, in the passenger         |           |
|   | compartment, that cargo was carried in an approved   |           |
|   | cargo bin.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(1); 121.367                    |           |
|   |                                                      |           |
|   | 54\. Check at the aircraft, in the passenger         |           |
|   | compartment, that cargo was carried in an approved   |           |
|   | cargo bin that has the maximum weight of cargo that  |           |
|   | the bin was approved to carry and any instructions   |           |
|   | necessary to insure proper weight distribution       |           |
|   | within the bin was conspicuously marked on the bin.  |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(2); 121.367                    |           |
|   |                                                      |           |
|   | 55\. Check at the aircraft, in the passenger         |           |
|   | compartment, that cargo was carried in an approved   |           |
|   | cargo bin that was attached to the seat tracks or to |           |
|   | the floor structure of the airplane.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 56\. Check at the aircraft, in the passenger         |           |
|   | compartment, that cargo was carried in an approved   |           |
|   | cargo bin that was fully enclosed and made of        |           |
|   | material that was at least flame resistant.          |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(6); 121.367                    |           |
|   |                                                      |           |
|   | 57\. Check at the aircraft, in the passenger         |           |
|   | compartment, that cargo was carried in an approved   |           |
|   | cargo bin that has suitable safeguards provided      |           |
|   | within the bin to prevent the cargo from shifting    |           |
|   | under emergency landing conditions.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(7); 121.367                    |           |
|   |                                                      |           |
|   | 58\. Check at the aircraft, in the passenger         |           |
|   | compartment, that cargo was carried in an approved   |           |
|   | cargo bin that was not installed in a position that  |           |
|   | obscures any passenger\'s view of the \"seat belt\"  |           |
|   | sign \"no smoking\" sign, or any required exit sign, |           |
|   | unless an auxiliary sign or other approved means for |           |
|   | proper notification of the passenger was provided.   |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(8); 121.367                    |           |
|   |                                                      |           |
|   | 59\. Check at an nontransport category airplane type |           |
|   | certificated after December 31, 1964, that cargo,    |           |
|   | including carry-on baggage was carried in an         |           |
|   | approved cargo rack, bin, or compartment installed   |           |
|   | in or on the airplane, if it was secured by an       |           |
|   | approved means.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.285(d); 121.367                       |           |
|   |                                                      |           |
|   | 60\. Check at the aircraft, that each baggage and    |           |
|   | cargo compartment, and each ballast location has a   |           |
|   | placard stating any limitations on contents,         |           |
|   | including weight, that are necessary under the       |           |
|   | loading requirements.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1557(a)                       |           |
|   |                                                      |           |
|   | 61\. Check at the aircraft, that means to prevent    |           |
|   | each item of galley equipment, when not in use,      |           |
|   | which was carried in a passenger or crew compartment |           |
|   | from becoming a hazard by shifting under the         |           |
|   | appropriate load factors corresponding to the        |           |
|   | emergency landing conditions under which the         |           |
|   | airplane was type certificated.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.576                          |           |
|   |                                                      |           |
|   | 62\. Check at the aircraft, that means to prevent    |           |
|   | each serving cart, when not in use, which was        |           |
|   | carried in a passenger or crew compartment, from     |           |
|   | becoming a hazard by shifting under the appropriate  |           |
|   | load factors corresponding to the emergency landing  |           |
|   | conditions under which the airplane was type         |           |
|   | certificated.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.576                          |           |
|   |                                                      |           |
|   | 63\. Check at the aircraft, that means to prevent    |           |
|   | each item of crew baggage, which was carried in a    |           |
|   | passenger or crew compartment from becoming a hazard |           |
|   | by shifting under the appropriate load factors       |           |
|   | corresponding to the emergency landing conditions    |           |
|   | under which the airplane was type certificated.      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.576                          |           |
|   |                                                      |           |
|   | 64\. Check at the aircraft, that a suitable closet   |           |
|   | was placarded for its maximum weight and providing   |           |
|   | proper restraint for all baggage or cargo stowed     |           |
|   | within, and in a manner that does not hinder the     |           |
|   | possible use of any emergency equipment was provided |           |
|   | for each article of baggage to be stowed.            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.589(c)(1)                    |           |
|   |                                                      |           |
|   | 65\. Check at the aircraft, that a baggage stowage   |           |
|   | compartment was placarded for its maximum weight and |           |
|   | providing proper restraint for all baggage or cargo  |           |
|   | stowed within, and in a manner that does not hinder  |           |
|   | the possible use of any emergency equipment was      |           |
|   | provided for each article of baggage to be stowed.   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.589(c)(1)                    |           |
|   |                                                      |           |
|   | 66\. Check that the Certificate Holder\'s inspection |           |
|   | program and program covering other maintenance,      |           |
|   | preventive maintenance and alterations ensures that  |           |
|   | each floor level door or exit in the side of the     |           |
|   | fuselage (other than those leading into a cargo or   |           |
|   | baggage compartment that was not accessible from the |           |
|   | passenger cabin) that was 44 or more inches high and |           |
|   | 20 or more inches wide, but not wider than 46        |           |
|   | inches.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.310(i); 121.367                       |           |
|   |                                                      |           |
|   | 67\. Check at the aircraft, that each flight         |           |
|   | attendant has a seat for takeoff and landing in the  |           |
|   | passenger compartment that is near a required floor  |           |
|   | level emergency exit, except that another location   |           |
|   | is acceptable if the emergency egress of passengers  |           |
|   | would be enhanced with that location.                |           |
|   |                                                      |           |
|   | *Sources:* 121.311(g); 121.367; 25.785(h)(1)         |           |
|   |                                                      |           |
|   | 68\. Check at the aircraft, that each flight         |           |
|   | attendant has a seat for takeoff and landing in the  |           |
|   | passenger compartment that was located adjacent to   |           |
|   | each Type A emergency exit.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.311(g); 121.367; 25.785(h)(1)         |           |
|   |                                                      |           |
|   | 69\. Check at the aircraft, that each flight         |           |
|   | attendant has a seat for takeoff and landing in the  |           |
|   | passenger compartment that was located adjacent to   |           |
|   | each Type B emergency exit.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.311(g); 121.367; 25.785(h)(1)         |           |
|   |                                                      |           |
|   | 70\. Check at the aircraft, that each flight         |           |
|   | attendant has a seat for takeoff and landing in the  |           |
|   | passenger compartment that is, to the extent         |           |
|   | possible, without compromising proximity to a        |           |
|   | required floor level emergency exit, located to      |           |
|   | provide a direct view of the cabin area for which    |           |
|   | the flight attendant is responsible.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.311(g); 121.367; 25.785(h)(2)         |           |
|   |                                                      |           |
|   | 71\. Check at the aircraft, that each flight         |           |
|   | attendant has a seat for takeoff and landing in the  |           |
|   | passenger compartment that is positioned so that the |           |
|   | seat will not interfere with the use of a passageway |           |
|   | or exit when the seat was not in use.                |           |
|   |                                                      |           |
|   | *Sources:* 121.311(g); 121.367; 25.785(h)(3)         |           |
|   |                                                      |           |
|   | 72\. Check at the aircraft, that each flight         |           |
|   | attendant has a seat for takeoff and landing in the  |           |
|   | passenger compartment that was located to minimize   |           |
|   | the probability that occupants would suffer injury   |           |
|   | by being struck by items dislodged from service      |           |
|   | areas, stowage compartments, or service equipment.   |           |
|   |                                                      |           |
|   | *Sources:* 121.311(g); 121.367; 25.785(h)(4)         |           |
|   |                                                      |           |
|   | 73\. Check at the aircraft, that each flight         |           |
|   | attendant has a seat for takeoff and landing in the  |           |
|   | passenger compartment that was either forward or     |           |
|   | rearward facing with an energy absorbing rest that   |           |
|   | was designed to support the arms, shoulders, head,   |           |
|   | and spine.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.311(g); 121.367; 25.785(h)(5)         |           |
|   |                                                      |           |
|   | 74\. Check at the aircraft, that each flight         |           |
|   | attendant has a seat for takeoff and landing in the  |           |
|   | passenger compartment that was equipped with a       |           |
|   | restraint system consisting of a combined safety     |           |
|   | belt and shoulder harness unit, equipped with a      |           |
|   | metal to metal latching device, with a single point  |           |
|   | release. There must be means to secure each          |           |
|   | restraint system when not in use to prevent          |           |
|   | interference with rapid egress in an emergency.      |           |
|   |                                                      |           |
|   | *Sources:* 121.311(g); 121.367; 25.785(h)(6);        |           |
|   | 25.785(i)                                            |           |
|   |                                                      |           |
|   | 75\. Check at the aircraft, that each compartment,   |           |
|   | when used for storing cargo or baggage, materials    |           |
|   | used in the construction of the compartments,        |           |
|   | including tie-down equipment, was at least flame     |           |
|   | resistant.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(3); 121.367                    |           |
|   |                                                      |           |
|   | 76\. Check at a transport category aircraft that was |           |
|   | type certificated after January 1, 1958 that each    |           |
|   | Class C compartment, that is greater than 200 cubic  |           |
|   | feet in volume has ceiling and sidewall liner panels |           |
|   | which are constructed of glass fiber reinforced      |           |
|   | resin or materials which meet the test requirements  |           |
|   | of part 25, appendix F, part III of this chapter; or |           |
|   | in the case of liner installations approved prior to |           |
|   | March 20, 1989, aluminum.                            |           |
|   |                                                      |           |
|   | *Sources:* 121.314(a)(1); 121.314(a)(2);             |           |
|   | 121.314(a)(3); 121.367                               |           |
|   |                                                      |           |
|   | 77\. Check at a transport category aircraft that was |           |
|   | type certificated after January 1, 1958 that each    |           |
|   | Class D compartment, that is greater than 200 cubic  |           |
|   | feet in volume has ceiling and sidewall liner panels |           |
|   | which are constructed of glass fiber reinforced      |           |
|   | resin or materials which meet the test requirements  |           |
|   | of part 25, appendix F, part III of this chapter; or |           |
|   | in the case of liner installations approved prior to |           |
|   | March 20, 1989, aluminum.                            |           |
|   |                                                      |           |
|   | *Sources:* 121.314(a)(1); 121.314(a)(2);             |           |
|   | 121.314(a)(3); 121.367                               |           |
|   |                                                      |           |
|   | 78\. Check at the record repository for an aircraft  |           |
|   | that operates at flight levels above 270, that it    |           |
|   | was successfully demonstrated to the Administrator   |           |
|   | that the concentration of ozone inside the cabin     |           |
|   | will not exceed 0.1 parts per million by volume, sea |           |
|   | level equivalent, time-weighted average for each     |           |
|   | flight segment that exceeds 4 hours and includes     |           |
|   | flight above that flight level.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.578(b)(2)                    |           |
|   |                                                      |           |
|   | 79\. Check at an aircraft that operates on a flight  |           |
|   | on which smoking is prohibited by part 252, that     |           |
|   | either the \"No Smoking\" passenger information      |           |
|   | signs are lighted during the entire flight, or one   |           |
|   | or more \"No Smoking\" placards meeting the          |           |
|   | requirements of 14 CFR Part 25.1541 of are posted    |           |
|   | during the entire flight segment.                    |           |
|   |                                                      |           |
|   | *Sources:* 121.317(c); 121.367                       |           |
|   |                                                      |           |
|   | 80\. Check at the aircraft, that it was equipped     |           |
|   | with passenger information signs that notify when    |           |
|   | seat belts should be fastened, constructed so that   |           |
|   | the crewmembers can turn them on and off and, when   |           |
|   | illuminated, are legible under all probable          |           |
|   | conditions of cabin illumination to each person      |           |
|   | seated in the cabin.                                 |           |
|   |                                                      |           |
|   | *Sources:* 121.317(a); 121.367; 25.791(b)            |           |
|   |                                                      |           |
|   | 81\. Check at an aircraft that operates as a         |           |
|   | passenger-carrying airplane, that at least one       |           |
|   | legible sign or placard that reads \"Fasten Seat     |           |
|   | Belt While Seated\" is visible from each passenger   |           |
|   | seat.                                                |           |
|   |                                                      |           |
|   | *Sources:* 121.317(d); 121.367                       |           |
|   |                                                      |           |
|   | 82\. Check at the aircraft, that a door is installed |           |
|   | between the passenger and pilot compartments (i.e.,  |           |
|   | flightdeck door), with a locking means to prevent    |           |
|   | passengers from opening it without the pilot\'s      |           |
|   | permission (except that nontransport category        |           |
|   | airplanes certificated after December 31, 1964).     |           |
|   |                                                      |           |
|   | *Sources:* 121.313(f); 121.367                       |           |
|   |                                                      |           |
|   | 83\. Check at the aircraft, that except for the      |           |
|   | flightdeck door, there was a key for each door that  |           |
|   | separates a passenger compartment from another       |           |
|   | compartment that has emergency exit provisions.      |           |
|   |                                                      |           |
|   | *Sources:* 121.313(g); 121.367                       |           |
|   |                                                      |           |
|   | 84\. Check at the aircraft, that there was a means   |           |
|   | for the crew, in an emergency to unlock each door    |           |
|   | that leads to a compartment that is normally         |           |
|   | accessible to passengers and that can be locked by   |           |
|   | passengers.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.313(g); 121.367                       |           |
|   |                                                      |           |
|   | 85\. Check at a large passenger-carrying             |           |
|   | turbojet-powered aircraft, that each ventral exit    |           |
|   | and tailcone exit was marked with a placard readable |           |
|   | from a distance of 30 inches and installed at a      |           |
|   | conspicuous location near the means of opening the   |           |
|   | exit, stating that the exit has been designed and    |           |
|   | constructed so that it cannot be opened during       |           |
|   | flight.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.310(k)(2); 121.367                    |           |
|   |                                                      |           |
|   | 86\. Check at the aircraft, that a placard is        |           |
|   | installed on each door that is the means of access   |           |
|   | to a required passenger emergency exit, to indicate  |           |
|   | that it must be open during takeoff and landing.     |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h); 121.367                       |           |
|   |                                                      |           |
|   | 87\. Check at the aircraft, that the airplane        |           |
|   | contains the specified markings and placards.        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1)                    |           |
|   |                                                      |           |
|   | 88\. Check at the aircraft, that each marking and    |           |
|   | placard may not be easily erased, disfigured, or     |           |
|   | obscured.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(b)(2)                    |           |
|   |                                                      |           |
|   | 89\. Check at the aircraft, that each baggage and    |           |
|   | cargo compartment, except underseat compartments     |           |
|   | designed for the storage of carry-on articles        |           |
|   | weighing not more than 20 pounds, and each ballast   |           |
|   | location must have a placard stating any limitations |           |
|   | on contents, including weight, that are necessary    |           |
|   | under the loading requirements.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1557(a)                       |           |
|   |                                                      |           |
|   | 90\. Check at the aircraft, that each megaphone,     |           |
|   | when carried in a compartment or container, is       |           |
|   | carried in a compartment or container marked as to   |           |
|   | contents.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(f)(1);             |           |
|   | 121.309(f)(2); 121.367                               |           |
|   |                                                      |           |
|   | 91\. Check at the aircraft, that each megaphone,     |           |
|   | when carried in a compartment or container, the      |           |
|   | compartment or container, or the megaphone itself,   |           |
|   | is marked as to date of last inspection.             |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(4); 121.309(f)(1);             |           |
|   | 121.309(f)(2); 121.367                               |           |
|   |                                                      |           |
|   | 92\. Check at an aircraft, for which the application |           |
|   | for the type certificate was filed prior to May 1,   |           |
|   | 1972, that the airplane is equipped with exterior    |           |
|   | lighting that is operable manually from the flight   |           |
|   | crew station.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.310(h)(1)(i); 121.367; 25.812(f)(1)   |           |
|   |                                                      |           |
|   | 93\. Check at an aircraft, for which the application |           |
|   | for the type certificate was filed prior to May 1,   |           |
|   | 1972, that the aircraft is equipped with exterior    |           |
|   | lighting that has an \"on,\" \"off,\" and \"armed\"  |           |
|   | position so that when armed in the cockpit or turned |           |
|   | on at either the cockpit or flight attendant station |           |
|   | the lights will either light or remain lighted upon  |           |
|   | interruption (except an interruption caused by a     |           |
|   | transverse vertical separation of the fuselage       |           |
|   | during crash landing) of the airplane\'s normal      |           |
|   | electric power. There must be a means to safeguard   |           |
|   | against inadvertent operation of the control device  |           |
|   | from the \"armed\" or \"on\" positions.              |           |
|   |                                                      |           |
|   | *Sources:* 121.310(d)(1)(ii); 121.310(h)(1)(i);      |           |
|   | 121.367                                              |           |
|   |                                                      |           |
|   | 94\. Check at an aircraft, with a seating capacity   |           |
|   | of more than 19 passengers, that it was equipped     |           |
|   | with a public address system which is approved in    |           |
|   | accordance with 14CFR 21.305 and is capable of       |           |
|   | operation independent of the crewmember interphone   |           |
|   | system required by 14 CFR 121.319, except for        |           |
|   | handsets, headsets, microphones, selector switches,  |           |
|   | and signaling devices.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.318(a); 121.318(b); 121.367           |           |
|   |                                                      |           |
|   | 95\. Check at an aircraft, with a seating capacity   |           |
|   | of more than 19 passengers, that it was equipped     |           |
|   | with a public address system which is approved in    |           |
|   | accordance with 14 CFR 21.305 and is accessible for  |           |
|   | immediate use from each of two flight crewmember     |           |
|   | stations in the pilot compartment.                   |           |
|   |                                                      |           |
|   | *Sources:* 121.318(b); 121.318(c); 121.367           |           |
|   |                                                      |           |
|   | 96\. Check at an aircraft, with a seating capacity   |           |
|   | of more than 19 passengers, that it was equipped     |           |
|   | with a public address system which is approved in    |           |
|   | accordance with 14 CFR 21.305 and for each required  |           |
|   | floor-level passenger emergency exit which has an    |           |
|   | adjacent flight attendant seat, has a microphone     |           |
|   | which is readily accessible to the seated flight     |           |
|   | attendant, except that one microphone may serve more |           |
|   | than one exit, provided the proximity of the exits   |           |
|   | allows unassisted verbal communication between       |           |
|   | seated flight attendants.                            |           |
|   |                                                      |           |
|   | *Sources:* 121.318(b); 121.318(d); 121.367           |           |
|   |                                                      |           |
|   | 97\. Check at an aircraft, with a seating capacity   |           |
|   | of more than 19 passengers, that it was equipped     |           |
|   | with a public address system which is approved in    |           |
|   | accordance with 14 CFR 21.305 and is capable of      |           |
|   | operation within 10 seconds by a flight attendant at |           |
|   | each of those stations in the passenger compartment  |           |
|   | from which its use is accessible.                    |           |
|   |                                                      |           |
|   | *Sources:* 121.318(b); 121.318(e); 121.367           |           |
|   |                                                      |           |
|   | 98\. Check at an aircraft, with a seating capacity   |           |
|   | of more than 19 passengers, that it was equipped     |           |
|   | with a public address system which is approved in    |           |
|   | accordance with 14 CFR 21.305 and is audible at all  |           |
|   | passenger seats, lavatories, and flight attendant    |           |
|   | seats and work stations.                             |           |
|   |                                                      |           |
|   | *Sources:* 121.318(b); 121.318(f); 121.367           |           |
|   |                                                      |           |
|   | 99\. Check at a transport category aircraft,         |           |
|   | manufactured on or after November 27, 1990, with a   |           |
|   | seating capacity of more than 19 passengers, that it |           |
|   | was equipped with a public address system which is   |           |
|   | approved in accordance with 14 CFR 21.305 and is     |           |
|   | powerable when the aircraft is in flight or stopped  |           |
|   | on the ground, after the shutdown or failure of all  |           |
|   | engines and auxiliary power units, or the            |           |
|   | disconnection or failure of all power sources        |           |
|   | dependent on their continued operation, for a time   |           |
|   | duration of at least 10 minutes, including an        |           |
|   | aggregate time duration of at least 5 minutes of     |           |
|   | announcements made by flight and cabin crewmembers,  |           |
|   | considering all other loads which may remain powered |           |
|   | by the same source when all other power sources are  |           |
|   | inoperative.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.318(b); 121.318(g); 121.367;          |           |
|   | 25.1423(a)(1)                                        |           |
|   |                                                      |           |
|   | 100\. Check at a transport category aircraft,        |           |
|   | manufactured on or after November 27, 1990, with a   |           |
|   | seating capacity of more than 19 passengers, that it |           |
|   | was equipped with a public address system which is   |           |
|   | approved in accordance with 14 CFR 21.305 and is     |           |
|   | powerable when the aircraft is in flight or stopped  |           |
|   | on the ground, after the shutdown or failure of all  |           |
|   | engines and auxiliary power units, or the            |           |
|   | disconnection or failure of all power sources        |           |
|   | dependent on their continued operation, for an       |           |
|   | additional time duration in its standby state        |           |
|   | appropriate or required for any other loads that are |           |
|   | powered by the same source and that are essential to |           |
|   | safety of flight or required during emergency        |           |
|   | conditions.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.318(b); 121.318(g); 121.367;          |           |
|   | 25.1423(a)(2)                                        |           |
|   |                                                      |           |
|   | 101\. Check that the Certificate Holder, who         |           |
|   | operates an airplane with a seating capacity of more |           |
|   | than 19 passengers has an inspection and a program   |           |
|   | and program covering other maintenance preventive    |           |
|   | maintenance and alterations that ensures that the    |           |
|   | airplane is equipped with a crewmember interphone    |           |
|   | system that is approved in accordance with 14 CFR    |           |
|   | 21.305 and is capable of operation independent of    |           |
|   | the public address system required by 14 CFR         |           |
|   | 121.318(a) except for handsets, headsets,            |           |
|   | microphones, selector switches, and signaling        |           |
|   | devices.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(2); 121.367                    |           |
|   |                                                      |           |
|   | 102\. Check at an aircraft, with a seating capacity  |           |
|   | of more than 19 passengers that the aircraft was     |           |
|   | equipped with a crewmember interphone system that is |           |
|   | approved in accordance with 14 CFR 21.305 and is and |           |
|   | provides a means of two-way communication between    |           |
|   | the pilot compartment and each passenger             |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(3); 121.319(b)(1)(i); 121.367  |           |
|   |                                                      |           |
|   | 103\. Check at an aircraft, with a seating capacity  |           |
|   | of more than 19 passengers that the aircraft was     |           |
|   | equipped with a crewmember interphone system that is |           |
|   | approved in accordance with 14 CFR 21.305 and is and |           |
|   | provides a means of two-way communication between    |           |
|   | the pilot compartment each galley located on other   |           |
|   | than the main passenger deck level.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(3); 121.319(b)(1)(ii); 121.367 |           |
|   |                                                      |           |
|   | 104\. Check at an aircraft, with a seating capacity  |           |
|   | of more than 19 passengers that the aircraft was     |           |
|   | equipped with a crewmember interphone system that is |           |
|   | approved in accordance with 14 CFR 21.305 and is     |           |
|   | accessible for immediate use from each of two flight |           |
|   | crewmember stations in the pilot compartment.        |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(3); 121.319(b)(2); 121.367     |           |
|   |                                                      |           |
|   | 105\. Check at an aircraft, with a seating capacity  |           |
|   | of more than 19 passengers that the aircraft was     |           |
|   | equipped with a crewmember interphone system that is |           |
|   | approved in accordance with 14 CFR 21.305 and is     |           |
|   | accessible for use from at least one normal flight   |           |
|   | attendant station in each passenger compartment.     |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(3); 121.319(b)(3); 121.367     |           |
|   |                                                      |           |
|   | 106\. Check at an aircraft, with a seating capacity  |           |
|   | of more than 19 passengers that the aircraft was     |           |
|   | equipped with a crewmember interphone system that is |           |
|   | approved in accordance with 14 CFR 21.305 and is     |           |
|   | capable of operation within 10 seconds by a flight   |           |
|   | attendant at those stations in each passenger        |           |
|   | compartment from which its use is accessible.        |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(3); 121.319(b)(4); 121.367     |           |
|   |                                                      |           |
|   | 107\. Check at a large turbojet-powered aircraft     |           |
|   | with a seating capacity of more than 19 passengers   |           |
|   | that the airplane is equipped with a crewmember      |           |
|   | interphone system that is approved in accordance     |           |
|   | with 14 CFR 21.305 and is accessible for use at      |           |
|   | enough flight attendant stations so that all         |           |
|   | floor-level emergency exits (or entryways to those   |           |
|   | exits in the case of exits located within galleys)   |           |
|   | in each passenger compartment are observable from    |           |
|   | one or more of those stations so equipped.           |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(3); 121.319(b)(5)(i); 121.367  |           |
|   |                                                      |           |
|   | 108\. Check at a large turbojet-powered aircraft     |           |
|   | with a seating capacity of more than 19 passengers   |           |
|   | that the airplane is equipped with a crewmember      |           |
|   | interphone system that is approved in accordance     |           |
|   | with 14 CFR 21.305 and has an alerting system        |           |
|   | incorporating aural or visual signals for use by     |           |
|   | flight crewmembers to alert flight attendants and    |           |
|   | for use by flight attendants to alert flight         |           |
|   | crewmembers.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(3); 121.319(b)(5)(ii); 121.367 |           |
|   |                                                      |           |
|   | 109\. Check at a large turbojet-powered aircraft     |           |
|   | with a seating capacity of more than 19 passengers   |           |
|   | ensures that the airplane is equipped with a         |           |
|   | crewmember interphone system that is approved in     |           |
|   | accordance with 14 CFR 21.305 and has an alerting    |           |
|   | system with a means for the recipient of a call to   |           |
|   | determine whether it is a normal call or an          |           |
|   | emergency call.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.319(b)(5)(iii); 121.367               |           |
|   |                                                      |           |
|   | 110\. Check at a large turbojet-powered aircraft     |           |
|   | with a seating capacity of more than 19 passengers   |           |
|   | that the airplane is equipped with a crewmember      |           |
|   | interphone system that is approved in accordance     |           |
|   | with 14 CFR 21.305 and when the airplane is on the   |           |
|   | ground, provides a means of two-way communication    |           |
|   | between ground personnel and either of at least two  |           |
|   | flight crewmembers in the pilot compartment. The     |           |
|   | interphone system station for use by ground          |           |
|   | personnel must be so located that personnel using    |           |
|   | the system may avoid visible detection from within   |           |
|   | the airplane.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.319(a)(3); 121.319(b)(5)(iv); 121.367 |           |
|   |                                                      |           |
|   | 111\. Check at the aircraft, that protective fuses   |           |
|   | were installed on the airplane.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.313(a); 121.367                       |           |
|   |                                                      |           |
|   | 112\. Check at the aircraft, that the number of      |           |
|   | spare fuses were approved for that aircraft and      |           |
|   | appropriately described in the Certificate Holder\'s |           |
|   | manual.                                              |           |
|   |                                                      |           |
|   | *Sources:* 121.313(a); 121.367                       |           |
|   |                                                      |           |
|   | 113\. Check at the aircraft, that protective fuses   |           |
|   | were installed on the airplane, the number of spare  |           |
|   | fuses approved for that airplane and appropriately   |           |
|   | described in the Certificate Holder\'s manual.       |           |
|   |                                                      |           |
|   | *Sources:* 121.313(a); 121.367                       |           |
|   |                                                      |           |
|   | 114\. Check at the aircraft, that the aircraft was   |           |
|   | equipped with a power supply and distribution system |           |
|   | that is able to produce and distribute the load for  |           |
|   | the required instruments and equipment, with use of  |           |
|   | an external power supply if any one power source or  |           |
|   | component of the power distribution system fails.    |           |
|   |                                                      |           |
|   | *Sources:* 121.313(c); 121.367                       |           |
|   |                                                      |           |
|   | 115\. Check at the aircraft, that each compartment,  |           |
|   | when used for storing cargo or baggage, is designed  |           |
|   | so that no compartment includes controls, wiring,    |           |
|   | lines, equipment, or accessories that would upon     |           |
|   | damage or failure, affect the safe operation of the  |           |
|   | airplane unless the item is adequately shielded,     |           |
|   | isolated, or otherwise protected so that it cannot   |           |
|   | be damaged by movement of cargo in the compartment   |           |
|   | and so that damage to or failure of the item would   |           |
|   | not create a fire hazard in the compartment.         |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 116\. Check at the aircraft, that each compartment,  |           |
|   | when used for storing cargo or baggage, is designed  |           |
|   | so that cargo or baggage may not interfere with the  |           |
|   | functioning of the fire-protective features of the   |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(2); 121.367                    |           |
|   |                                                      |           |
|   | 117\. Check at an aircraft, with a Class A cargo     |           |
|   | compartment, that a fire therein would be readily    |           |
|   | discernible to a member of the crew while at his     |           |
|   | station.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.221(b)(1); 121.367                    |           |
|   |                                                      |           |
|   | 118\. Check at an aircraft, with a Class A cargo     |           |
|   | compartment that all parts of the compartment are    |           |
|   | easily accessible in flight.                         |           |
|   |                                                      |           |
|   | *Sources:* 121.221(b)(2); 121.367                    |           |
|   |                                                      |           |
|   | 119\. Check at the aircraft, that each class B       |           |
|   | compartment was lined with fire-resistant material,  |           |
|   | except that additional service lining of             |           |
|   | flame-resistant material may be used.                |           |
|   |                                                      |           |
|   | *Sources:* 121.221(c)(3); 121.367                    |           |
|   |                                                      |           |
|   | 120\. Check at an aircraft, with a Class B cargo     |           |
|   | compartment, that each class B compartment has a     |           |
|   | liner, separate from (but may be attached to) the    |           |
|   | airplane structure.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(b)                        |           |
|   |                                                      |           |
|   | 121\. Check at an aircraft, with a Class C cargo     |           |
|   | compartment, that each class C cargo compartment has |           |
|   | a separate approved smoke or fire detector system to |           |
|   | give warning at the pilot or flight engineer         |           |
|   | station.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.221(d)(1); 121.367                    |           |
|   |                                                      |           |
|   | 122\. Check at an aircraft, with a Class C cargo     |           |
|   | compartment, that each class C cargo compartment has |           |
|   | an approved built-in fire-extinguishing system       |           |
|   | controlled from the pilot or flight engineer         |           |
|   | station.                                             |           |
|   |                                                      |           |
|   | *Sources:* 121.221(d)(2); 121.367                    |           |
|   |                                                      |           |
|   | 123\. Check at an aircraft, with a Class C cargo     |           |
|   | compartment, that each class C cargo compartment     |           |
|   | ventilation and draft is controlled so that the      |           |
|   | extinguishing agent provided can control any fire    |           |
|   | that may start in the compartment.                   |           |
|   |                                                      |           |
|   | *Sources:* 121.221(d)(4); 121.367                    |           |
|   |                                                      |           |
|   | 124\. Check at an aircraft, with a Class C cargo     |           |
|   | compartment, that each class C cargo compartment was |           |
|   | lined with fire-resistant material, except that      |           |
|   | additional service lining of flame-resistant         |           |
|   | material may be used.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.221(d)(5); 121.367                    |           |
|   |                                                      |           |
|   | 125\. Check at an aircraft, type certificated after  |           |
|   | January 1, 1958 with a Class C cargo compartment,    |           |
|   | that is greater than 200 cubic feet in volume, that  |           |
|   | each class C cargo compartment has ceiling and       |           |
|   | sidewall liner panels which are constructed of glass |           |
|   | fiber reinforced resin, or meet the test             |           |
|   | requirements of 14 CFR part 25, appendix F, part     |           |
|   | III.                                                 |           |
|   |                                                      |           |
|   | *Sources:* 121.314(a)(1); 121.314(a)(2); 121.367     |           |
|   |                                                      |           |
|   | 126\. Check at a transport category aircraft, type   |           |
|   | certificated after January 1, 1958 with a Class C    |           |
|   | cargo compartment, that is greater than 200 cubic    |           |
|   | feet in volume, that has liner installations         |           |
|   | approved prior to March 20, 1989 that each class C   |           |
|   | cargo compartment has ceiling and sidewall liner     |           |
|   | panels, which are constructed of aluminum.           |           |
|   |                                                      |           |
|   | *Sources:* 121.314(a)(3); 121.367                    |           |
|   |                                                      |           |
|   | 127\. Check at an aircraft, with a Class C cargo     |           |
|   | compartment that if the cargo compartment lamps were |           |
|   | installed, each lamp must be installed so as to      |           |
|   | prevent contact between lamp bulb and cargo.         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.787(c)                        |           |
|   |                                                      |           |
|   | 128\. Check at an aircraft, with a Class C cargo     |           |
|   | compartment, that each Class C cargo and baggage     |           |
|   | compartment not occupied by crew or passengers has a |           |
|   | liner that is separate from (but may be attached to) |           |
|   | the airplane structure.                              |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(b)                        |           |
|   |                                                      |           |
|   | 129\. Check at a transport category airplane type    |           |
|   | certificated after January 1, 1958 that After March  |           |
|   | 19, 2001, each Class D compartment, regardless of    |           |
|   | volume, meets the standards of 14 CFR 25.857(c) for  |           |
|   | a Class C compartment.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.314(c); 121.367                       |           |
|   |                                                      |           |
|   | 130\. Check at a non-transport category airplane, or |           |
|   | an airplane type certificated before January 1,      |           |
|   | 1958, with a Class D cargo compartment that a fire   |           |
|   | occurring therein will be completely confined        |           |
|   | without endangering the safety of the airplane or    |           |
|   | the occupants.                                       |           |
|   |                                                      |           |
|   | *Sources:* 121.221(e); 121.367                       |           |
|   |                                                      |           |
|   | 131\. Check at a non-transport category airplane, or |           |
|   | an airplane type certificated before January 1,      |           |
|   | 1958, with a Class D cargo compartment that each     |           |
|   | Class D compartment had a means to exclude hazardous |           |
|   | quantities of smoke, flames, or noxious gases from   |           |
|   | entering any compartment occupied by the crew or     |           |
|   | passengers.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.221(e)(1); 121.367                    |           |
|   |                                                      |           |
|   | 132\. Check at a non-transport category airplane, or |           |
|   | an airplane type certificated before January 1,      |           |
|   | 1958, with a Class D cargo compartment that, in each |           |
|   | Class D compartment, ventilation and drafts are      |           |
|   | controlled within each compartment so that any fire  |           |
|   | likely to occur in the compartment will not progress |           |
|   | beyond safe limits.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.221(e)(2); 121.367                    |           |
|   |                                                      |           |
|   | 133\. Check at a non-transport category airplane, or |           |
|   | an airplane type certificated before January 1,      |           |
|   | 1958, with a Class D cargo compartment, that each    |           |
|   | Class D compartment is completely lined with         |           |
|   | fire-resistant material.                             |           |
|   |                                                      |           |
|   | *Sources:* 121.221(e)(3); 121.367                    |           |
|   |                                                      |           |
|   | 134\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that in any case where partitions       |           |
|   | between compartments have louvers or other means     |           |
|   | allowing air to flow between compartments, there was |           |
|   | a means convenient to the crew for closing the flow  |           |
|   | of air through the partitions, when necessary.       |           |
|   |                                                      |           |
|   | *Sources:* 121.219; 121.367                          |           |
|   |                                                      |           |
|   | 135\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that each Class E compartment is        |           |
|   | completely lined with fire-resistant material.       |           |
|   |                                                      |           |
|   | *Sources:* 121.221(f)(1); 121.367                    |           |
|   |                                                      |           |
|   | 136\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that each Class E compartment has a     |           |
|   | separate system of an approved type smoke or fire    |           |
|   | detector to give warning at the pilot or flight      |           |
|   | engineer station.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.221(f)(2); 121.367                    |           |
|   |                                                      |           |
|   | 137\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that each Class E compartment has a     |           |
|   | means to shut off the ventilating air flow to or     |           |
|   | within the compartment and the controls for that     |           |
|   | means must be accessible to the flight crew in the   |           |
|   | crew compartment.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.221(f)(3); 121.367                    |           |
|   |                                                      |           |
|   | 138\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that each Class E compartment has a     |           |
|   | means to exclude hazardous quantities of smoke,      |           |
|   | flames, or noxious gases from entering the flight    |           |
|   | crew compartment.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.221(f)(4); 121.367                    |           |
|   |                                                      |           |
|   | 139\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that each Class E compartment has a     |           |
|   | liner, separate from (but may be attached to) the    |           |
|   | airplane structure.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(b)                        |           |
|   |                                                      |           |
|   | 140\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that no Class E compartment contains    |           |
|   | any controls, wiring, lines, equipment, or           |           |
|   | accessories whose damage or failure would affect     |           |
|   | safe operation, unless those items are protected so  |           |
|   | that cannot be damaged by the movement of cargo in   |           |
|   | the compartment.                                     |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 141\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that no Class E compartment contains    |           |
|   | any controls, wiring, lines, equipment, or           |           |
|   | accessories whose damage or failure would affect     |           |
|   | safe operation, unless those items are protected so  |           |
|   | that their breakage or failure will not create a     |           |
|   | fire hazard.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 142\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that there is a means to prevent cargo  |           |
|   | or baggage from interfering with the functioning of  |           |
|   | the fire protective features of the compartment.     |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(2); 121.367                    |           |
|   |                                                      |           |
|   | 143\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that sources of heat within the         |           |
|   | compartment are shielded and insulated to prevent    |           |
|   | igniting the cargo or baggage.                       |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(g)                        |           |
|   |                                                      |           |
|   | 144\. Check at an aircraft with a Class E cargo      |           |
|   | compartment, that each Class E compartment is        |           |
|   | completely lined with fire-resistant material.       |           |
|   |                                                      |           |
|   | *Sources:* 121.221(f)(1); 121.367                    |           |
|   |                                                      |           |
|   | 145\. Check at the aircraft, that materials used in  |           |
|   | the construction of the compartments, including      |           |
|   | tie-down equipment, is at least flame resistant.     |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(3); 121.367                    |           |
|   |                                                      |           |
|   | 146\. Check at the aircraft, that compartments, when |           |
|   | used for storing cargo or baggage, include no        |           |
|   | controls, wiring, lines, equipment, or accessories   |           |
|   | that would upon damage or failure, affect the safe   |           |
|   | operation of the airplane unless the item is         |           |
|   | adequately shielded, isolated, or otherwise          |           |
|   | protected so that it cannot be damaged by movement   |           |
|   | of cargo in the compartment and so that damage to or |           |
|   | failure of the item would not create a fire hazard   |           |
|   | in the compartment.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(1); 121.367                    |           |
|   |                                                      |           |
|   | 147\. Check at the aircraft, that cargo or baggage   |           |
|   | will not interfere with the functioning of the       |           |
|   | fire-protective features of the compartment.         |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(2); 121.367                    |           |
|   |                                                      |           |
|   | 148\. Check at the aircraft, that when used for      |           |
|   | storing cargo or baggage, each compartment includes  |           |
|   | provisions for safeguarding against fires according  |           |
|   | to the classifications set forth in 14 CFR Part      |           |
|   | 121.221 paragraphs (b) through (f).                  |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(4); 121.367                    |           |
|   |                                                      |           |
|   | 149\. Check at the aircraft, that where partitions   |           |
|   | between compartments have louvers or other means     |           |
|   | allowing air to flow between compartments, there is  |           |
|   | a means convenient to the crew for closing the flow  |           |
|   | of air through the partitions, when necessary.       |           |
|   |                                                      |           |
|   | *Sources:* 121.219; 121.367                          |           |
|   |                                                      |           |
|   | 150\. Check at an aircraft that was converted from a |           |
|   | passenger to a Class E cargo compartment that        |           |
|   | aircraft weight and center of gravity were within    |           |
|   | the approved limits determined in 14 CFR. 25.23      |           |
|   | through 25.27, as operating limitations.             |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(21); 25.1519                   |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s inspection and         | Yes       |
| . | maintenance records show that the certificate        |           |
| 7 | holder\'s aircraft met the requirements of its       | No,       |
| . | inspection program and the program covering other    | Explain   |
|   | maintenance, preventive maintenance, and             |           |
|   | alterations? **     **                               |           |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the records repository, that for an    |           |
|   | aircraft that was manufactured in a foreign country  |           |
|   | and never issued a U.S. Airworthiness Certificate,   |           |
|   | an original export Certificate of Airworthiness      |           |
|   | exists certifying that the aircraft conforms to the  |           |
|   | type design and is in condition for safe operation   |           |
|   | from the country in which the aircraft was           |           |
|   | manufactured.                                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 21.183(c)                        |           |
|   |                                                      |           |
|   | 2\. Check, at the records repository, that for an    |           |
|   | aircraft that was manufactured in the United States  |           |
|   | and never issued a U.S. Airworthiness Certificate,   |           |
|   | an original export Certificate of Airworthiness from |           |
|   | the United States exists certifying that the         |           |
|   | aircraft conforms to the type design and is in       |           |
|   | condition for safe operation from the country in     |           |
|   | which the aircraft was manufactured.                 |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 21.183(c)                        |           |
|   |                                                      |           |
|   | 3\. Check, at the records repository, that the       |           |
|   | applicant for a standard airworthiness certificate   |           |
|   | presented evidence to the Administrator that the     |           |
|   | aircraft conforms to a type design approved under a  |           |
|   | type certificate or supplemental type certificate.   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 21.183(d)(1)                     |           |
|   |                                                      |           |
|   | 4\. Check, at the records repository, that the       |           |
|   | applicant for a standard airworthiness certificate   |           |
|   | presented evidence to the Administrator that the     |           |
|   | aircraft conforms to applicable airworthiness        |           |
|   | directives.                                          |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 21.183(d)(1)                     |           |
|   |                                                      |           |
|   | 5\. Check, at the records repository, that the       |           |
|   | aircraft, if it was not manufactured under a         |           |
|   | production or type certificate, was inspected in     |           |
|   | accordance with the performance rules for 100-hour   |           |
|   | inspections set forth in Sec. 43.15 and found        |           |
|   | airworthy by the manufacturer, a repair station      |           |
|   | certificated under Part 145, a certificated mechanic |           |
|   | or a Part 121 Certificate Holder having a            |           |
|   | maintenance and inspection organization appropriate  |           |
|   | to the aircraft type.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 21.183(a); 21.183(b);            |           |
|   | 21.183(d)(2)(i); 21.183(d)(2)(ii);                   |           |
|   | 21.183(d)(2)(iii); 21.183(d)(2)(iv)                  |           |
|   |                                                      |           |
|   | 6\. Check, at the records repository, that the       |           |
|   | aircraft weight and center of gravity was within     |           |
|   | approved limits in accordance with the Certificate   |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(20)                            |           |
|   |                                                      |           |
|   | 7\. Check, at the records repository, that the       |           |
|   | aircraft and its component parts, accessories, and   |           |
|   | appliances were maintained in accordance with the    |           |
|   | time limits for the accomplishment of the overhaul,  |           |
|   | replacement, periodic inspection, including CMRs and |           |
|   | routine checks in accordance with the Certificate    |           |
|   | Holders design.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367(a); D.072(c)                      |           |
|   |                                                      |           |
|   | 8\. Check, at the records repository, that items     |           |
|   | identified as \"on condition\" were maintained by    |           |
|   | periodic inspections, checks, service, repair,       |           |
|   | and/or preventive maintenance in accordance with the |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367(a); D.072(d)                      |           |
|   |                                                      |           |
|   | 9\. Check, at the records repository, that parts or  |           |
|   | subassemblies of components that do not have         |           |
|   | specific time intervals were checked, inspected,     |           |
|   | and/or overhauled in accordance with the Certificate |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367(a); D.072(e)                      |           |
|   |                                                      |           |
|   | 10\. Check, at the records repository, that a proof  |           |
|   | test was conducted to demonstrate the integrity of   |           |
|   | the static pressure system in accordance with the    |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1325(c)(2)                    |           |
|   |                                                      |           |
|   | 11\. Check, at the records repository, if the        |           |
|   | operator was authorized to conduct RVSM operations,  |           |
|   | that the aircraft was maintained for RVSM operations |           |
|   | in accordance with the Certificate Holder\'s design. |           |
|   |                                                      |           |
|   | *Sources:* 91 App..GSection 3(b)(1)                  |           |
|   |                                                      |           |
|   | 12\. Check, at the records repository, that the      |           |
|   | aircraft subject to supplemental structural          |           |
|   | inspections as identified in the structural          |           |
|   | inspection document was inspected in accordance with |           |
|   | the Certificate Holder\'s design.                    |           |
|   |                                                      |           |
|   | *Sources:* FAA Order 8900.1, Vol 3, Ch 43, Para      |           |
|   | 3-3869 C.                                            |           |
|   |                                                      |           |
|   | 13\. Check, at the records repository, that if the   |           |
|   | aircraft was subject to a CPCP, the CPCP tasks were  |           |
|   | accomplished in accordance with the Certificate      |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* AD 90-25-03 AD 92-22-08 R1 AD 94-18-02    |           |
|   |                                                      |           |
|   | 14\. Check, at the technical publications library,   |           |
|   | that for STC\'s that do not include instructions for |           |
|   | continued airworthiness for an appliance or product  |           |
|   | installed in the airplane, the Certificate Holder    |           |
|   | has incorporated into the maintenance program the    |           |
|   | method techniques and practices and the information  |           |
|   | essential to the continued airworthiness of the      |           |
|   | airplane in accordance with the Certificate          |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25 App..H25.1(b); 43.13(a)       |           |
|   |                                                      |           |
|   | 15\. Check, at the records repository, that the      |           |
|   | current status of all applicable airworthiness       |           |
|   | directives, includes the date and methods of         |           |
|   | compliance, and, if the airworthiness directive      |           |
|   | involves recurring action, the time and date when    |           |
|   | the next action was required in accordance with the  |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367(a); 121.380(a)(2)(vi)             |           |
|   |                                                      |           |
|   | 16\. Check, at the technical publications library,   |           |
|   | that the Certificate Holder who has an alternate     |           |
|   | means of compliance for the accomplishment of an     |           |
|   | airworthiness directive, includes the specific       |           |
|   | actions that address the unsafe condition or the     |           |
|   | change in compliance time in accordance with the     |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367(a); 39.17; 39.19                  |           |
|   |                                                      |           |
|   | 17\. Check, at the records repository, that the      |           |
|   | airplane certificated takeoff weight in excess of    |           |
|   | 12,500 pounds, that conforms to an amended or        |           |
|   | supplemental type certificate issued in accordance   |           |
|   | with SFAR No. 41 of 14 CFR part 21, that materials   |           |
|   | (including finishes or decorative surfaces applied   |           |
|   | to the materials) meet the applicable test criteria  |           |
|   | prescribed in part I of appendix F of 14 CFR part    |           |
|   | 25, or other approved equivalent methods.            |           |
|   |                                                      |           |
|   | *Sources:* 121.312(c); 121.367; 25.853(a)            |           |
|   |                                                      |           |
|   | 18\. Check at the Records Repository for an aircraft |           |
|   | that operates with an alteration limited to the      |           |
|   | installation of miscellaneous, non-required          |           |
|   | electrical equipment, that flammability requirements |           |
|   | should be met for materials used in non-electrical   |           |
|   | components, or materials external to a metal         |           |
|   | enclosure (which will contain a fire) used for       |           |
|   | electrical components.                               |           |
|   |                                                      |           |
|   | *Sources:* AC 25-10 Paragraph 5b(2)                  |           |
|   |                                                      |           |
|   | 19\. Check at the Record Repository, that each       |           |
|   | compartment, when used for storing cargo or baggage, |           |
|   | is designed so that materials used in the            |           |
|   | construction of the compartments, including tie-down |           |
|   | equipment, are at least flame resistant.             |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(3); 121.367                    |           |
|   |                                                      |           |
|   | 20\. Check at the Technical Library, that the        |           |
|   | airplane contains the specified markings and         |           |
|   | placards.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1541(a)(1)                    |           |
|   |                                                      |           |
|   | 21\. Check at the Record Repository, that for each   |           |
|   | compartment occupied by the crew or passengers,      |           |
|   | materials (including finishes or decorative surfaces |           |
|   | applied to the materials) meet the applicable test   |           |
|   | criteria prescribed in part I of appendix F of 14    |           |
|   | CFR Part 25, or other approved equivalent methods,   |           |
|   | regardless of the passenger capacity of the          |           |
|   | airplane.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(a)                        |           |
|   |                                                      |           |
|   | 22\. Check at the Record Repository, that, for each  |           |
|   | compartment occupied by the crew or passengers, seat |           |
|   | cushions, except those on flight crewmember seats,   |           |
|   | meet the test requirements of part II of appendix F  |           |
|   | of 14 CFR Part 25, or other equivalent methods,      |           |
|   | regardless of the passenger capacity of the          |           |
|   | airplane.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(c)                        |           |
|   |                                                      |           |
|   | 23\. Check at the Record Repository for an aircraft  |           |
|   | with a passenger capacity of 20 or more that each    |           |
|   | compartment occupied by the crew or passengers,      |           |
|   | partitions, other than transparent panels needed to  |           |
|   | enhance cabin safety meet the test requirements of   |           |
|   | parts IV and V of appendix F 14 CFR Part 25 or other |           |
|   | approved equivalent method.                          |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(d)(2)                     |           |
|   |                                                      |           |
|   | 24\. Check at the Record Repository for an aircraft, |           |
|   | with a passenger capacity of 20 or more, that each   |           |
|   | compartment occupied by the crew or passengers,      |           |
|   | galley structure, including exposed surfaces of      |           |
|   | stowed carts and standard containers and the cavity  |           |
|   | walls that are exposed when a full complement of     |           |
|   | such carts or containers is not carried meet the     |           |
|   | test requirements of parts IV and V of appendix F 14 |           |
|   | CFR Part 25, or other approved equivalent method.    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(d)(3)                     |           |
|   |                                                      |           |
|   | 25\. Check at the Record Repository for an aircraft, |           |
|   | with a passenger capacity of 20 or more, that each   |           |
|   | compartment occupied by the crew or passengers,      |           |
|   | large cabinets and cabin stowage compartments, other |           |
|   | than underseat stowage compartments for stowing      |           |
|   | small items such as magazines and maps meet the test |           |
|   | requirements of parts IV and V of appendix F 14 CFR  |           |
|   | Part 25, or other approved equivalent method.        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.853(d)(4)                     |           |
|   |                                                      |           |
|   | 26\. Check at the Records Repository, that for each  |           |
|   | cargo and baggage compartment not occupied by crew   |           |
|   | or passengers, flight tests were conducted to show   |           |
|   | compliance with the provisions of 14 CFR 25.857      |           |
|   | concerning compartment accessibility.                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(h)(1)                     |           |
|   |                                                      |           |
|   | 27\. Check at the Records Repository, that for each  |           |
|   | cargo and baggage compartment not occupied by crew   |           |
|   | or passengers, flight tests were conducted to show   |           |
|   | compliance with the provisions of 14 CFR 25.857      |           |
|   | concerning the entries of hazardous quantities of    |           |
|   | smoke or extinguishing agent into compartments       |           |
|   | occupied by the crew or passengers.                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(h)(1)                     |           |
|   |                                                      |           |
|   | 28\. Check at the Records Repository, that for each  |           |
|   | cargo and baggage compartment not occupied by crew   |           |
|   | or passengers, flight tests were conducted to show   |           |
|   | compliance with the provisions of 14 CFR 25.857      |           |
|   | concerning the dissipation of the extinguishing      |           |
|   | agent in Class C compartments, and that no           |           |
|   | inadvertent operation of smoke or fire detectors in  |           |
|   | any compartment would occur as a result of fire      |           |
|   | contained in any other compartment, either during or |           |
|   | after extinguishment, unless the extinguishing       |           |
|   | system floods each such compartment simultaneously.  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(h)(3)(i)                  |           |
|   |                                                      |           |
|   | 29\. Check at the Records Repository, that each      |           |
|   | emergency exit, including a flight crew emergency    |           |
|   | exit, is a movable door or hatch in the external     |           |
|   | walls of the fuselage, allowing unobstructed opening |           |
|   | to the outside, capable of being opened from the     |           |
|   | inside and the outside with the airplane in each of  |           |
|   | the attitudes corresponding to collapse of one or    |           |
|   | more legs of the landing gear.                       |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.809(a); 25.809(b)(1)          |           |
|   |                                                      |           |
|   | 30\. Check at the Records Repository, that when      |           |
|   | introducing a major change in type design, not great |           |
|   | enough to require a new application for a type       |           |
|   | certificate under Sec. 21.19 that the application    |           |
|   | was made to the Administrator for a supplemental     |           |
|   | type certificate, in a form and manner prescribed by |           |
|   | the Administrator.                                   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 21.113                           |           |
|   |                                                      |           |
|   | 31\. Check at the Records Repository, for an         |           |
|   | aircraft that operates above flight level 320, that  |           |
|   | concentration of ozone inside the cabin will not     |           |
|   | exceed 0.25 parts per million by volume, sea level   |           |
|   | equivalent, at any time above that flight level.     |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.578(b)(1)                    |           |
|   |                                                      |           |
|   | 32\. Check at the Records Repository, for an         |           |
|   | aircraft that operates above flight level 270, that  |           |
|   | concentration of ozone inside the cabin will not     |           |
|   | exceed 0.1 parts per million by volume, sea level    |           |
|   | equivalent, time-weighted average for each flight    |           |
|   | segment that exceeds 4 hours and includes flight     |           |
|   | above that flight level. (For this purpose, the      |           |
|   | amount of ozone below flight level 180 is considered |           |
|   | to be zero.)                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.578(b)(2)                    |           |
|   |                                                      |           |
|   | 33\. Check at the Records Repository, that carbon    |           |
|   | monoxide concentration in crew and passenger         |           |
|   | compartment air does not exceed 0.5 percent by       |           |
|   | volume (sea level equivalent).                       |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.831(b)(2)                     |           |
|   |                                                      |           |
|   | 34\. Check at the Records Repository for an aircraft |           |
|   | that operates at flight levels above 320, that the   |           |
|   | aircraft\'s cabin ozone concentration during flight  |           |
|   | will not to exceed 0.25 parts per million by volume, |           |
|   | sea level equivalent.                                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.832(a)(1)                     |           |
|   |                                                      |           |
|   | 35\. Check at the Records Repository for an aircraft |           |
|   | that operates at flight levels above 270 during any  |           |
|   | 3 hour interval, that the aircraft\'s cabin ozone    |           |
|   | concentration during flight will not to exceed 0.1   |           |
|   | parts per million by volume, sea level equivalent,   |           |
|   | time-weighted average.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.832(a)(2)                     |           |
|   |                                                      |           |
|   | 36\. Check at the Records Repository for an aircraft |           |
|   | that will not be operated at an altitude which would |           |
|   | result in cabin ozone concentrations exceeding the   |           |
|   | limits prescribed by paragraph 14 CFR 25.832(a), or  |           |
|   | the ventilation system, including any ozone control  |           |
|   | equipment, has been shown by analysis or tests,      |           |
|   | based on airplane operational procedures and         |           |
|   | performance limitation, that demonstrate that it     |           |
|   | will maintain cabin ozone concentrations at or below |           |
|   | the limits prescribed by 14 CFR 25.832(a).           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.832(c)(1); 25.832(c)(2)       |           |
|   |                                                      |           |
|   | 37\. Check at the Records Repository for an          |           |
|   | aircraft, that when pressurized cabins and           |           |
|   | compartments are to be occupied, are equipped to     |           |
|   | provide a cabin pressure altitude of not more than   |           |
|   | 8,000 feet at the maximum operating altitude of the  |           |
|   | airplane under normal operating conditions.          |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.841(a)                        |           |
|   |                                                      |           |
|   | 38\. Check at the Records Repository for a           |           |
|   | non-transport category airplane or an airplane type  |           |
|   | certificated before January 1, 1958, with a Class D  |           |
|   | cargo compartment, has an inspection program and     |           |
|   | program covering other maintenance, preventive       |           |
|   | maintenance and alterations that ensures that, in    |           |
|   | Class D cargo compartments all other materials used  |           |
|   | in the construction of the cargo or baggage          |           |
|   | compartment meet the applicable test criteria        |           |
|   | prescribed in 14 CFR Part 25, Part I of Appendix F   |           |
|   | or other approved equivalent methods.                |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(d)                        |           |
|   |                                                      |           |
|   | 39\. Check at the Records Repository for an aircraft |           |
|   | with a Class E cargo compartment, that flight tests  |           |
|   | were conducted to show there are means to exclude    |           |
|   | hazardous quantities of smoke, flames, or noxious    |           |
|   | gases, from the flight crew compartment.             |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(h)(2); 25.857(e)(4)       |           |
|   |                                                      |           |
|   | 40\. Check at the Record Repository, that for normal |           |
|   | operating conditions, the ventilation system         |           |
|   | provides each occupant with an airflow containing at |           |
|   | least 0.55 pounds of fresh air per minute.           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.831(a)                        |           |
|   |                                                      |           |
|   | 41\. Check at the Technical Publications Library,    |           |
|   | for instructions of continued airworthiness, for an  |           |
|   | aircraft that was converted from a passenger to a    |           |
|   | Class E cargo compartment, that were prepared in     |           |
|   | accordance with 14 CFR parts 25, Appendix H, and     |           |
|   | that were acceptable to the Administrator.           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1529                          |           |
|   |                                                      |           |
|   | 42\. Check, at the certificate holding district      |           |
|   | office, that the operator who conducts domestic,     |           |
|   | flag or commuter operations, sent a copy of the      |           |
|   | record (current list of each aircraft that it        |           |
|   | operates) and each change to the certificate-holding |           |
|   | district office in accordance with its design.       |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.685                    |           |
|   |                                                      |           |
|   | 43\. Check, at the records repository, that records  |           |
|   | containing the total time in service of the airframe |           |
|   | are kept in accordance with the Certificate          |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(i)                 |           |
|   |                                                      |           |
|   | 44\. Check, at the records repository, that records  |           |
|   | containing the time since last overhaul of all items |           |
|   | installed on the aircraft which are required to be   |           |
|   | overhauled on a specified time basis are kept in     |           |
|   | accordance with the Certificate Holder\'s design.    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(iv)                |           |
|   |                                                      |           |
|   | 45\. Check, at the records repository, that records  |           |
|   | containing the identification of the current         |           |
|   | inspection status of the aircraft, including the     |           |
|   | times since the last inspections required by the     |           |
|   | inspection program under which the aircraft and its  |           |
|   | appliances are maintained are kept in accordance     |           |
|   | with the Certificate Holder\'s design.               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(v)                 |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s inspection and         | Yes       |
| . | maintenance records show that the certificate        |           |
| 8 | holder\'s engines and parts thereof met the          | No,       |
| . | requirements of its inspection program and the       | Explain   |
|   | program covering other maintenance, preventive       |           |
|   | maintenance, and alterations? **     **              |           |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the records repository that, aircraft  |           |
|   | required to be modified to meet Stage 3 operating    |           |
|   | noise limits, were modified in accordance with the   |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 91.853                           |           |
|   |                                                      |           |
|   | 2\. Check, records repository, that a review of the  |           |
|   | Type Certificate Data Sheet for applicable           |           |
|   | airworthiness requirements to ensure that the        |           |
|   | aircraft engines meet type design was accomplished   |           |
|   | in accordance with the Certificate Holder\'s design. |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(16); 121.367; 21.41            |           |
|   |                                                      |           |
|   | 3\. Check, at the records repository, that records   |           |
|   | containing the total time in service of each engine  |           |
|   | and propeller are kept in accordance with the        |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(ii)                |           |
|   |                                                      |           |
|   | 4\. Check, at the records repository, that records   |           |
|   | containing the current status of life-limited parts  |           |
|   | of each airframe, engine, propeller, and appliance   |           |
|   | are kept in accordance with the Certificate          |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(iii)               |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s inspection and         | Yes       |
| . | maintenance records show that the certificate        |           |
| 9 | holder\'s propellers and parts thereof met the       | No,       |
| . | requirements of its inspection program and the       | Explain   |
|   | program covering other maintenance, preventive       |           |
|   | maintenance, and alterations? **     **              | Not       |
|   |                                                      | A         |
|   | *Related Performance JTIs:*                          | pplicable |
|   |                                                      |           |
|   | 1\. Check, at the records repository, that records   |           |
|   | containing the total time in service of each engine  |           |
|   | and propeller are kept in accordance with the        |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(ii)                |           |
|   |                                                      |           |
|   | 2\. Check, at the records repository, that records   |           |
|   | containing the current status of life-limited parts  |           |
|   | of each airframe, engine, propeller, and appliance   |           |
|   | are kept in accordance with the Certificate          |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(iii)               |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s inspection and         | Yes       |
| . | maintenance records show that the certificate        |           |
| 1 | holder\'s appliances and parts thereof met the       | No,       |
| 0 | requirements of its inspection program and the       | Explain   |
| . | program covering other maintenance, preventive       |           |
|   | maintenance, and alterations? **     **              |           |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the records repository, that within    |           |
|   | the preceding 24 calendar months, the ATC            |           |
|   | transponder was tested and inspected in accordance   |           |
|   | with the Certificate Holder\'s design.               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 91.413(a)                        |           |
|   |                                                      |           |
|   | 2\. Check, at the records repository that, if there  |           |
|   | was an aircraft registration number change, the      |           |
|   | discrete aircraft address for the Mode S transponder |           |
|   | that identifies the aircraft was obtained from the   |           |
|   | appropriate airworthiness authority.                 |           |
|   |                                                      |           |
|   | *Sources:* AC 20-131A Paragraph 3 c (1)              |           |
|   |                                                      |           |
|   | 3\. Check, at the records repository, that           |           |
|   | documentation established compliance with the        |           |
|   | applicable RVSM aircraft requirements and the        |           |
|   | conformity tests used to ensure that aircraft        |           |
|   | approved with the data package meet the RVSM         |           |
|   | aircraft requirements.                               |           |
|   |                                                      |           |
|   | *Sources:* 91 App..GSection 2(b)(1); 91              |           |
|   | App..GSection 2(b)(2)                                |           |
|   |                                                      |           |
|   | 4\. Check, at the records repository, that the       |           |
|   | aircraft complies with appropriate flight recorder   |           |
|   | requirements applicable to that aircraft in          |           |
|   | accordance with the Certificate Holder\'s design.    |           |
|   |                                                      |           |
|   | *Sources:* 121.343(c)(1)thru(11);                    |           |
|   | 121.343(d)(1)thru(17); 121.343(e); 121.343(f);       |           |
|   | 121.344(a)(1)thru(88); 121.344(b)(1);                |           |
|   | 121.344(b)(1)(i); 121.344(b)(2); 121.344(b)(2);      |           |
|   | 121.344(c)(1); 121.344(c)(2); 121.344(d)(1);         |           |
|   | 121.344(e)(1); 121.344(f)(1); 121.344a(a)(1);        |           |
|   | 121.344a(a)(2); 121.344a(b)(1); 121.344a(c); 121.367 |           |
|   |                                                      |           |
|   | 5\. Check, at the technical publications library,    |           |
|   | that airspeed limitation information was expressed   |           |
|   | in knots.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.303(c); 121.367                       |           |
|   |                                                      |           |
|   | 6\. Check, at the technical publication library,     |           |
|   | that powerplant limitations information, that was    |           |
|   | appropriate to the airplane, necessary for marking   |           |
|   | the instruments required by Section 25.1549, was     |           |
|   | furnished, verified, and approved and was            |           |
|   | segregated, identified, and clearly distinguished    |           |
|   | from each unapproved part of that manual.            |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.1581(b); 25.1583(b)(3)        |           |
|   |                                                      |           |
|   | 7\. Check, at the records repository, that records   |           |
|   | containing the identification of the current         |           |
|   | inspection status of the aircraft, including the     |           |
|   | times since the last inspections required by the     |           |
|   | inspection program under which the aircraft and its  |           |
|   | appliances are maintained are kept in accordance     |           |
|   | with the Certificate Holder\'s design.               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(v)                 |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s inspection and         | Yes       |
| . | maintenance records show that the certificate        |           |
| 1 | holder\'s emergency equipment and parts thereof met  | No,       |
| 1 | the requirements of its inspection program and the   | Explain   |
| . | program covering other maintenance, preventive       |           |
|   | maintenance, and alterations? **     **              |           |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check at the records repository for an aircraft, |           |
|   | that operates in extended overwater operations, that |           |
|   | batteries used in the approved survival type         |           |
|   | emergency locator transmitter, are replaced (or      |           |
|   | recharged, if the battery was rechargeable) when the |           |
|   | transmitter has been in use for more than 1          |           |
|   | cumulative hour, or when 50 percent of their useful  |           |
|   | life (or for rechargeable batteries, 50 percent of   |           |
|   | their useful life of charge) has expired.            |           |
|   |                                                      |           |
|   | *Sources:* 121.339(a)(4); 121.367                    |           |
|   |                                                      |           |
|   | 2\. Check at the records repository for an aircraft, |           |
|   | that operates in extended overwater operations, that |           |
|   | each approved survival type emergency locator        |           |
|   | transmitter was inspected regularly in accordance    |           |
|   | with inspection periods established in the           |           |
|   | operations specifications to ensure its condition    |           |
|   | for continued serviceability and immediate readiness |           |
|   | to perform its intended emergency purposes.          |           |
|   |                                                      |           |
|   | *Sources:* 121.309(b)(1); 121.339(a)(4); 121.367     |           |
|   |                                                      |           |
|   | 3\. Check at the Records Repository, that each hand  |           |
|   | fire extinguisher for use in each Class A cargo      |           |
|   | compartment was inspected regularly in accordance    |           |
|   | with inspection periods established in the           |           |
|   | operations specifications to ensure its condition    |           |
|   | for continued serviceability and immediate readiness |           |
|   | to perform its intended emergency purposes.          |           |
|   |                                                      |           |
|   | *Sources:* 121.221(b)(2); 121.309(b)(1); 121.367     |           |
|   |                                                      |           |
|   | 4\. Check at the Record Repository, that each hand   |           |
|   | fire extinguisher for use in each Class B cargo      |           |
|   | compartment was inspected regularly in accordance    |           |
|   | with inspection periods established in the           |           |
|   | operations specifications to ensure its condition    |           |
|   | for continued serviceability and immediate readiness |           |
|   | to perform its intended emergency purposes.          |           |
|   |                                                      |           |
|   | *Sources:* 121.221(c)(2); 121.309(b)(1); 121.367     |           |
+---+------------------------------------------------------+-----------+
| 1 | Did the certificate holder\'s inspection and         | Yes       |
| . | maintenance records show that the certificate        |           |
| 1 | holder\'s airframe and parts thereof met the         | No,       |
| 2 | requirements of its inspection program and the       | Explain   |
| . | program covering other maintenance, preventive       |           |
|   | maintenance, and alterations? **     **              |           |
|   |                                                      |           |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the records repository, that           |           |
|   | documentation established compliance with the        |           |
|   | applicable RVSM aircraft requirements and the        |           |
|   | conformity tests used to ensure that aircraft        |           |
|   | approved with the data package meet the RVSM         |           |
|   | aircraft requirements.                               |           |
|   |                                                      |           |
|   | *Sources:* 91 App..GSection 2(b)(1); 91              |           |
|   | App..GSection 2(b)(2)                                |           |
|   |                                                      |           |
|   | 2\. Check, at the records repository, that the       |           |
|   | Certificate Holder has a list of current major       |           |
|   | alterations for that airframe, engine, propeller, or |           |
|   | appliance in accordance with the Certificate         |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.380(a)(2)(vii)               |           |
|   |                                                      |           |
|   | 3\. Check, at the records repository, that major     |           |
|   | alteration and/or major repairs have been            |           |
|   | accomplished in accordance with technical data       |           |
|   | approved by the Administrator in accordance with the |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* AC 120-77 paragraph 9(c)                  |           |
|   |                                                      |           |
|   | 4\. Check, at the technical publications library,    |           |
|   | that repair assessment guidelines applicable to the  |           |
|   | fuselage pressure boundary (fuselage skin, door      |           |
|   | skin, and bulkhead webs), were incorporated in its   |           |
|   | maintenance program in accordance with the           |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 121.370(a)(1); 121.370(a)(10);   |           |
|   | 121.370(a)(11); 121.370(a)(12); 121.370(a)(2);       |           |
|   | 121.370(a)(3); 121.370(a)(4); 121.370(a)(5);         |           |
|   | 121.370(a)(6); 121.370(a)(7); 121.370(a)(8);         |           |
|   | 121.370(a)(9)                                        |           |
|   |                                                      |           |
|   | 5\. Check, at the records repository, that a survey  |           |
|   | of the structure of each airplane for structural     |           |
|   | repairs without accompanying documentation was       |           |
|   | accomplished in accordance with the Certificate      |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* AC 120-73 Paragraph 5a(1)(a)              |           |
|   |                                                      |           |
|   | 6\. Check, at the records repository, that an STC    |           |
|   | involving an increase in passenger seating for which |           |
|   | the airplane was type certificated meets the         |           |
|   | requirements of CFR 25.2(a).                         |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.2(a)                          |           |
|   |                                                      |           |
|   | 7\. Check, at the records repository, that an STC    |           |
|   | for an aircraft manufactured after October 16, 1987, |           |
|   | involving an increase in passenger seating for which |           |
|   | the airplane was type certificated meets the         |           |
|   | requirements of CFR 25.2(a) and (b).                 |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.2(a); 25.2(b)                 |           |
|   |                                                      |           |
|   | 8\. Check, at the records repository that the        |           |
|   | aircraft was painted using methods, techniques, and  |           |
|   | practices prescribed in the current manufacturer\'s  |           |
|   | maintenance manual or Instructions for Continued     |           |
|   | Airworthiness in accordance with the Certificate     |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 43.13(a)                         |           |
|   |                                                      |           |
|   | 9\. Check, at the records repository that the        |           |
|   | aircraft was painted using materials of such a       |           |
|   | quality, that the condition of the aircraft,         |           |
|   | airframe, aircraft engine, propeller, or appliance   |           |
|   | painted will be at least equal to its original or    |           |
|   | properly altered condition in accordance with the    |           |
|   | Certificate Holder\'s design.                        |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 43.13(b)                         |           |
|   |                                                      |           |
|   | 10\. Check, at the records repository, that flight   |           |
|   | controls that were painted were statically balanced  |           |
|   | if required in accordance with the Certificate       |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* AC 120-27C Paragraph 15                   |           |
|   |                                                      |           |
|   | 11\. Check at the Records Repository, that aircraft  |           |
|   | structure is designed to give each occupant every    |           |
|   | reasonable chance of escaping serious injury in a    |           |
|   | minor crash landing when the occupant experiences    |           |
|   | upward, 3.0g inertia forces relative to the          |           |
|   | surrounding structure.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.561(b)(3)(i)                  |           |
|   |                                                      |           |
|   | 12\. Check at the Records Repository, that aircraft  |           |
|   | structure is designed to give each occupant every    |           |
|   | reasonable chance of escaping serious injury in a    |           |
|   | minor crash landing when the occupant experiences    |           |
|   | forward, 9.0g relative to the surrounding structure. |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.561(b)(3)(ii)                 |           |
|   |                                                      |           |
|   | 13\. Check at the Records Repository, that aircraft  |           |
|   | structure is designed to give each occupant every    |           |
|   | reasonable chance of escaping serious injury in a    |           |
|   | minor crash landing when the occupant experiences    |           |
|   | sideward, 3.0g on the airframe.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.561(b)(3)(iii)                |           |
|   |                                                      |           |
|   | 14\. Check at the Records Repository, that aircraft  |           |
|   | structure is designed to give each occupant every    |           |
|   | reasonable chance of escaping serious injury in a    |           |
|   | minor crash landing when the occupant experiences    |           |
|   | sideward, 4.0g on the seats and their attachments.   |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.561(b)(3)(iii)                |           |
|   |                                                      |           |
|   | 15\. Check at the Records Repository, that aircraft  |           |
|   | structure is designed to give each occupant every    |           |
|   | reasonable chance of escaping serious injury in a    |           |
|   | minor crash landing when the occupant experiences    |           |
|   | downward, 6.0g relative to the surrounding           |           |
|   | structure.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.561(b)(3)(iv)                 |           |
|   |                                                      |           |
|   | 16\. Check at the Records Repository, that aircraft  |           |
|   | structure is designed to give each occupant every    |           |
|   | reasonable chance of escaping serious injury in a    |           |
|   | minor crash landing when the occupant experiences    |           |
|   | rearward, 1.5g relative to the surrounding           |           |
|   | structure.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.561(b)(3)(v)                  |           |
|   |                                                      |           |
|   | 17\. Check at the Records Repository, that an        |           |
|   | approved cargo bin that was attached to the seat     |           |
|   | tracks or to the floor structure of the airplane,    |           |
|   | and its attachment must withstand the load factors   |           |
|   | and emergency landing conditions applicable to the   |           |
|   | passenger seats of the airplane in which the bin was |           |
|   | installed, multiplied by either the factor 1.15 or   |           |
|   | the seat attachment factor specified for the         |           |
|   | airplane, whichever was greater, using the combined  |           |
|   | weight of the bin and the maximum weight of cargo    |           |
|   | that may be carried in the bin.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.285(b)(4); 121.367                    |           |
|   |                                                      |           |
|   | 18\. Check at the Records Repository, that each      |           |
|   | airplane has an emergency lighting system,           |           |
|   | independent of the main lighting system that         |           |
|   | provides enough general lighting in the passenger    |           |
|   | cabin so that the average illumination when measured |           |
|   | at 40-inch intervals at seat armrest height, on the  |           |
|   | centerline of the main passenger aisle, is at least  |           |
|   | 0.05 foot-candles.                                   |           |
|   |                                                      |           |
|   | *Sources:* 121.310(c)(2); 121.367                    |           |
|   |                                                      |           |
|   | 19\. Check at the Records Repository, that each      |           |
|   | interphone restraint system is designed so that when |           |
|   | subjected to the load factors specified in 14 CFR    |           |
|   | 25.561(b)(3), the interphone will remain in its      |           |
|   | stowed position.                                     |           |
|   |                                                      |           |
|   | *Sources:* 121.367(b); 25.789(b)                     |           |
|   |                                                      |           |
|   | 20\. Check at the Records Repository, that the       |           |
|   | structure is designed to give each occupant every    |           |
|   | reasonable chance of escaping serious injury in a    |           |
|   | minor crash landing when the occupant experiences    |           |
|   | forward, 9.0g inertia forces relative to the         |           |
|   | surrounding structure.                               |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.561(b)(3)(ii)                 |           |
|   |                                                      |           |
|   | 21\. Check at the Records Repository, that the entry |           |
|   | of hazardous quantities of smoke or extinguishing    |           |
|   | agent into compartments occupied by the crew or      |           |
|   | passengers, was shown by tests in flight that no     |           |
|   | inadvertent operation of smoke or fire detectors in  |           |
|   | other compartments within the airplane would occur   |           |
|   | as a result of fire contained in any one             |           |
|   | compartment, either during the time it is being      |           |
|   | extinguished, or thereafter, unless the              |           |
|   | extinguishing system floods those compartments       |           |
|   | simultaneously.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.323(a); 121.367                       |           |
|   |                                                      |           |
|   | 22\. Check at the Records Repository, that the entry |           |
|   | of hazardous quantities of smoke or extinguishing    |           |
|   | agent into compartments occupied by the crew or      |           |
|   | passengers, and the dissipation of the extinguishing |           |
|   | agent in Class \"C\" compartments was shown by tests |           |
|   | in flight that no inadvertent operation of smoke or  |           |
|   | fire detectors in other compartments within the      |           |
|   | airplane would occur as a result of fire contained   |           |
|   | in any one compartment, either during the time it is |           |
|   | being extinguished, or thereafter, unless the        |           |
|   | extinguishing system floods those compartments       |           |
|   | simultaneously.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.323(a); 121.367                       |           |
|   |                                                      |           |
|   | 23\. Check at the Records Repository for an aircraft |           |
|   | with a Class C cargo compartment, that each class C  |           |
|   | cargo compartment was designed to exclude hazardous  |           |
|   | quantities of smoke, flames, or extinguishing agents |           |
|   | from entering into any compartment occupied by the   |           |
|   | crew or passengers.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.221(d)(3); 121.367                    |           |
|   |                                                      |           |
|   | 24\. Check at the Record Repository for an aircraft  |           |
|   | type certificated after January 1, 1958 with a Class |           |
|   | C cargo compartment, that is greater than 200 cubic  |           |
|   | feet in volume, that each class C cargo compartment  |           |
|   | has ceiling and sidewall liner panels which are      |           |
|   | constructed of glass fiber reinforced resin, or meet |           |
|   | the test requirements of 14 CFR part 25, appendix F, |           |
|   | part III.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.314(a)(1); 121.314(a)(2); 121.367     |           |
|   |                                                      |           |
|   | 25\. Check at the Record Repository for a transport  |           |
|   | category aircraft, type certificated after January   |           |
|   | 1, 1958 with a Class C cargo compartment, that is    |           |
|   | greater than 200 cubic feet in volume, that has      |           |
|   | liner installations approved prior to March 20, 1989 |           |
|   | that each class C cargo compartment has ceiling and  |           |
|   | sidewall liner panels which are constructed of       |           |
|   | aluminum.                                            |           |
|   |                                                      |           |
|   | *Sources:* 121.314(a)(3); 121.367                    |           |
|   |                                                      |           |
|   | 26\. Check at the Records Repository for an          |           |
|   | aircraft, with a Class C cargo compartment, that the |           |
|   | ceiling and sidewall liner panels of Class C         |           |
|   | compartments meet the test requirements of 14 CFR    |           |
|   | parts 25, Part III of Appendix F or other approved   |           |
|   | equivalent methods.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(c)                        |           |
|   |                                                      |           |
|   | 27\. Check at the Records Repository for an          |           |
|   | aircraft, with a Class C cargo compartment that all  |           |
|   | other materials used in the construction of the      |           |
|   | cargo or baggage compartment meet the applicable     |           |
|   | test criteria prescribed in 14 CFR 25, Part I of     |           |
|   | Appendix F or other approved equivalent methods.     |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(d)                        |           |
|   |                                                      |           |
|   | 28\. Check at the Records Repository for a transport |           |
|   | category airplane type certificated after January 1, |           |
|   | 1958 that After March 19, 2001, each Class D         |           |
|   | compartment, regardless of volume, meets the         |           |
|   | standards of 14 CFR 25.857(c) for a Class C          |           |
|   | compartment.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.314(c); 121.367                       |           |
|   |                                                      |           |
|   | 29\. Check at the Records Repository for a           |           |
|   | non-transport category airplane or an airplane type  |           |
|   | certificated before January 1, 1958, with a Class D  |           |
|   | cargo compartment, that in each Class D cargo        |           |
|   | compartments, the entry of hazardous quantities of   |           |
|   | smoke or extinguishing agent into compartments       |           |
|   | occupied by the crew or passengers was shown by      |           |
|   | tests in flight that no inadvertent operation of     |           |
|   | smoke or fire detectors in other compartments within |           |
|   | the airplane would occur as a result of fire         |           |
|   | contained in any one compartment, either during the  |           |
|   | time it is being extinguished, or thereafter, unless |           |
|   | the extinguishing system floods those compartments   |           |
|   | simultaneously.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.367                                   |           |
|   |                                                      |           |
|   | 30\. Check at the Records Repository for an aircraft |           |
|   | with a Class E cargo compartment, that each Class E  |           |
|   | compartment has been shown by tests in flight, that  |           |
|   | no inadvertent operation of smoke or fire detectors  |           |
|   | in other compartments within the airplane would      |           |
|   | occur as a result of fire contained in any one       |           |
|   | compartment, either during the time it is being      |           |
|   | extinguished, or thereafter, unless the              |           |
|   | extinguishing system floods those compartments       |           |
|   | simultaneously.                                      |           |
|   |                                                      |           |
|   | *Sources:* 121.223; 121.367                          |           |
|   |                                                      |           |
|   | 31\. Check at the Records Repository for an aircraft |           |
|   | with a Class E cargo compartment, that in each Class |           |
|   | E compartment, all other materials used in the       |           |
|   | construction of the cargo or baggage compartment     |           |
|   | meet the applicable test criteria prescribed in 14   |           |
|   | CFR 25, Part I of Appendix F or other approved       |           |
|   | equivalent methods.                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.855(d)                        |           |
|   |                                                      |           |
|   | 32\. Check at the Records Repository, that materials |           |
|   | used in the construction of the compartments,        |           |
|   | including tie-down equipment, is at least flame      |           |
|   | resistant.                                           |           |
|   |                                                      |           |
|   | *Sources:* 121.221(a)(3); 121.367                    |           |
|   |                                                      |           |
|   | 33\. Check at the Records Repository for a transport |           |
|   | category airplane, with passenger seating capacity   |           |
|   | of 20 or more, manufactured after August 19, 1988,   |           |
|   | but prior to August 20, 1990, that all materials in  |           |
|   | each compartment used by the crewmembers and         |           |
|   | passengers complies with the heat release rate       |           |
|   | testing provisions of 14 CFR 25.853(d), except that  |           |
|   | the total heat release over the first 2 minutes of   |           |
|   | sample exposure must not exceed 100 kilowatt minutes |           |
|   | per square meter and the peak heat release rate must |           |
|   | not exceed 100 kilowatts per square meter.           |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(1)(i); 121.367                 |           |
|   |                                                      |           |
|   | 34\. Check at the Records Repository for a transport |           |
|   | category airplane, type certificated before January  |           |
|   | 1, 1965, with passenger seating capacity of 20 or    |           |
|   | more, manufactured after August 19, 1988, but prior  |           |
|   | to August 20, 1990, all materials in each            |           |
|   | compartment used by the crewmembers and passengers   |           |
|   | complies with the heat release rate testing          |           |
|   | provisions of 14 CFR 25.853(d), except that the      |           |
|   | total heat release over the first 2 minutes of       |           |
|   | sample exposure must not exceed 100 kilowatt minutes |           |
|   | per square meter and the peak heat release rate must |           |
|   | not exceed 100 kilowatts per square meter.           |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(1)(i); 121.367                 |           |
|   |                                                      |           |
|   | 35\. Check at the Records Repository for a transport |           |
|   | category airplane, with passenger seating capacity   |           |
|   | of 20 or more, manufactured after August 19, 1990,   |           |
|   | that all materials in each compartment used by the   |           |
|   | crewmembers and passengers complies with the heat    |           |
|   | release rate testing provisions of Sec. 25.853(d) in |           |
|   | effect March 6, 1995, except that the total heat     |           |
|   | release over the first 2 minutes of sample exposure  |           |
|   | must not exceed 100 kilowatt minutes per square      |           |
|   | meter and the peak heat release rate must not exceed |           |
|   | 100 kilowatts per square meter.                      |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(1)(ii); 121.367                |           |
|   |                                                      |           |
|   | 36\. Check at the Records Repository for a transport |           |
|   | category airplane, type certificated before January  |           |
|   | 1, 1965, with passenger seating capacity of 20 or    |           |
|   | more, manufactured after August 19, 1990, but prior  |           |
|   | to August 20, 1990, that all materials in each       |           |
|   | compartment used by the crewmembers and passengers   |           |
|   | complies with the heat release rate testing          |           |
|   | provisions of 14 CFR 25.853(d).                      |           |
|   |                                                      |           |
|   | *Sources:* 121.312(a)(1)(ii); 121.367                |           |
|   |                                                      |           |
|   | 37\. Check at the Records Repository for an aircraft |           |
|   | that was converted from a passenger to a Class E     |           |
|   | cargo compartment that aircraft weight and center of |           |
|   | gravity were within the approved limits determined   |           |
|   | in 14 CFR. 25.23 through 25.27, as operating         |           |
|   | limitations.                                         |           |
|   |                                                      |           |
|   | *Sources:* 121.135(b)(21); 25.1519                   |           |
+---+------------------------------------------------------+-----------+
| 2 | Were the certificate holder\'s policies, procedures, | Yes       |
| \ | instructions, and information for the Aircraft       |           |
| . | Airworthiness process, followed? **     **           | No,       |
|   |                                                      | Explain   |
|   | *Related Performance JTIs:*                          |           |
|   |                                                      |           |
|   | 1\. Check, at the aircraft with two type III exits   |           |
|   | in each side of the fuselage that are separated by   |           |
|   | fewer than three passenger seat rows, that combined  |           |
|   | maximum number of passenger seats was not more than  |           |
|   | 65.                                                  |           |
|   |                                                      |           |
|   | *Sources:* 121.367; 25.807(g)(7)                     |           |
|   |                                                      |           |
|   | 2\. Check at the Technical Publications Library,     |           |
|   | that the operator, who conducts domestic, flag or    |           |
|   | commuter operations, obtained operations             |           |
|   | specifications containing type of aircraft,          |           |
|   | registration markings, and serial numbers of each    |           |
|   | aircraft authorized for use were obtained in         |           |
|   | accordance with the Certificate Holder\'s design.    |           |
|   |                                                      |           |
|   | *Sources:* 119.49(a)(4); 121.135(a)(1); 121.685      |           |
|   |                                                      |           |
|   | 3\. Check at the Technical Publications Library,     |           |
|   | that the operator, who conducts supplemental         |           |
|   | operations, obtained operations specifications       |           |
|   | containing type of aircraft, registration markings,  |           |
|   | and serial numbers of each aircraft authorized for   |           |
|   | use were obtained in accordance with the Certificate |           |
|   | Holder\'s design.                                    |           |
|   |                                                      |           |
|   | *Sources:* 119.49(b)(4); 121.135(a)(1)               |           |
|   |                                                      |           |
|   | 4\. Check, at the certificate holding district       |           |
|   | office, that the operator who conducts domestic,     |           |
|   | flag or commuter operations, sent a copy of the      |           |
|   | record (current list of each aircraft that it        |           |
|   | operates) and each change to the certificate-holding |           |
|   | district office in accordance with its design.       |           |
|   |                                                      |           |
|   | *Sources:* 121.135(a)(1); 121.685                    |           |
+---+------------------------------------------------------+-----------+
| 3 | Were the Aircraft Airworthiness process controls     | Yes       |
| \ | followed? **     **                                  |           |
| . |                                                      | No,       |
|   |                                                      | Explain   |
+---+------------------------------------------------------+-----------+
| 4 | Did the records for the Aircraft Airworthiness       | Yes       |
| \ | process comply with the instructions provided by the |           |
| . | certificate holder? **     **                        | No,       |
|   |                                                      | Explain   |
+---+------------------------------------------------------+-----------+
| 5 | Were the process measurements for the Aircraft       | Yes       |
| \ | Airworthiness process effective in identifying       |           |
| . | problems or potential problems and providing         | No,       |
|   | corrective action for them? **     **                | Explain   |
+---+------------------------------------------------------+-----------+
| 6 | Did personnel properly handle the associated         | Yes       |
| \ | interfaces by complying with other written policies, |           |
| . | procedures, instructions, and information that are   | No,       |
|   | related to this element? **     **                   | Explain   |
+---+------------------------------------------------------+-----------+

+---+-------------------------------------------------------------------+
| # |                                                                   |
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|   |                                                                   |
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| o |                                                                   |
| n |                                                                   |
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|   |                                                                   |
| - |                                                                   |
|   |                                                                   |
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| f |                                                                   |
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|   |                                                                   |
| O |                                                                   |
| b |                                                                   |
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| r |                                                                   |
| v |                                                                   |
| a |                                                                   |
| b |                                                                   |
| l |                                                                   |
| e |                                                                   |
| s |                                                                   |
|   |                                                                   |
| * |                                                                   |
| * |                                                                   |
| D |                                                                   |
| r |                                                                   |
| o |                                                                   |
| p |                                                                   |
| - |                                                                   |
| D |                                                                   |
| o |                                                                   |
| w |                                                                   |
| n |                                                                   |
| M |                                                                   |
| e |                                                                   |
| n |                                                                   |
| u |                                                                   |
| * |                                                                   |
| * |                                                                   |
+---+-------------------------------------------------------------------+
| 1 | Personnel.                                                        |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 2 | Tools and Equipment.                                              |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 3 | Technical Data.                                                   |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 4 | Procedures, policies or instructions or information.              |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 5 | Materials.                                                        |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 6 | Facilities.                                                       |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 7 | Controls.                                                         |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 8 | Process Measures.                                                 |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 9 | Interfaces.                                                       |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 1 | Desired Outcome.                                                  |
| 0 |                                                                   |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 1 | Other.                                                            |
| 1 |                                                                   |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+

+---+-------------------------------------------------------------------+
| * |                                                                   |
| * |                                                                   |
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| s |                                                                   |
| * |                                                                   |
| * |                                                                   |
+---+-------------------------------------------------------------------+
| * |                                                                   |
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| s |                                                                   |
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| m |                                                                   |
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| t |                                                                   |
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| n |                                                                   |
| s |                                                                   |
| i |                                                                   |
| b |                                                                   |
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| l |                                                                   |
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| y |                                                                   |
| . |                                                                   |
| ) |                                                                   |
+---+-------------------------------------------------------------------+
| # |                                                                   |
| # |                                                                   |
|   |                                                                   |
| T |                                                                   |
| a |                                                                   |
| s |                                                                   |
| k |                                                                   |
| s |                                                                   |
+---+-------------------------------------------------------------------+
|   | To meet this objective, the inspector must accomplish the         |
|   | following tasks:                                                  |
+---+-------------------------------------------------------------------+
|   | NOTE: If no personnel or major program changes (as defined by the |
|   | principal inspector (PI)) affecting the responsibility or         |
|   | authority attributes for this element have occurred since the     |
|   | last SAI and/or EPI was accomplished, then do not perform tasks   |
|   | 3-6. Answer questions 1 and 2, below, and provide the name/title. |
+---+-------------------------------------------------------------------+
| 1 | Identify the person who has overall responsibility for the        |
| \ | Aircraft Airworthiness process.                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 2 | Identify the person who has overall authority for the Aircraft    |
| \ | Airworthiness process.                                            |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 3 | Review the duties and responsibilities for those who manage the   |
| \ | Aircraft Airworthiness process.                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 4 | Review the appropriate organizational chart.                      |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 5 | Discuss the Aircraft Airworthiness process with the management    |
| \ | personnel identified in tasks 1 and 2.                            |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 6 | Evaluate the qualifications and work experience of the management |
| \ | personnel identified in tasks 1 and 2.                            |
| . |                                                                   |
+---+-------------------------------------------------------------------+

+---+------------------------------------------------------+-----------+
| # |                                                      |           |
| # |                                                      |           |
|   |                                                      |           |
| Q |                                                      |           |
| u |                                                      |           |
| e |                                                      |           |
| s |                                                      |           |
| t |                                                      |           |
| i |                                                      |           |
| o |                                                      |           |
| n |                                                      |           |
| s |                                                      |           |
+---+------------------------------------------------------+-----------+
|   | To meet this objective, the inspector must answer    |           |
|   | the following questions:                             |           |
+---+------------------------------------------------------+-----------+
| 1 | Is there a clearly identified person who is          | Yes       |
| \ | responsible for the quality of the Aircraft          |           |
| . | Airworthiness process? **     **                     | No,       |
|   |                                                      | Explain   |
|   |                                                      |           |
|   |                                                      | Na        |
|   |                                                      | me/Title: |
|   |                                                      |           |
|   |                                                      |           |
+---+------------------------------------------------------+-----------+
| 2 | Is there a clearly identified person who has         | Yes       |
| \ | authority to establish and modify the certificate    |           |
| . | holder\'s policies, procedures, instructions, and    | No,       |
|   | information for the Aircraft Airworthiness process?  | Explain   |
|   | **     **                                            |           |
|   |                                                      | Na        |
|   |                                                      | me/Title: |
|   |                                                      |           |
|   |                                                      |           |
+---+------------------------------------------------------+-----------+
| 3 | Does the responsible person know that he/she has     | Yes       |
| \ | responsibility for the Aircraft Airworthiness        |           |
| . | process? **     **                                   | No,       |
|   |                                                      | Explain   |
|   |                                                      |           |
|   |                                                      | No Change |
+---+------------------------------------------------------+-----------+
| 4 | Does the person with authority know that he/she has  | Yes       |
| \ | authority for the Aircraft Airworthiness process?    |           |
| . | **     **                                            | No,       |
|   |                                                      | Explain   |
|   |                                                      |           |
|   |                                                      | No Change |
+---+------------------------------------------------------+-----------+
| 5 | Does the person with responsibility for the Aircraft | Yes       |
| \ | Airworthiness process meet the qualification         |           |
| . | standards? **     **                                 | No,       |
|   |                                                      | Explain   |
|   |                                                      |           |
|   |                                                      | No Change |
+---+------------------------------------------------------+-----------+
| 6 | Does the person with authority to establish and      | Yes       |
| \ | modify the Aircraft Airworthiness process meet the   |           |
| . | qualification standards? **     **                   | No,       |
|   |                                                      | Explain   |
|   |                                                      |           |
|   |                                                      | No Change |
+---+------------------------------------------------------+-----------+
| 7 | Does the person with responsibility understand the   | Yes       |
| \ | controls, process measurements, and interfaces       |           |
| . | associated with the Aircraft Airworthiness process?  | No,       |
|   | **     **                                            | Explain   |
|   |                                                      |           |
|   |                                                      | No Change |
+---+------------------------------------------------------+-----------+
| 8 | Does the person with authority understand the        | Yes       |
| \ | controls, process measurements, and interfaces       |           |
| . | associated with the Aircraft Airworthiness process?  | No,       |
|   | **     **                                            | Explain   |
|   |                                                      |           |
|   |                                                      | No Change |
+---+------------------------------------------------------+-----------+
| 9 | Does the responsible person know who has authority   | Yes       |
| \ | to establish and modify the Aircraft Airworthiness   |           |
| . | process? **     **                                   | No,       |
|   |                                                      | Explain   |
|   |                                                      |           |
|   |                                                      | No Change |
+---+------------------------------------------------------+-----------+
| 1 | Does the individual with authority know who has the  | Yes       |
| 0 | responsibility for the Aircraft Airworthiness        |           |
| \ | process? **     **                                   | No,       |
| . |                                                      | Explain   |
|   |                                                      |           |
|   |                                                      | No Change |
+---+------------------------------------------------------+-----------+

+---+-------------------------------------------------------------------+
| # |                                                                   |
| # |                                                                   |
| # |                                                                   |
| # |                                                                   |
|   |                                                                   |
| E |                                                                   |
| P |                                                                   |
| I |                                                                   |
|   |                                                                   |
| S |                                                                   |
| e |                                                                   |
| c |                                                                   |
| t |                                                                   |
| i |                                                                   |
| o |                                                                   |
| n |                                                                   |
|   |                                                                   |
| 2 |                                                                   |
|   |                                                                   |
| - |                                                                   |
|   |                                                                   |
| M |                                                                   |
| a |                                                                   |
| n |                                                                   |
| a |                                                                   |
| g |                                                                   |
| e |                                                                   |
| m |                                                                   |
| e |                                                                   |
| n |                                                                   |
| t |                                                                   |
|   |                                                                   |
| R |                                                                   |
| e |                                                                   |
| s |                                                                   |
| p |                                                                   |
| o |                                                                   |
| n |                                                                   |
| s |                                                                   |
| i |                                                                   |
| b |                                                                   |
| i |                                                                   |
| l |                                                                   |
| i |                                                                   |
| t |                                                                   |
| y |                                                                   |
|   |                                                                   |
| & |                                                                   |
|   |                                                                   |
| A |                                                                   |
| u |                                                                   |
| t |                                                                   |
| h |                                                                   |
| o |                                                                   |
| r |                                                                   |
| i |                                                                   |
| t |                                                                   |
| y |                                                                   |
|   |                                                                   |
| O |                                                                   |
| b |                                                                   |
| s |                                                                   |
| e |                                                                   |
| r |                                                                   |
| v |                                                                   |
| a |                                                                   |
| b |                                                                   |
| l |                                                                   |
| e |                                                                   |
| s |                                                                   |
|   |                                                                   |
| * |                                                                   |
| * |                                                                   |
| D |                                                                   |
| r |                                                                   |
| o |                                                                   |
| p |                                                                   |
| - |                                                                   |
| D |                                                                   |
| o |                                                                   |
| w |                                                                   |
| n |                                                                   |
| M |                                                                   |
| e |                                                                   |
| n |                                                                   |
| u |                                                                   |
| * |                                                                   |
| * |                                                                   |
+---+-------------------------------------------------------------------+
| 1 | Assignment of responsibility.                                     |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 2 | Assignment of authority.                                          |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 3 | Does not understand procedures, policies or instructions and      |
| \ | information.                                                      |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 4 | Does not understand controls.                                     |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 5 | Does not understand process measurements.                         |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 6 | Does not understand interfaces.                                   |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 7 | Span of control.                                                  |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 8 | Position vacant.                                                  |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+
| 9 | Other.                                                            |
| \ |                                                                   |
| . |                                                                   |
+---+-------------------------------------------------------------------+