### 3308 Federal Register / Vol. 81, No. 13 / Thursday, January 21, 2016 / Rules and Regulations

Eurocopter Deutschland GmbH): Amendment 39–18373; Docket No. FAA–2015–0669; Directorate Identifier 2013–SW–038–AD.
(a) Applicability

This AD applies to AHD Model MBB–BK 117 A–1, A–3, A–4, B–1, B–2, C–1, and C– 2 helicopters, certificated in any category.

(b) Unsafe Condition

This AD defines the unsafe condition as corrosion, a crack, or a scratch on an N2 control arm. This condition could lead to failure of the N2 control arm, resulting in a reduction in rotor speed and subsequent loss of control of the helicopter.

(c) Effective Date

This AD becomes effective February 25,

2016. (d) Compliance

You are responsible for performing each action required by this AD within the specified compliance time unless it has already been accomplished prior to that time.
(e) Required Actions

For helicopters that have not reached 2 years from the date of first flight, within 1 year or before reaching 2 years from the date of first flight, whichever occurs first; and for helicopters that have reached or exceeded 2 years from the date of first flight, within 50 hours TIS:

(1) Visually inspect each N2 control arm for corrosion, a crack, and a scratch as depicted in Figure 1 of Eurocopter Alert Service Bulletin (ASB) MBB–BK117–60A– 126 or ASB MBB–BK117 C–2–76A–005, both Revision 0, and both dated June 24, 2013, as applicable to your model helicopter.

(i) If an N2 control arm has corrosion or a scratch less than 0.5 millimeter (mm) (0.020 inch) in depth, before further flight, remove the corrosion and repair the scratch.

(ii) If an N2 control arm has any exfoliation corrosion, a crack, or has corrosion or a scratch 0.5 mm (0.020 inch) or greater in depth, before further flight, replace the N2 control arm.

(2) Thereafter, perform the requirements in paragraph (e)(1) of this AD at intervals not to exceed 12 months.
(f) Alternative Methods of Compliance (AMOCs)

(1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: James Blyn, Aviation Safety Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222–5110; email 9- ASW-FTW-AMOC-Requests@faa.gov

.

(2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, we suggest that you notify your principal inspector, or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC. (g) Additional Information The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2013–0154, dated July 22, 2013. You may view the EASA AD on the Internet at http:// www.regulations.gov in Docket No. FAA–
2015–0669. (h) Subject

Joint Aircraft Service Component (JASC) Code: Engine Controls, 7600.
(i) Material Incorporated by Reference

(1) The Director of the Federal Register approved the incorporation by reference of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.

(i) Eurocopter Alert Service Bulletin (ASB) MBB–BK117–60A–126, Revision 0, dated June 24, 2013.

(ii) Eurocopter ASB MBB–BK117 C–2– 76A–005, Revision 0, dated June 24, 2013.

(3) For Eurocopter service information identified in this final rule, contact Airbus Helicopters, Inc., 2701 N. Forum Drive, Grand Prairie, Texas 75052; telephone (972) 641–0000 or (800) 232–0323; fax (972) 641– 3775; or at http:// www.airbushelicopters.com/techpub

.

(4) You may view this service information at FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222–5110.

(5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741–6030, or go to: http://www.archives.gov/federal-register/cfr/ibrlocations.html

.

Issued in Fort Worth, Texas, on January 6,
2016. Bruce E. Cain, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2016–00658 Filed 1–20–16; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2015–1935; Directorate Identifier 2014–SW–008–AD; Amendment**  **39–18374; AD 2016–01–15]**

**RIN 2120–AA64**

**Airworthiness Directives; Agusta S.p.A. Helicopters** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule. **SUMMARY :**  We are adopting a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model AB139 and AW139 helicopters. This AD requires visually inspecting certain subfloor frames for a crack. This AD wasprompted by reports of cracks on inservice helicopters. The actions of this AD are intended to detect or prevent a crack in the subfloor frame, which could result in failure of the pilot and co-pilot pedal support frame and subsequent loss of control of the helicopter.

**DATES :**  This AD is effective February 25,
2016.

The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD as of February 25, 2016.

**ADDRESSES :**  For service information identified in this rule, contact AgustaWestland, Product Support Engineering, Via del Gregge, 100, 21015 Lonate Pozzolo (VA) Italy, ATTN: Maurizio D’Angelo; telephone 39–0331– 664757; fax 39–0331–664680; or at http://www.agustawestland.com/ technical-bulletins. You may review the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX
76177. Examining the AD Docket

You may examine the AD docket on the Internet at http:// www.regulations.gov by searching for and locating Docket No. FAA–2015– 1935 or in person at the Docket Operations Office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the European Aviation Safety Agency (EASA) AD, any incorporated-by-reference service information, the economic evaluation, any comments received, and other information. The street address for the Docket Operations Office (phone: 800– 647–5527) is U.S. Department of Transportation, Docket Operations Office, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590.

**FOR FURTHER INFORMATION CONTACT :**  Robert Grant, Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222–5110; email robert.grant@ faa.gov

. **SUPPLEMENTARY INFORMATION :** 

Discussion

On June 5, 2015, at 80 FR 32072, the Federal Register published our notice of proposed rulemaking (NPRM), which


### 3309 Federal Register / Vol. 81, No. 13 / Thursday, January 21, 2016 / Rules and Regulations

proposed to amend 14 CFR part 39 by adding an AD that would apply to Agusta Model AB139 and AW139 helicopters, serial number (S/N) 31005 through 31517 (except S/N 31007, 31415, 31431, 31491, 31500, 31508, and 31516) and S/N 41001 through 41356 (except S/N 41355). The NPRM proposed to require visually inspecting certain subfloor frames for a crack. The proposed requirements were intended to detect or prevent a crack in the subfloor frame, which could result in failure of the pilot and co-pilot pedal support frame and subsequent loss of control of the helicopter.

The NPRM was prompted by AD No. 2014–0048, dated March 4, 2014, issued by EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for Agusta Model AB139 and AW139 helicopters with a S/N 31005 through 31517 (except S/N 31007, 31415, 31431, 31491, 31500, 31508, and 31516) and S/ N 41001 through 41356 (except S/N 41355). EASA advises that cracks have been reported in the subfloor frame at station (STA) 2105 on in-service helicopters. This condition, if not detected and corrected, could lead to failure of the pedals supporting the frame, which in turn could lead to the pedals being inoperative and subsequent loss of control of the helicopter, EASA advises.

The EASA AD requires repetitive inspections of the subfloor frame at STA 2105 for a crack. The EASA AD also requires installation of frame reinforcements before further flight if there is a crack or within 1,200 flight hours if there is no crack. The EASA AD provides that installation of the frame reinforcements constitutes terminating action for the repetitive inspections required by the AD.

Since the NPRM was issued, the FAA Southwest Regional Office has relocated and a group email address has been established for requesting an FAA Alternative Method of Compliance (AMOC) for a helicopter of foreign design. This AD contains the current physical address of the FAA Southwest Regional Office and the new email address for requesting an AMOC.

Comments

We gave the public the opportunity to participate in developing this AD, but we received no comments on the NPRM (80 FR 32072, June 5, 2015).

FAA’s Determination

These helicopters have been approved by the aviation authority of Italy and are approved for operation in the United States. Pursuant to our bilateral agreement with Italy, EASA, its technical representative, has notified us of the unsafe condition described in the EASA AD. We are issuing this AD because we evaluated all information provided by EASA and determined the unsafe condition exists and is likely to exist or develop on other helicopters of these same type designs and that air safety and the public interest require adopting the AD requirements as proposed.

Differences Between This AD and the EASA AD

The EASA AD requires conducting the initial inspection within 30 flight hours or 2 months, whichever occurs first, and thereafter, at intervals not to exceed 300 flight hours or 6 months, whichever occurs first. This AD requires conducting the initial inspection within 30 hours time-in-service (TIS), and thereafter, at intervals not to exceed 300 hours TIS.

Related Service Information Under 1 CFR Part 51

We reviewed AgustaWestland Bolletino Tecnico No. 139–311, Revision B, dated June 4, 2014 (BT), for certain serial-numbered Agusta Model AB139 and AW139 helicopters. The BT calls for visual inspections of the subfloor frames within 30 flight hours or two months, whichever occurs first, and thereafter at intervals of 300 flight hours or 6 months, whichever comes first, until frame reinforcements are installed to prevent future failures. The BT also specifies installing the frame reinforcements immediately if a crack is found and within 1,200 flight hours if a crack is not found. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the **ADDRESSES** section. Costs of Compliance

We estimate that this AD affects 102 U.S.-registered helicopters and that labor costs average $85 a work hour. Based on these estimates, we expect the following costs:

• The visual inspection requires 2 work-hours for a labor cost of $170 per helicopter. No parts are needed, so the cost totals $170 per helicopter, $17,340 for the U.S. fleet.

• If there are no cracks, installing theframe reinforcements requires 240 workhours for a labor cost of $20,400 and $2,274 for parts. The total cost is $22,674 per helicopter.

• If there is a crack, installing theframe reinforcements requires 240 workhours for a labor cost of $20,400 and $3,401 for parts. The total cost is $23,801 per helicopter. Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA’s authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency’s authority.

We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ‘‘General requirements.’’ Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on helicopters identified in this rulemaking action. Regulatory Findings

This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.

For the reasons discussed above, I certify that this AD:

(1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866;

(2) Is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979);

(3) Will not affect intrastate aviation in Alaska to the extent that it justifies making a regulatory distinction; and

(4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

We prepared an economic evaluation of the estimated costs to comply with this AD and placed it in the AD docket. List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:


### 3310 Federal Register / Vol. 81, No. 13 / Thursday, January 21, 2016 / Rules and Regulations

**PART 39—AIRWORTHINESS DIRECTIVES** 

■ 1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

**§ 39.13 [Amended]**

■ 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD):
2016–01–15 Agusta S.p.A.: Amendment 39– 18374; Docket No. FAA–2015–1935; Directorate Identifier 2014–SW–008–AD.
(a) Applicability

This AD applies to Agusta S.p.A. Model AB139 and AW139 helicopters, serial number (S/N) 31005 through 31517 (except S/N 31007, 31415, 31431, 31491, 31500, 31508, and 31516) and S/N 41001 through 41356 (except S/N 41355), certificated in any category.
(b) Unsafe Condition

This AD defines the unsafe condition as a crack in a subfloor frame. This conditioncould result in failure of the pilot and copilot pedal support frame and subsequent loss of control of the helicopter.

(c) Effective Date

This AD becomes effective February 25,
2016. (d) Compliance

You are responsible for performing each action required by this AD within the specified compliance time unless it has already been accomplished prior to that time.
(e) Required Actions

(1) Within 30 hours time-in-service (TIS) and thereafter at intervals not to exceed 300 hours TIS, using a light, inspect all visible surfaces of the left hand subfloor frame, right hand subfloor frame, and middle subfloor frame at station (STA) 2105 for a crack as shown in Figures 10 through 13 of AgustaWestland Bollettino Tecnico No. 139– 311, Revision B, dated June 4, 2014 (BT 139– 311).

(2) If there is a crack, before further flight, install frame STA 2105 retromod part number (P/N) 3G5306P47211 by following the Compliance Instructions, Part II, paragraphs 7 through 7.10. of BT 139–311.

(3) If there are no cracks, within 1200 hours TIS, install frame STA 2105 retromod P/N 3G5306P47211 by following the Compliance Instructions, Part II, paragraphs 7 through 7.10. of BT 139–311.

(4) Installing frame STA 2105 retromod P/ N 3G5306P47211 terminates the repetitive inspection requirements in paragraph (e)(1) of this AD.
(f) Special Flight Permits

Special flight permits are prohibited.
(g) Alternative Methods of Compliance (AMOCs)

(1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Robert Grant, Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222–5110; email 9-ASWFTW-AMOC-Requests@faa.gov.

(2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, we suggest that you notify your principal inspector, or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC.

(h) Additional Information

The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2014–0048, dated March 4, 2014. You may view the EASA AD on the Internet at http://www.regulations.gov in Docket No.
FAA–2015–1935.
(i) Subject

Joint Aircraft Service Component (JASC) Code: 5300, Fuselage Structure (General).
(j) Material Incorporated by Reference

(1) The Director of the Federal Register approved the incorporation by reference of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.

(i) AgustaWestland Bollettino Tecnico No. 139–311, Revision B, dated June 4, 2014.

(ii) Reserved. (3) For Agusta S.p.A. service information identified in this AD, contact AgustaWestland, Product Support Engineering, Via del Gregge, 100, 21015 Lonate Pozzolo (VA) Italy, ATTN: Maurizio D’Angelo; telephone 39–0331–664757; fax
39–0331–664680; or at http://www.agustawestland.com/technicalbulletins.

(4) You may view this service information at FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222–5110.

(5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741–6030, or go to: http://www.archives.gov/federal-register/cfr/ibrlocations.html.

Issued in Fort Worth, Texas, on January 6,

2016. Bruce E. Cain, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2016–00659 Filed 1–20–16; 8:45 am]

**BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION** 

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2014–0577; Directorate Identifier 2013–SW–042–AD; Amendment**  **39–18375; AD 2015–12–09 R1]**

**RIN 2120–AA64**

**Airworthiness Directives; Airbus Helicopters Deutschland GmbH**  **(Previously Eurocopter Deutschland GmbH) (Airbus Helicopters)** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule.

**SUMMARY :**  We are revising airworthiness directive (AD) 2015–12–09 for Airbus Helicopters Model EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, EC135T2+, and MBB–BK 117 C–2 helicopters. AD 2015–12–09 required inspecting certain washers for movement and making the appropriate repairs if the washers move. As published, AD 2015–12–09 referenced an incorrect date for the service information in the Credit for Previous Actions section. This AD corrects the error while retaining the requirements of AD 2015–12–09. These actions are intended to prevent loss of concerned control axis and subsequent loss of control of the helicopter.

**DATES :**  This AD is effective February 25,
2016.

The Director of the Federal Register approved the incorporation by reference of certain documents listed in this AD as of July 23, 2015 (80 FR 34831, June 18, 2015).

**ADDRESSES :**  For service information identified in this final rule, contact Airbus Helicopters, Inc., 2701 N. Forum Drive, Grand Prairie, TX 75052; telephone (972) 641–0000 or (800) 232– 0323; fax (972) 641–3775; or at http:// www.airbushelicopters.com/techpub

. You may review the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, Room 6N–321, 10101 Hillwood Pkwy, Fort Worth, TX 76177. Examining the AD Docket

You may examine the AD docket on the Internet at http:// www.regulations.gov by searching for and locating Docket No. FAA–2014– 0577; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the European Aviation Safety Agency (EASA) AD, any