10074 Federal Register / Vol. 81, No. 39 / Monday, February 29, 2016 / Rules and Regulations 

that is likely to exist or develop on 

products 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, 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. 

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: 

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): 

2016–04–24 The Boeing Company: 

Amendment 39–18418; Docket No. 

FAA–2015–1423; Directorate Identifier 

2014–NM–173–AD. 

(a) Effective Date 

This AD is effective April 4, 2016. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to The Boeing Company 

Model 757–200 series airplanes, certificated 

in any category, modified by the applicable 

supplemental type certificate identified in 

paragraphs (c)(1) and (c)(2) of this AD. 

(1) ST01529SE (http://rgl.faa.gov/

Regulatory_and_Guidance_Library/rgstc.nsf/

0/0af09c3701a237ee86257a5d0064b3aa/

$FILE/ST01529SE.pdf). 

(2) ST02278SE (http://rgl.faa.gov/

Regulatory_and_Guidance_Library/rgstc.nsf/

0/e54b5289a2e9f6ef86257b7f0056edaf/

$FILE/ST02278SE.pdf). 

(d) Subject 

Air Transport Association (ATA) of 

America Code 11, Placards and Markings. 

(e) Unsafe Condition 

This AD was prompted by reports of a 

main cargo door being blown past its full 

open position while on the ground during 

gusty wind conditions, which resulted in 

uncontrolled fall down to its closed position. 

We are issuing this AD to prevent damage to 

the main cargo door, which could result in 

rapid decompression of the airplane, or 

injury to maintenance and ground crew 

during ground operations. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Installation 

Within 90 days after the effective date of 

this AD, install a new placard and bracket, 

replace the existing placard, and replace the 

main cargo door control panel, in accordance 

with the Accomplishment Instructions of 

Precision Conversions Service Bulletin PC– 

757–11–0023, dated August 1, 2014. 

(h) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle Aircraft 

Certification Office (ACO), FAA, has the 

authority to approve AMOCs for this AD, if 

requested using the procedures found in 14 

CFR 39.19. In accordance with 14 CFR 39.19, 

send your request to your principal inspector 

or local Flight Standards District Office, as 

appropriate. If sending information directly 

to the manager of the ACO, send it to the 

attention of the person identified in 

paragraph (i)(1) of this AD. Information may 

be emailed to: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local flight standards district office/

certificate holding district office. 

(i) Related Information 

For more information about this AD, 

contact Narinder Luthra, Aerospace Engineer, 

Airframe Branch, ANM–120S, FAA, Seattle 

Aircraft Certification Office (ACO), 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

phone: 425–917–6513; fax: 425–917–6590; 

email: Narinder.Luthra@faa.gov. 

(j) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) 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) Precision Conversions Service Bulletin 

PC–757–11–0023, dated August 1, 2014. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Precision Conversions LLC, 

4900 SW Griffith Drive, Suite 133, Beaverton, 

OR 97005; ATTN: Steven A. Lopez; phone: 

503–601–3001; email: Steven.Lopez@

precisionaircraft.com. 

(4) You may view this service information 

at FAA, Transport Airplane Directorate, 1601 

Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(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 Renton, Washington, on February 

16, 2016. 

Dionne Palermo, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–04036 Filed 2–26–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2016–3981; Directorate 

Identifier 2015–NM–053–AD; Amendment 

39–18417; AD 2016–04–23] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

The Boeing Company Model 787–8 

airplanes. This AD requires an 

inspection of the station 337 (door 

number 1) outboard partitions for a tie 

rod and quick release pins, and to 

ensure that both partition supports are 

engaged in the structural bracket at each 

outboard partition, and corrective 

actions if necessary. This AD was 

prompted by reports of missing right 

and left outboard partition tie rods at 

door number 1. We are issuing this AD 

to detect and correct partitions with 

missing tie rods or release pins or with 

supports that are not engaged in the 

structural bracket. These partitions 

could come loose during a highacceleration event and strike the flight 

attendant seats in the door 1 location, 

causing serious injury to the seat 

occupants, or could affect safe egress 

from the airplane. 


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Federal Register / Vol. 81, No. 39 / Monday, February 29, 2016 / Rules and Regulations 10075 

DATES: This AD is effective March 15, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of March 15, 2016. 

We must receive comments on this 

AD by April 14, 2016. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: 202–493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

For service information identified in 

this final rule, contact Boeing 

Commercial Airplanes, Attention: Data 

& Services Management, P.O. Box 3707, 

MC 2H–65, Seattle, WA 98124–2207; 

telephone 206–544–5000, extension 1; 

fax 206–766–5680; Internet https://

www.myboeingfleet.com. You may view 

this referenced service information at 

the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., 

Renton, WA. For information on the 

availability of this material at the FAA, 

call 425–227–1221. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA 2016– 

3981. 

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–2016– 

3981; 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 regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Office (phone: 800–647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Francis Smith, Aerospace Engineer, 

Cabin Safety and Environmental 

Systems Branch, ANM–150S, FAA, 

Seattle Aircraft Certification Office, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; phone 425–917–6596; fax 

425–917–6590; email: francis.smith@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We have received reports of missing 

right and left outboard partition tie rods 

at station 337 (door number 1) on Model 

787–8 airplanes as a result of a 

manufacturing escape (i.e., insufficient 

documentation to show engineering 

details). We are issuing this AD to detect 

and correct partitions with missing tie 

rods or release pins or with supports 

that are not engaged in the structural 

bracket. These partitions could come 

loose during a high-acceleration event 

and strike the flight attendant seats in 

the door 1 location, causing serious 

injury to the seat occupants, or could 

affect safe egress from the airplane. 

Related Service Information Under 1 

CFR Part 51 

We reviewed Boeing Service Bulletin 

B787–81205–SB250081–00, Issue 001, 

dated December 9, 2014. The service 

bulletin describes procedures for an 

inspection of the station 337 outboard 

partitions for a tie rod and quick release 

pins, and also to determine that both 

partition supports are engaged in the 

structural bracket, and corrective 

actions. 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. 

FAA’s Determination 

We are issuing this AD because we 

evaluated all the relevant information 

and determined the unsafe condition 

described previously is likely to exist or 

develop in other products of the same 

type design. 

AD Requirements 

This AD requires accomplishing the 

actions specified in the service 

information described previously, 

except as discussed under ‘‘Differences 

Between the AD and the Service 

Information.’’ 

The phrase ‘‘corrective actions’’ is 

used in this AD. ‘‘Corrective actions’’ 

are actions that correct or address any 

condition found. Corrective actions in 

an AD could include, for example, 

repairs. 

Differences Between the AD and the 

Service Information 

Boeing Service Bulletin B787–81205– 

SB250081–00, Issue 001, dated 

December 9, 2014, specifies to do the 

general visual inspection ‘‘in 

accordance with the Tasks in Table 6’’ 

of the service information. However 

‘‘Table 6’’ does not exist. The tasks are 

identified in Table 4 of the service 

information. Therefore, this AD requires 

that the inspection be done in 

accordance with the tasks in Table 4 of 

the Accomplishment Instructions of 

Boeing Service Bulletin B787–81205– 

SB250081–00, Issue 001, dated 

December 9, 2014. 

FAA’s Justification and Determination 

of the Effective Date 

Since there are currently no domestic 

operators of this product, we find that 

notice and opportunity for prior public 

comment are unnecessary and that good 

cause exists for making this amendment 

effective in less than 30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety and 

was not preceded by notice and an 

opportunity for public comment. 

However, we invite you to send any 

written data, views, or arguments about 

this AD. Send your comments to an 

address listed under the ADDRESSES

section. Include ‘‘Docket Number FAA– 

2016–3981; Directorate Identifier 2015– 

NM–053–AD’’ at the beginning of your 

comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this AD. We will consider all 

comments received by the closing date 

and may amend this AD because of 

those comments. 

We will post all comments we 

receive, without change, to http://

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this AD. 

Costs of Compliance 

We estimate that this AD affects 0 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 


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10076 Federal Register / Vol. 81, No. 39 / Monday, February 29, 2016 / Rules and Regulations 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Inspection ................................ 3 work-hours × $85 per hour = $255 ..................................... $0 $255 $0 

We estimate the following costs to do 

any necessary repairs that would be 

required based on the results of the 

inspection. We have no way of 

determining the number of aircraft that 

might need these repairs: 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per 

product 

Corrective action .............................. 1 work-hour × $85 per hour = $85 ............................................................ $1,027 $1,112 

According to the manufacturer, some 

of the costs of this AD may be covered 

under warranty, thereby reducing the 

cost impact on affected individuals. We 

do not control warranty coverage for 

affected individuals. As a result, we 

have included all costs in our cost 

estimate. 

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 

products 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, 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. 

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: 

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): 

2016–04–23 The Boeing Company: 

Amendment 39–18417; Docket No. 

FAA–2016–3981; Directorate Identifier 

2015–NM–053–AD. 

(a) Effective Date 

This AD is effective March 15, 2016. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to The Boeing Company 

Model 787–8 airplanes, certificated in any 

category, as identified in Boeing Service 

Bulletin B787–81205–SB250081–00, Issue 

001, dated December 9, 2014. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 25, Equipment/furnishings. 

(e) Unsafe Condition 

This AD was prompted by reports of 

missing right and left outboard partition tie 

rods at station 337 (door number 1). We are 

issuing this AD to detect and correct 

partitions with missing tie rods or release 

pins or with supports that are not engaged in 

the structural bracket. These partitions could 

come loose during a high-acceleration event 

and strike the flight attendant seats in the 

door 1 location, causing serious injury to the 

seat occupants, or could affect safe egress 

from the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection and Corrective Actions 

Within 60 months after the effective date 

of this AD: Do a general visual inspection of 

the applicable station 337 outboard partitions 

for a tie rod and quick release pins, and to 

ensure that both partition supports are 

engaged in the structural bracket at each 

outboard partition; and do all applicable 

corrective actions; in accordance with the 

Accomplishment Instructions of Boeing 

Service Bulletin B787–81205–SB250081–00, 

Issue 001, dated December 9, 2014; except 

where Boeing Service Bulletin B787–81205– 

SB250081–00, Issue 001, dated December 9, 

2014, specifies to do the general visual 

inspection ‘‘in accordance with the Tasks in 

Table 6,’’ this AD requires that the inspection 

be done in accordance with the tasks in Table 

4 of the Accomplishment Instructions of 

Boeing Service Bulletin B787–81205– 

SB250081–00, Issue 001, dated December 9, 

2014. Do all applicable corrective actions 

before further flight. 

(h) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle Aircraft 

Certification Office (ACO), FAA, has the 

authority to approve AMOCs for this AD, if 

requested using the procedures found in 14 

CFR 39.19. In accordance with 14 CFR 39.19, 

send your request to your principal inspector 

or local Flight Standards District Office, as 


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Federal Register / Vol. 81, No. 39 / Monday, February 29, 2016 / Rules and Regulations 10077 

appropriate. If sending information directly 

to the manager of the ACO, send it to the 

attention of the person identified in 

paragraph (i) of this AD. Information may be 

emailed to: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local flight standards district office/

certificate holding district office. 

(3) An AMOC that provides an acceptable 

level of safety may be used for any repair, 

modification, or alteration required by this 

AD if it is approved by the Boeing 

Commercial Airplanes Organization 

Designation Authorization (ODA) that has 

been authorized by the Manager, Seattle 

ACO, to make those findings. To be 

approved, the repair method, modification 

deviation, or alteration deviation must meet 

the certification basis of the airplane, and the 

approval must specifically refer to this AD. 

(i) Related Information 

For more information about this AD, 

contact Francis Smith, Aerospace Engineer, 

Cabin Safety and Environmental Systems 

Branch, ANM–150S, FAA, Seattle ACO, 1601 

Lind Avenue SW., Renton, WA 98057–3356; 

phone 425–917–6596; fax 425–917–6590; 

email: francis.smith@faa.gov. 

(j) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) 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) Boeing Service Bulletin B787–81205– 

SB250081–00, Issue 001, dated December 9, 

2014. 

(ii) Reserved. 

(3) For Boeing service information 

identified in this AD, contact Boeing 

Commercial Airplanes, Attention: Data & 

Services Management, P.O. Box 3707, MC 

2H–65, Seattle, WA 98124–2207; telephone 

206–544–5000, extension 1; fax 206–766– 

5680; Internet https://

www.myboeingfleet.com. 

(4) You may view this service information 

at the FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(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 Renton, Washington, on February 

18, 2016. 

Dionne Palermo, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–04138 Filed 2–26–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 97 

[Docket No. 31063; Amdt. No. 3684] 

Standard Instrument Approach 

Procedures, and Takeoff Minimums 

and Obstacle Departure Procedures; 

Miscellaneous Amendments 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This rule amends, suspends, 

or removes Standard Instrument 

Approach Procedures (SIAPs) and 

associated Takeoff Minimums and 

Obstacle Departure Procedures for 

operations at certain airports. These 

regulatory actions are needed because of 

the adoption of new or revised criteria, 

or because of changes occurring in the 

National Airspace System, such as the 

commissioning of new navigational 

facilities, adding new obstacles, or 

changing air traffic requirements. These 

changes are designed to provide for the 

safe and efficient use of the navigable 

airspace and to promote safe flight 

operations under instrument flight rules 

at the affected airports. 

DATES: This rule is effective February 

29, 2016. The compliance date for each 

SIAP, associated Takeoff Minimums, 

and ODP is specified in the amendatory 

provisions. 

The incorporation by reference of 

certain publications listed in the 

regulations is approved by the Director 

of the Federal Register as of February 

29, 2016. 

ADDRESSES: Availability of matter 

incorporated by reference in the 

amendment is as follows: 

For Examination 

1. U.S. Department of Transportation, 

Docket Ops-M30, 1200 New Jersey 

Avenue SE., West Bldg., Ground Floor, 

Washington, DC 20590–0001; 

2. The FAA Air Traffic Organization 

Service Area in which the affected 

airport is located; 

3. The office of Aeronautical 

Navigation Products, 6500 South 

MacArthur Blvd., Oklahoma City, OK 

73169 or, 

4. 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/code_of_federal_

regulations/ibr_locations.html. 

Availability 

All SIAPs and Takeoff Minimums and 

ODPs are available online free of charge. 

Visit the National Flight Data Center 

online at nfdc.faa.gov to register. 

Additionally, individual SIAP and 

Takeoff Minimums and ODP copies may 

be obtained from the FAA Air Traffic 

Organization Service Area in which the 

affected airport is located. 

FOR FURTHER INFORMATION CONTACT: 

Thomas J. Nichols, Flight Procedure 

Standards Branch (AFS–420) Flight 

Technologies and Procedures Division, 

Flight Standards Service, Federal 

Aviation Administration, Mike 

Monroney Aeronautical Center, 6500 

South MacArthur Blvd., Oklahoma City, 

OK 73169 (Mail Address: P.O. Box 

25082 Oklahoma City, OK 73125) 

telephone: (405) 954–4164. 

SUPPLEMENTARY INFORMATION: This rule 

amends Title 14, Code of Federal 

Regulations, Part 97 (14 CFR part 97) by 

amending the referenced SIAPs. The 

complete regulatory description of each 

SIAP is listed on the appropriate FAA 

Form 8260, as modified by the National 

Flight Data Center (NFDC)/Permanent 

Notice to Airmen (P–NOTAM), and is 

incorporated by reference under 5 

U.S.C. 552(a), 1 CFR part 51, and 14 

CFR 97.20. The large number of SIAPs, 

their complex nature, and the need for 

a special format make their verbatim 

publication in the Federal Register 

expensive and impractical. Further, 

airmen do not use the regulatory text of 

the SIAPs, but refer to their graphic 

depiction on charts printed by 

publishers of aeronautical materials. 

Thus, the advantages of incorporation 

by reference are realized and 

publication of the complete description 

of each SIAP contained on FAA form 

documents is unnecessary. This 

amendment provides the affected CFR 

sections, and specifies the SIAPs and 

Takeoff Minimums and ODPs with their 

applicable effective dates. This 

amendment also identifies the airport 

and its location, the procedure and the 

amendment number. 

Availability and Summary of Material 

Incorporated by Reference 

The material incorporated by 

reference is publicly available as listed 

in the ADDRESSES section. 

The material incorporated by 

reference describes SIAPs, Takeoff 

Minimums and ODPs as identified in 

the amendatory language for part 97 of 

this final rule. 

The Rule 

This amendment to 14 CFR part 97 is 

effective upon publication of each 


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