This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents.

Rules and Regulations Federal Register

42929 

Vol. 82, No. 176 

Wednesday, September 13, 2017 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2017–0809; Product 

Identifier 2017–NM–094–AD; Amendment 

39–19030; AD 2017–18–21] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are superseding 

Airworthiness Directive (AD) 2017–13– 

12, which applied to all Airbus Model 

A318 and A319 series airplanes; Model 

A320–211, –212, –214, –231, –232, and 

–233 airplanes; and Model A321–111, 

–112, –131, –211, –212, –213, –231, and 

–232 airplanes. AD 2017–13–12 

required modification or replacement of 

certain side stay assemblies of the main 

landing gear (MLG). This new AD 

clarifies the formatting of a figure in the 

published version of AD 2017–13–12. 

This new AD was prompted by reports 

indicating that affected parties 

misinterpreted the applicability of the 

affected part numbers due to the 

formatting of a figure in the published 

version of AD 2017–13–12, which could 

result in a negative effect on 

compliance. We are issuing this AD to 

address the unsafe condition on these 

products. 

DATES: This AD is effective September 

28, 2017. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of August 9, 2017 (82 FR 30949, July 

5, 2017). 

We must receive comments on this 

AD by October 30, 2017. 

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, between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

For Airbus service information 

identified in this final rule, contact 

Airbus, Airworthiness Office–EIAS, 1 

Rond Point Maurice Bellonte, 31707 

Blagnac Cedex, France; telephone: +33 5 

61 93 36 96; fax: +33 5 61 93 44 51; 

email: account.airworth-eas@

airbus.com; Internet: http://

www.airbus.com. 

For Messier-Dowty service 

information identified in this final rule, 

contact Messier-Dowty: Messier 

Services Americas, Customer Support 

Center, 45360 Severn Way, Sterling, VA 

20166–8910; telephone: 703–450–8233; 

fax: 703–404–1621; Internet: https://

techpubs.services/messier-dowty.com. 

You may view this referenced service 

information at the FAA, Transport 

Standards Branch, 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–2017– 

0809. 

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–2017– 

0809; 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 (telephone 800–647– 

5527) is Docket Management Facility, 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue SE., 

Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Sanjay Ralhan, Aerospace Engineer, 

International Section, Transport 

Standards Branch, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone 425–227–1405; fax 425–227– 

1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

On June 19, 2017, we issued AD 

2017–13–12, Amendment 39–18942 (82 

FR 30949, July 5, 2017) (‘‘AD 2017–13– 

12’’), which applied to all Airbus Model 

A318 series airplanes and A319 series 

airplanes; Model A320–211, –212, –214, 

–231, –232, and –233 airplanes; and 

Model A321–111, –112, –131, –211, 

–212, –213, –231, and –232 airplanes. 

AD 2017–13–12 was prompted by an 

evaluation by the design approval 

holder (DAH), which indicates that the 

main landing gear (MLG) does not 

comply with certification specifications, 

which could result in a locking failure 

of the MLG side stay. AD 2017–13–12 

required modification or replacement of 

certain MLG side stay assemblies. We 

issued AD 2017–13–12 prevent possible 

collapse of the MLG during takeoff and 

landing. 

Since we issued AD 2017–13–12, we 

have received reports indicating that 

affected parties misinterpreted the 

applicability of the affected part 

numbers due to the formatting of figure 

1 to paragraphs (g), (h), and (i) in the 

published version of AD 2017–13–12, 

which could result in a negative effect 

on compliance. Therefore, we have 

determined that clarification of the 

formatting of the published figure is 

necessary. 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA AD 2016– 

0018R1, dated September 14, 2016 

(referred to after this as the Mandatory 

Continuing Airworthiness Information, 

or ‘‘the MCAI’’), to correct an unsafe 

condition for all Airbus Model A318 

and A319 series airplanes; Model A320– 

211, –212, –214, –231, –232, and –233 

airplanes; and Model A321–111, –112, 

–131, –211, –212, –213, –231, and –232 

airplanes. The EASA AD is referenced 

in AD 2017–13–12. EASA has not 


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42930 Federal Register / Vol. 82, No. 176 / Wednesday, September 13, 2017 / Rules and Regulations 

revised its AD since the issuance of AD 

2017–13–12. 

You may examine the MCAI in the 

AD docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2017– 

0809. 

Related Service Information Under 1 

CFR Part 51 

We have reviewed the following 

service information. 

• Airbus Service Bulletin A320–32– 

1429, Revision 01, dated February 29, 

2016. 

• Messier-Bugatti-Dowty Service 

Bulletin 200–32–315, dated April 24, 

2015. 

• Messier-Bugatti-Dowty Service 

Bulletin 201–32–63, dated April 24, 

2015. 

The service information describes 

procedures for modifying the MLG side 

stay assembly. The Messier-BugattiDowty documents are distinct since 

they apply to different airplane models. 

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 and Requirements 

of This AD 

This product has been approved by 

the aviation authority of another 

country, and is approved for operation 

in the United States. Pursuant to our 

bilateral agreement with the State of 

Design Authority, we have been notified 

of the unsafe condition described in the 

MCAI and service information 

referenced above. We are issuing this 

AD because we evaluated all pertinent 

information and determined the unsafe 

condition exists and is likely to exist or 

develop on other products of the same 

type design. 

FAA’s Justification and Determination 

of the Effective Date 

We are superseding AD 2017–13–12 

to clarify the formatting of a figure in 

the regulatory text of the published AD. 

No other changes have been made to AD 

2017–13–12. Therefore, we determined 

that notice and opportunity for prior 

public comment are unnecessary. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments about this AD. 

Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2017–0809; 

Product Identifier 2017–NM–094–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 959 

airplanes of U.S. registry. This AD adds 

no new economic burden to AD 2017– 

13–12. We estimate the following costs 

to comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Replacement or modification (retained actions from AD 2017–13–12).9 work-hours × $85 per hour = $765 ............. $14,104 $14,869 $14,259,371 

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. 

This AD is issued in accordance with 

authority delegated by the Executive 

Director, Aircraft Certification Service, 

as authorized by FAA Order 8000.51C. 

In accordance with that order, issuance 

of ADs is normally a function of the 

Compliance and Airworthiness 

Division, but during this transition 

period, the Executive Director has 

delegated the authority to issue ADs 

applicable to transport category 

airplanes to the Director of the System 

Oversight Division. 

Regulatory Findings 

We determined that 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 the 

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 

removing airworthiness directive (AD) 


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Federal Register / Vol. 82, No. 176 / Wednesday, September 13, 2017 / Rules and Regulations 42931 

2017–13–12, Amendment 39–18942 (82 

FR 30949, July 5, 2017), and adding the 

following new AD: 

2017–18–21 Airbus: Amendment 39–19030; 

Docket No. FAA–2017–0809; Product 

Identifier 2017–NM–094–AD. 

(a) Effective Date 

This AD is effective September 28, 2017. 

(b) Affected ADs 

This AD replaces AD 2017–13–12, 

Amendment 39–18942 (82 FR 30949, July 5, 

2017) (‘‘AD 2017–13–12’’). 

(c) Applicability 

This AD applies to the airplanes identified 

in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) 

of this AD, certificated in any category, all 

manufacturer serial numbers. 

(1) Airbus Model A318–111, –112, –121, 

and –122 airplanes. 

(2) Airbus Model A319–111, –112, –113, 

–114, –115, –131, –132, and –133 airplanes. 

(3) Airbus Model A320–211, –212, –214, 

–231, –232, and –233 airplanes. 

(4) Airbus Model A321–111, –112, –131, 

–211, –212, –213, –231, and –232 airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 32, Landing Gear. 

(e) Reason 

This AD was prompted by an evaluation by 

the design approval holder that indicates that 

the main landing gear (MLG) does not 

comply with certification specifications, 

which could result in a locking failure of the 

MLG side stay. We are issuing this AD to 

prevent possible collapse of the MLG during 

takeoff and landing. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Retained Modification or Replacement, 

With Revised Figure Formatting 

This paragraph restates the requirements of 

paragraph (g) of AD 2017–13–12, with 

revised figure formatting. Within 120 months 

after August 9, 2017 (the effective date of AD 

2017–13–12), accomplish the action specified 

in paragraph (g)(1) or (g)(2) of this AD. 

(1) Modify each MLG side stay assembly 

having a part number listed in figure 1 to 

paragraphs (g), (h), and (i) of this AD, in 

accordance with the Accomplishment 

Instructions of Airbus Service Bulletin A320– 

32–1429, Revision 01, dated February 29, 

2016, and the service information specified 

in paragraph (g)(1)(i) or (g)(1)(ii) of this AD, 

as applicable. The modification may be done 

‘‘off wing,’’ provided the modified MLG is 

reinstalled on the airplane. 

(i) For Model A318 Ssries airplanes; Model 

A319 series airplanes; and Model A320–211, 

–212, –214, –231, –232, and –233 airplanes: 

Messier-Bugatti-Dowty Service Bulletin 200– 

32–315, dated April 24, 2015. 

(ii) For Model A321 series airplanes: 

Messier-Bugatti-Dowty Service Bulletin 201– 

32–63, dated April 24, 2015. 

(2) Replace the MLG side stay assembly 

with a side stay assembly that has been 

modified in accordance with paragraph (g)(1) 

of this AD. Do the replacement using a 

method approved by the Manager, 

International Section, Transport Standards 

Branch, FAA; or the European Aviation 

Safety Agency (EASA); or Airbus’s EASA 

Design Organization Approval (DOA). 

Note 1 to paragraph (g)(2) of this AD: 

Additional guidance for the replacement can 

be found in Chapter 32 of the Airbus A318/ 

A319/A320/A321 Aircraft Maintenance 

Manual. 

FIGURE 1 TO PARAGRAPHS (g), (h), AND (i) OF THIS AD—AFFECTED MLG SIDE STAY ASSEMBLIES

Models Affected part Nos. 

(P/N) 

Strike 

number not 

cancelled 

A318–111, A318–112, A318–121, A318–122, A319–111, A319–112, 

A319–113, A319–114, A319–115, A319–131, A319–132, A319–133, 

A320–211, A320–212, A320–214, A320–231, A320–232, and A320– 

233 airplanes.

201166001–xxx 1 .........................................................

201166002–xxx.1

201166003–xxx.1

201166004–xxx.1

201166005–xxx.1

12 

201166006–xxx.1

201166007–xxx.1

201166008–xxx.1

201166009–xxx.1

201166010–xxx.1

201166011–xxx.1

201166012–xxx.2

201166013–000 through 201166013–030 inclusive.2

201166014–000 through 201166014–030 inclusive.2

A321–111, A321–112, and A321–131 airplanes ...................................... 201390001–000 through 201390001–040 inclusive.2

201390002–000 through 201390002–040 inclusive.2

15 

201527001–000 through 201527001–025 inclusive.2

201527002–000 through 201527002–025 inclusive.2

A321–211, A321–212, A321–213, A321–231, and A321–232 airplanes 201524001–000 through 201524001–035 inclusive.2

201524002–000 through 201524002–035 inclusive.2

201660001–000 through 201660001–030 inclusive.2

201660002–000 through 201660002–030 inclusive.2

15 

1The ‘xxx’ used in this figure can be any 3-digit combination. 

2 Units having a P/N with no dash number after the first 9 digits are also affected. Units having a P/N with the first 9 digits and a dash number 

higher than those listed, are not affected by the requirements of this AD. 

(h) Retained Provisions for Unaffected 

Airplanes, With No Changes 

This paragraph restates the provisions of 

paragraph (h) of AD 2017–13–12, with no 

changes. An airplane on which Airbus 

Modification (Mod) 156646, Airbus Mod 

161202, or Airbus Mod 161346 has been 

embodied in production is not affected by the 

requirements of paragraph (g) of this AD, 

provided it is determined that no part having 

a part number identified in figure 1 to 

paragraphs (g), (h), and (i) of this AD has 

been installed on that airplane since the date 

of issuance of the original certificate of 

airworthiness or the original export 

certificate of airworthiness. A review of the 

airplane maintenance records is acceptable to 

make this determination, provided that these 

records are accurate and can be relied upon 

to conclusively make that determination. 

(i) Retained Parts Installation Prohibition, 

With No Changes 

This paragraph restates the requirements of 

paragraph (i) of AD 2017–13–12, with no 

changes. As of August 9, 2017 (the effective 

date of AD 2017–13–12), do not install on 

any airplane, an MLG side stay assembly 

having a part number, with the strike number 

not cancelled, as identified in figure 1 to 

paragraphs (g), (h), and (i) of this AD, unless 


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42932 Federal Register / Vol. 82, No. 176 / Wednesday, September 13, 2017 / Rules and Regulations 

it has been modified in accordance with the 

requirements of paragraph (g) of this AD. 

(j) Retained Credit for Previous Actions, 

With No Changes 

This paragraph restates the provisions of 

paragraph (j) of AD 2017–13–12, with no 

changes. This paragraph provides credit for 

actions required by paragraph (g) of this AD, 

if those actions were performed before 

August 9, 2017 (the effective date of AD 

2017–13–12), using Airbus Service Bulletin 

A320–32–1429, dated September 10, 2015. 

(k) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Section, Transport Standards Branch, 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 International 

Section, send it to the attention of the person 

identified in paragraph (l)(2) of this AD. 

Information may be emailed to: 9-ANM-116- 

AMOC-REQUESTS@faa.gov. 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. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer, the action must 

be accomplished using a method approved 

by the Manager, International Section, 

Transport Standards Branch, FAA; or EASA; 

or Airbus’s EASA DOA. If approved by the 

DOA, the approval must include the DOAauthorized signature. 

(3) Required for Compliance (RC): If any 

service information contains procedures or 

tests that are identified as RC, those 

procedures and tests must be done to comply 

with this AD; any procedures or tests that are 

not identified as RC are recommended. Those 

procedures and tests that are not identified 

as RC may be deviated from using accepted 

methods in accordance with the operator’s 

maintenance or inspection program without 

obtaining approval of an AMOC, provided 

the procedures and tests identified as RC can 

be done and the airplane can be put back in 

an airworthy condition. Any substitutions or 

changes to procedures or tests identified as 

RC require approval of an AMOC. 

(l) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA AD 

2016–0018R1, dated September 14, 2016, for 

related information. You may examine the 

MCAI on the Internet at http://

www.regulations.gov by searching for and 

locating Docket No. FAA–2017–0809. 

(2) For more information about this AD, 

contact Sanjay Ralhan, Aerospace Engineer, 

International Section, Transport Standards 

Branch, FAA, 1601 Lind Avenue SW., 

Renton, WA 98057–3356; telephone 425– 

227–1405; fax 425–227–1149. 

(3) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

paragraphs (m)(3), (m)(4), and (m)(5) of this 

AD. 

(m) 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 this AD specifies otherwise. 

(3) The following service information was 

approved for IBR on August 9, 2017 (82 FR 

30949, July 5, 2017). 

(i) Airbus Service Bulletin A320–32–1429, 

Revision 01, dated February 29, 2016. 

(ii) Messier-Bugatti-Dowty Service Bulletin 

200–32–315, dated April 24, 2015. 

(iii) Messier-Bugatti-Dowty Service 

Bulletin 201–32–63, dated April 24, 2015. 

(4) For Airbus service information 

identified in this AD, contact Airbus, 

Airworthiness Office—EIAS, 1 Rond Point 

Maurice Bellonte, 31707 Blagnac Cedex, 

France; telephone: +33 5 61 93 36 96; fax: 

+33 5 61 93 44 51; email: account.airwortheas@airbus.com; Internet: http://

www.airbus.com. 

(5) For Messier-Dowty service information 

identified in this AD, contact Messier-Dowty: 

Messier Services Americas, Customer 

Support Center, 45360 Severn Way, Sterling, 

VA 20166–8910; telephone: 703–450–8233; 

fax: 703–404–1621; Internet: https://

techpubs.services/messier-dowty.com. 

(6) You may view this service information 

at the FAA, Transport Standards Branch, 

1601 Lind Avenue SW., Renton, WA. For 

information on the availability of this 

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

(7) 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 August 

31, 2017. 

Dionne Palermo, 

Acting Director, System Oversight Division, 

Aircraft Certification Service. 

[FR Doc. 2017–19301 Filed 9–12–17; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 97 

[Docket No. 31152; Amdt. No. 3763] 

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 establishes, amends, 

suspends, or removes Standard 

Instrument Approach Procedures 

(SIAPs) and associated Takeoff 

Minimums and Obstacle Departure 

Procedures (ODPs) 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 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 September 

13, 2017. 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 September 

13, 2017. 

ADDRESSES: Availability of matters 

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. 


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