26836 Federal Register / Vol. 83, No. 112 / Monday, June 11, 2018 / 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): 

2018–12–06 The Boeing Company: 

Amendment 39–19310; Docket No. 

FAA–2017–0904; Product Identifier 

2017–NM–071–AD. 

(a) Effective Date 

This AD is effective July 16, 2018. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to The Boeing Company 

Model 787–8 and 787–9 airplanes, 

certificated in any category, as identified in 

the applicable service information specified 

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

(1) Boeing Service Bulletin B787–81205– 

SB210075–00, Issue 003, dated March 29, 

2017 (for Model 787–8 airplanes); 

(2) Boeing Service Bulletin B787–81205– 

SB210077–00, Issue 004, dated September 

22, 2017 (for Model 787–9 airplanes). 

(d) Subject 

Air Transport Association (ATA) of 

America Code 21, Air conditioning. 

(e) Unsafe Condition 

This AD was prompted by a report of an 

in-service reliability issue involving a latent 

flow sensor failure combined with single 

cabin air compressor (CAC) operation. This 

condition resulted in reduced airflow which 

led to a persistent single CAC surge condition 

that caused overheat damage to the CAC 

inlet. We are issuing this AD to prevent CAC 

inlet overheating leading to structural 

degradation of the CAC inlet, fumes in the 

cabin and flight deck, and interruption to inservice air conditioning. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Software and Hardware Installation 

Within 36 months after the effective date 

of this AD: Install new pack control unit 

(PCU) software for the cabin air conditioning 

and temperature control system (CACTCS) 

and new CAC outlet pressure sensor J-tube 

hardware, and do all applicable related 

investigative and corrective actions; in 

accordance with the Accomplishment 

Instructions of the applicable service 

information specified in paragraph (g)(1) or 

(g)(2) of this AD. Related investigative and 

corrective actions must be done before 

further flight. 

(1) Boeing Service Bulletin B787–81205– 

SB210075–00, Issue 003, dated March 29, 

2017 (for Boeing Model 787–8 airplanes); or 

Boeing Service Bulletin B787–81205– 

SB210077–00, Issue 004, dated September 

22, 2017 (for Boeing Model 787–9 airplanes). 

(2) Boeing Service Bulletin B787–81205– 

SB210083–00, Issue 001, dated February 9, 

2017 (for all airplanes); and Work Packages 

2 and 3 of the applicable service information 

identified in paragraph (g)(1) of this AD. 

(h) Credit for Previous Actions 

This paragraph provides credit for the 

actions specified in paragraph (g) of this AD, 

if those actions were performed before the 

effective date of this AD using the applicable 

service information specified in paragraphs 

(h)(1) through (h)(5) of this AD. 

(1) Boeing Service Bulletin B787–81205– 

SB210075–00, Issue 001, dated February 24, 

2016 (for Model 787–8 airplanes); 

(2) Boeing Service Bulletin B787–81205– 

SB210075–00, Issue 002, dated May 11, 2016 

(for Model 787–8 airplanes); 

(3) Boeing Service Bulletin B787–81205– 

SB210077–00, Issue 001, dated April 19, 

2016 (for Model 787–9 airplanes); 

(4) Boeing Service Bulletin B787–81205– 

SB210077–00, Issue 002, dated May 11, 2016 

(for Model 787–9 airplanes); 

(5) Boeing Service Bulletin B787–81205– 

SB210077–00, Issue 003, dated October 20, 

2016 (for Model 787–9 airplanes). 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle ACO 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 

certification office, send it to the attention of 

the person identified in paragraph (j) of this 

AD. Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@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 

Branch, 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. 

(j) Related Information 

For more information about this AD, 

contact Allison Buss, Aerospace Engineer, 

Cabin Safety and Environmental Systems 

Section, FAA, Seattle ACO Branch, 2200 

South 216th St., Des Moines, WA 98198; 

phone and fax: 206–231–3564; email: 

allison.buss@faa.gov. 

(k) 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– 

SB210075–00, Issue 003, dated March 29, 

2017; 

(ii) Boeing Service Bulletin B787–81205– 

SB210077–00, Issue 004, dated September 

22, 2017; 

(iii) Boeing Service Bulletin B787–81205– 

SB210083–00, Issue 001, dated February 9, 

2017. 

(3) For The Boeing Company service 

information identified in this AD, contact 

Boeing Commercial Airplanes, Attention: 

Contractual & Data Services (C&DS), 2600 

Westminster Blvd., MC 110–SK57, Seal 

Beach, CA 90740–5600; telephone 562–797– 

1717; internet https://

www.myboeingfleet.com. 

(4) You may view this service information 

at the FAA, Transport Standards Branch, 

2200 South 216th St., Des Moines, WA. For 

information on the availability of this 

material at the FAA, call 206–231–3195. 

(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 Des Moines, Washington, on May 

31, 2018. 

Michael Kaszycki, 

Acting Director, System Oversight Division, 

Aircraft Certification Service. 

[FR Doc. 2018–12285 Filed 6–8–18; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2017–1163; Product 

Identifier 2017–CE–041–AD; Amendment 

39–19260; AD 2018–09–04] 

RIN 2120–AA64 

Airworthiness Directives; Gulfstream 

Aerospace Corporation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. The 

AD applies to certain Gulfstream 

Aerospace Corporation Models G–IV 

and GIV–X airplanes. Paragraphs (h)(3) 

through (5) of the AD incorrectly 

reference Customer Bulletin 238A as 

Customer Bulletin 283A. This document 

corrects that error. In all other respects, 

the original document remains the 


daltland on DSKBBV9HB2PROD with RULES
Federal Register / Vol. 83, No. 112 / Monday, June 11, 2018 / Rules and Regulations 26837 

same; however for the sake of clarity, we 

are publishing the entire rule in the 

Federal Register. 

DATES: The effective date of AD 2018– 

09–04 remains June 11, 2018. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of June 11, 2018 (83 FR 19922, May 

7, 2018). 

ADDRESSES: You may examine the AD 

docket on the internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2017– 

1163; or in person at the Docket 

Operations between 9 a.m. and 5 p.m., 

Monday through Friday, except Federal 

holidays. The AD docket contains this 

final rule, the regulatory evaluation, any 

comments received, and other 

information. The address for the Docket 

Operations (phone: 800–647–5527) is 

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: 

William O. Herderich, Aerospace 

Engineer, Atlanta ACO Branch, FAA, 

1701 Columbia Avenue, College Park, 

Georgia 30337; phone: (404) 474–5547; 

fax: (404) 474–5605; email: 

william.o.herderich@faa.gov. 

SUPPLEMENTARY INFORMATION: AD 2018– 

09–04, Amendment 39–19260 (83 FR 

19922, May 7, 2018), requires 

incorporating new revisions into the 

Instructions for Continued 

Airworthiness of the Limitations section 

of the FAA-approved maintenance 

program (e.g., maintenance manual) that 

establish an inspection cycle for the 

repaired main landing gear side brace 

actuator fittings. 

As published, paragraphs (h)(3) 

through (5) of the AD contain a 

typographical error. The published 

references are Customer Bulletin No. 

283A, dated June 15, 2017, and they 

should be Customer Bulletin No. 238A, 

dated June 15, 2017. 

Although no other part of the 

preamble or regulatory information has 

been corrected, for the sake of clarity, 

we are publishing the entire rule in the 

Federal Register. 

The effective date of this AD remains 

June 11, 2018. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Correction 

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 [Corrected] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2018–09–04 Gulfstream Aerospace 

Corporation: Amendment 39–19260; 

Docket No. FAA–2017–1163; Product 

Identifier 2017–CE–041–AD. 

(a) Effective Date 

This AD is effective June 11, 2018. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the following 

Gulfstream Aerospace Corporation model 

airplanes that are certificated in any category: 

(1) Model G–IV, serial numbers (S/Ns) 

1000 through 1399 having Aircraft Service 

Change (ASC) 416A (MSG–3) incorporated; 

and S/Ns 1400 through 1535; and 

(2) Model GIV–X, S/Ns 4001 through 4355. 

(d) Subject 

Joint Aircraft System Component (JASC)/ 

Air Transport Association (ATA) of America 

Code 32, Landing Gear. 

(e) Unsafe Condition 

This AD was prompted by the potential for 

fatigue cracks in the main landing gear (MLG) 

actuator attachment fitting that had a certain 

repair incorporated. We are issuing this AD 

to prevent failure of the MLG actuator 

attachment. The unsafe condition, if not 

addressed, could compromise the lateral 

support of the MLG during ground 

maneuvers, possibly leading to collapse of 

the affected MLG with consequent loss of 

control. In addition, this condition could also 

cause the MLG side brace to fail, which could 

result in a penetration of the wing fuel tank 

causing an uncontained fire. 

(f) Compliance 

At whichever of the following compliance 

times in paragraphs (f)(1) and (f)(2) that 

occurs later, comply with the actions in 

paragraphs (g) through (i) of this AD, unless 

already done. 

(1) Within the next 100 hours time-inservice after June 11, 2018 (the effective date 

of this AD); or 

(2) Within the next 3 months after June 11, 

2018 (the effective date of this AD). 

(g) Inspect Maintenance Records 

Inspect the airplane maintenance records 

to determine if repair SE05732102 for the 

MLG side brace fitting has been incorporated. 

To do this inspection, use the 

Accomplishment Instructions in Gulfstream 

G350 Customer Bulletin Number 192A; 

Gulfstream G450 Customer Bulletin 192A; 

Gulfstream IV Customer Bulletin Number 

238A; Gulfstream G300 Customer Bulletin 

Number 238A; and Gulfstream G400 

Customer Bulletin Number 238A; all dated 

June 15, 2017, as applicable. The service 

information referenced in this paragraph 

specifies sending a service reply card back to 

Gulfstream Aerospace Corporation if repair 

SE05732102 for the MLG side brace fitting 

has been not been incorporated. This action 

is not required in this AD. 

(h) Determine Initial and Repetitive 

Inspection Requirements 

If it is determined during the maintenance 

records inspection required in paragraph (g) 

that repair SE05732102 for the MLG side 

brace fitting has been incorporated, 

determine the initial and repetitive 

inspection requirements using the 

Accomplishment Instructions of the service 

information identified in paragrap (g) along 

with the following documents, as applicable. 

Comply with the inspection requirements as 

determined. 

(1) Appendix A, Gulfstream Document 

GIV–SGER–553, Revision A, Instructions for 

Continued Airworthiness for Gulfstream 

Repair Drawing SE05732102, dated 

December 14, 2016, to Gulfstream G350 

Customer Bulletin No. 192A, dated June 15, 

2017; 

(2) Appendix A, Gulfstream Document 

GIV–SGER–553, Revision A, Instructions for 

Continued Airworthiness for Gulfstream 

Repair Drawing SE05732102, dated 

December 14, 2016, to Gulfstream G450 

Customer Bulletin No. 192A, dated June 15, 

2017; 

(3) Appendix A, Gulfstream Document 

GIV–SGER–553, Revision A, Instructions for 

Continued Airworthiness for Gulfstream 

Repair Drawing SE05732102, dated 

December 14, 2016, to Gulfstream IV 

Customer Bulletin No. 238A, dated June 15, 

2017; 

(4) Appendix A, Gulfstream Document 

GIV–SGER–553, Revision A, Instructions for 

Continued Airworthiness for Gulfstream 

Repair Drawing SE05732102, dated 

December 14, 2016, to Gulfstream G300 

Customer Bulletin No. 238A, dated June 15, 

2017; and 

(5) Appendix A, Gulfstream Document 

GIV–SGER–553, Revision A, Instructions for 

Continued Airworthiness for Gulfstream 

Repair Drawing SE05732102, dated 

December 14, 2016, to Gulfstream G400 

Customer Bulletin No. 238A, dated June 15, 

2017. 

(i) Revise Limitations Section 

Insert the documents listed in paragraphs 

(h)(1) through (5) of this AD into the 

Instructions for Continued Airworthiness of 

the Limitations section of the FAA-approved 

maintenance program (e.g., maintenance 

manual), as applicable. The revised 

limitations sections establish inspections of 

the repaired MLG side brace actuator fittings. 

(j) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Atlanta ACO Branch, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 


daltland on DSKBBV9HB2PROD with RULES
26838 Federal Register / Vol. 83, No. 112 / Monday, June 11, 2018 / Rules and Regulations 

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 

certification office, send it to the attention of 

the person identified in paragraph (k) of this 

AD. 

(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) For service information that contains 

steps that are labeled as Required for 

Compliance (RC), the provisions of 

paragraphs (g) through (i) of this AD apply. 

(i) The steps labeled as RC, including 

substeps under an RC step and any figures 

identified in an RC step, must be done to 

comply with the AD. An AMOC is required 

for any deviations to RC steps, including 

substeps and identified figures. 

(ii) Steps not labeled 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 RC steps, 

including substeps and identified figures, can 

still be done as specified, and the airplane 

can be put back in an airworthy condition. 

(k) Related Information 

For more information about this AD, 

contact William O. Herderich, Aerospace 

Engineer, Atlanta ACO Branch, FAA, 1701 

Columbia Avenue, College Park, Georgia 

30337; phone: (404) 474–5547; fax: (404) 

474–5605; email: william.o.herderich@

faa.gov. 

(l) 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) Gulfstream G350 Customer Bulletin 

Number 192A, dated June 15, 2017, that 

incorporates Appendix A, Gulfstream 

Document GIV–SGER–553, Revision A, 

Instructions for Continued Airworthiness for 

Gulfstream Repair Drawing SE05732102, 

dated December 14, 2016. 

(ii) Gulfstream G450 Customer Bulletin 

192A, dated June 15, 2017, that incorporates 

Appendix A, Gulfstream Document GIV– 

SGER–553, Revision A, Instructions for 

Continued Airworthiness for Gulfstream 

Repair Drawing SE05732102, dated 

December 14, 2016. 

(iii) Gulfstream IV Customer Bulletin 

Number 238A, dated June 15, 2017, that 

incorporates Appendix A, Gulfstream 

Document GIV–SGER–553, Revision A, 

Instructions for Continued Airworthiness for 

Gulfstream Repair Drawing SE05732102, 

dated December 14, 2016. 

(iv) Gulfstream G300 Customer Bulletin 

Number 238A, dated June 15, 2017, that 

incorporates Appendix A, Gulfstream 

Document GIV–SGER–553, Revision A, 

Instructions for Continued Airworthiness for 

Gulfstream Repair Drawing SE05732102, 

dated December 14, 2016. 

(v) Gulfstream G400 Customer Bulletin 

Number 238A, dated June 15, 2017, that 

incorporates Appendix A, Gulfstream 

Document GIV–SGER–553, Revision A, 

Instructions for Continued Airworthiness for 

Gulfstream Repair Drawing SE05732102, 

dated December 14, 2016. 

(3) For Gulfstream Aerospace Corporation 

service information identified in this AD, 

contact Gulfstream Aerospace Corporation, 

P.O. Box 2206, Savannah, Georgia 31402– 

2206; telephone: (800) 810–4853; fax 912– 

965–3520; email: pubs@gulfstream.com; 

internet: http://www.gulfstream.com/ 

product_support/technical_pubs/pubs/ 

index.htm. 

(4) You may view this service information 

at FAA, Policy and Innovation Division, 901 

Locust, Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329–4148. 

(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 Kansas City, Missouri, on June 5, 

2018. 

David R. Showers, 

Aircraft Certification Service, Acting Deputy 

Director, Policy and Innovation Division, 

AIR–601. 

[FR Doc. 2018–12519 Filed 6–8–18; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2017–0610; Airspace 

Docket No. 17–AEA–13] 

RIN 2120–AA66 

Revocation of Class E Airspace; Seven 

Springs, PA, and Amendment of Class 

E Airspace; Somerset, PA 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule, correction. 

SUMMARY: This action corrects a final 

rule published in the Federal Register 

on April 20, 2018, amending and 

removing Class E airspace at Seven 

Springs, PA, by correcting the 

geographic coordinates in the legal 

description of Class E airspace 

extending upward from 700 feet or more 

above the surface for Somerset County 

Airport. 

DATES: Effective 0901 UTC, July 19, 

2018. The Director of the Federal 

Register approves this incorporation by 

reference action under title 1, Code of 

Federal Regulations, part 51, subject to 

the annual revision of FAA Order 

7400.11 and publication of conforming 

amendments. 

FOR FURTHER INFORMATION CONTACT: John 

Fornito, Operations Support Group, 

Eastern Service Center, Federal Aviation 

Administration, P.O. Box 20636, 

Atlanta, Georgia 30320; telephone (404) 

305–6364. 

SUPPLEMENTARY INFORMATION: 

History 

The FAA published a final rule in the 

Federal Register (83 FR 17480, April 20, 

2018) for Doc. No. FAA–2017–0610, 

amending Class E airspace extending 

upward from 700 feet or more above the 

surface at Somerset County Airport, 

Somerset, PA. Subsequent to 

publication, the FAA found that the 

geographic coordinates of the airport 

listed in the description under Class E 

airspace area extending upward from 

700 feet above the surface were 

incorrect. This action corrects the error. 

Class E airspace designations are 

published in paragraph 6005, of FAA 

Order 7400.11B dated August 3, 2017, 

and effective September 15, 2017, which 

is incorporated by reference in 14 CFR 

part 71.1. The Class E airspace 

designations listed in this document 

will be published subsequently in the 

Order. 

Availability and Summary of 

Documents for Incorporation by 

Reference 

This document amends FAA Order 

7400.11B, Airspace Designations and 

Reporting Points, dated August 3, 2017, 

and effective September 15, 2017. FAA 

Order 7400.11B is publicly available as 

listed in the ADDRESSES section of this 

document. FAA Order 7400.11B lists 

Class A, B, C, D, and E airspace areas, 

air traffic service routes, and reporting 

points. 

Correction to Final Rule 

Accordingly, pursuant to the 

authority delegated to me, in the 

Federal Register of April 20, 2018 (83 

FR 17480) FR Doc. 2018–08037, the 

amendment of Class E Airspace for 

Somerset County Airport, Somerset, PA, 

is corrected as follows: 

§ 71.1 [Amended] 

AEA PA E5 Somerset, PA [Amended] 

■ On page 17481, column 3 line 22, 

remove (Lat. 40°02′20′′ N, long. 

79°00′54′′ W) and add in its place (Lat. 

40°02′19′′ N, long. 79°00′55′′ W). 


daltland on DSKBBV9HB2PROD with RULES