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2019_register
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2019-12-07
article
Airworthiness Directives; The Boeing Company Airplanes
Rules and Regulations
D09002ee1bdb679b5
D09002ee1bdb67a12
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 airplanes. This AD was prompted by a report of fatigue cracking in the lug root radius of a main landing gear (MLG) aft hanger link lug fitting. This AD requires repetitive surface high frequency eddy current (HFEC) inspections of the left and right side MLG aft hanger link lug fitting for cracking, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
84 FR 67174
https://www.govinfo.gov/app/details/FR-2019-12-09/2019-26401
2019-26401
fr09de19-3
RIN 2120-AA64
4910-13-P
Docket No. FAA-2019-0671
Product Identifier 2019-NM-080-AD
Amendment 39-19788
AD 2019-22-09
https://www.govinfo.gov/app/details/FR-2019-12-09/2019-26401
https://www.govinfo.gov/content/pkg/FR-2019-12-09/html/2019-26401.htm
https://www.govinfo.gov/content/pkg/FR-2019-12-09/pdf/2019-26401.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
67174
67176
84 FR 67174
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes; Federal Register Vol. 84, Issue
RULE
2019-26401
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2020-01-13
Docket No. FAA-2019-0671
Product Identifier 2019-NM-080-AD
Amendment 39-19788
AD 2019-22-09
4910-13-P
2019-26401
Final rule.
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 airplanes. This AD was prompted by a report of fatigue cracking in the lug root radius of a main landing gear (MLG) aft hanger link lug fitting. This AD requires repetitive surface high frequency eddy current (HFEC) inspections of the left and right side MLG aft hanger link lug fitting for cracking, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products.
This AD is effective January 13, 2020.
Greg Rutar, Aerospace Engineer, Airframe Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3529; email: greg.rutar@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
The Boeing Company Airplanes,
9-ANM-Seattle-ACO-AMOC-Requests@faa.gov
fedreg.legal@nara.gov
greg.rutar@faa.gov
https://www.archives.gov/federal-register/cfr/ibr-locations.html
https://www.myboeingfleet.com
https://www.regulations.gov
Federal Register
Vol. 84, no. 236
Office of the Federal Register, National Archives and Records Administration
2019-12-09
continuing
daily
deposited
born digital
182 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2019-12-09
P0b002ee1a3f18b68
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr09de19
https://www.govinfo.gov/app/details/FR-2019-12-09
https://www.govinfo.gov/content/pkg/FR-2019-12-09/pdf/FR-2019-12-09.pdf
https://www.govinfo.gov/content/pkg/FR-2019-12-09/xml/FR-2019-12-09.xml
fdlp
67169
67341
DGPO
2019-12-07
2023-04-28
FR-2019-12-09
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eng
FR
FR-2019-12-09
84
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