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2010-09-24
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Airworthiness Directives; Boeing Model 767 Series Airplanes
Rules and Regulations
D09002ee1bdfc6179
D09002ee1bdfc621d
United States
Department of Transportation
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United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 767 series airplanes, that requires detailed visual inspections to detect corrosion or chrome plating cracks on the fuse pins of the outboard support of the main landing gear (MLG) beam. This AD also would require either installation of the existing fuse pins and repetitive inspections; or installation of newer-type fuse pins, which constitutes terminating action for the repetitive inspections. This amendment is prompted by a report indicating that corrosion was found on a fuse pin in the outboard support of the MLG beam. The actions specified by this AD are intended to detect and correct such corrosion and cracking, which could result in the failure of a fuse pin and, consequently, lead to collapse of the MLG.
64 FR 29778
https://www.govinfo.gov/app/details/FR-1999-06-03/99-13878
99-13878
fr03jn99-2
RIN 2120-AA64
4910-13-U
Docket No. 97-NM-51-AD
Amendment 39-11185
AD 99-11-14
https://www.govinfo.gov/app/details/FR-1999-06-03/99-13878
https://www.govinfo.gov/content/pkg/FR-1999-06-03/html/99-13878.htm
https://www.govinfo.gov/content/pkg/FR-1999-06-03/pdf/99-13878.pdf
4 p.
29778
29781
64 FR 29778
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Boeing Model 767 Series Airplanes; Federal Register Vol. 64, Issue
RULE
99-13878
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
1999-07-08
Docket No. 97-NM-51-AD
Amendment 39-11185
AD 99-11-14
4910-13-U
99-13878
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 767 series airplanes, that requires detailed visual inspections to detect corrosion or chrome plating cracks on the fuse pins of the outboard support of the main landing gear (MLG) beam. This AD also would require either installation of the existing fuse pins and repetitive inspections; or installation of newer-type fuse pins, which constitutes terminating action for the repetitive inspections. This amendment is prompted by a report indicating that corrosion was found on a fuse pin in the outboard support of the MLG beam. The actions specified by this AD are intended to detect and correct such corrosion and cracking, which could result in the failure of a fuse pin and, consequently, lead to collapse of the MLG.
Effective July 8, 1999.
James G. Rehrl, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington; telephone (425) 227-2783; fax (425) 227-1181.
Federal Register
Vol. 64, no. 106
Office of the Federal Register, National Archives and Records Administration
1999-06-03
continuing
daily
deposited
born digital
179 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-1999-06-03
P0b002ee180a4da06
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr03jn99
https://www.govinfo.gov/app/details/FR-1999-06-03
https://www.govinfo.gov/content/pkg/FR-1999-06-03/pdf/FR-1999-06-03.pdf
fdlp
29777
29944
DGPO
2010-09-24
2023-05-05
FR-1999-06-03
machine generated
eng
FR
FR-1999-06-03
64
106