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2010-09-23
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Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes
Rules and Regulations
D09002ee1bdef7faa
D09002ee1bdef803b
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
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD-90-30 airplanes, that requires modification of the main battery ground stud and installation of a nameplate which indicates torque requirements for the ground stud nut. The actions specified by this AD are intended to prevent the ground stud nut from being inadequately tightened or becoming loose, which could result in electrical arcing between the ground stud and the adjacent structure, leading to damage to electrical or electronic equipment or possibly to fire in the airplane.
67 FR 34818
https://www.govinfo.gov/app/details/FR-2002-05-16/02-12066
02-12066
fr16my02-2
RIN 2120-AA64
4910-13-P
Docket No. 2000-NM-198-AD
Amendment 39-12747
AD 2002-10-01
https://www.govinfo.gov/app/details/FR-2002-05-16/02-12066
https://www.govinfo.gov/content/pkg/FR-2002-05-16/html/02-12066.htm
https://www.govinfo.gov/content/pkg/FR-2002-05-16/pdf/02-12066.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
34818
34820
67 FR 34818
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes; Federal Register Vol. 67, Issue
RULE
02-12066
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2002-06-20
Docket No. 2000-NM-198-AD
Amendment 39-12747
AD 2002-10-01
4910-13-P
02-12066
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD-90-30 airplanes, that requires modification of the main battery ground stud and installation of a nameplate which indicates torque requirements for the ground stud nut. The actions specified by this AD are intended to prevent the ground stud nut from being inadequately tightened or becoming loose, which could result in electrical arcing between the ground stud and the adjacent structure, leading to damage to electrical or electronic equipment or possibly to fire in the airplane.
Effective June 20, 2002.
George Mabuni, Aerospace Engineer, Systems and Equipment Branch, ANM-130L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5341; fax (562) 627-5210.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
McDonnell Douglas,
Federal Register
Vol. 67, no. 95
Office of the Federal Register, National Archives and Records Administration
2002-05-16
continuing
daily
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187 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2002-05-16
P0b002ee1809cb471
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr16my02
https://www.govinfo.gov/app/details/FR-2002-05-16
https://www.govinfo.gov/content/pkg/FR-2002-05-16/pdf/FR-2002-05-16.pdf
https://www.govinfo.gov/content/pkg/FR-2002-05-16/xml/FR-2002-05-16.xml
fdlp
34817
34990
DGPO
2010-09-23
2023-05-04
FR-2002-05-16
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eng
FR
FR-2002-05-16
67
95