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2010-09-23
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Airworthiness Directives; McDonnell Douglas Model DC-9-15 Airplane
Rules and Regulations
D09002ee1bdea6e01
D09002ee1bdea6eb1
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 a certain McDonnell Douglas Model DC-9-15 airplane, that requires an inspection to detect chafing or overheat damage of the electrical wires located at fuselage station Y=110.000 bulkhead of the lower nose left tunnel; and corrective actions, if necessary. This amendment also requires replacing the external power ground stud with a new ground stud using new attaching parts, torquing new attachments, and installing a nameplate. This action is necessary to prevent loose external power ground wires, which could cause arcing and overheated wire insulation and consequent smoke/fire in the cockpit. This action is intended to address the identified unsafe condition.
69 FR 16785
https://www.govinfo.gov/app/details/FR-2004-03-31/04-6955
04-6955
fr31mr04-8
RIN 2120-AA64
4910-13-P
Docket No. 2003-NM-31-AD
Amendment 39-13552
AD 2004-07-08
https://www.govinfo.gov/app/details/FR-2004-03-31/04-6955
https://www.govinfo.gov/content/pkg/FR-2004-03-31/html/04-6955.htm
https://www.govinfo.gov/content/pkg/FR-2004-03-31/pdf/04-6955.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
2 p.
16785
16786
69 FR 16785
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 DC-9-15 Airplane; Federal Register Vol. 69, Issue
RULE
04-6955
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2004-05-05
Docket No. 2003-NM-31-AD
Amendment 39-13552
AD 2004-07-08
4910-13-P
04-6955
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to a certain McDonnell Douglas Model DC-9-15 airplane, that requires an inspection to detect chafing or overheat damage of the electrical wires located at fuselage station Y=110.000 bulkhead of the lower nose left tunnel; and corrective actions, if necessary. This amendment also requires replacing the external power ground stud with a new ground stud using new attaching parts, torquing new attachments, and installing a nameplate. This action is necessary to prevent loose external power ground wires, which could cause arcing and overheated wire insulation and consequent smoke/fire in the cockpit. This action is intended to address the identified unsafe condition.
Effective May 5, 2004.
Elvin Wheeler, Aerospace Engineer, Systems and Equipment Branch, ANM-130L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5344; fax (562) 627-5210.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
McDonnell Douglas,
Federal Register
Vol. 69, no. 62
Office of the Federal Register, National Archives and Records Administration
2004-03-31
continuing
daily
deposited
born digital
277 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-03-31
P0b002ee180984a31
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr31mr04
https://www.govinfo.gov/app/details/FR-2004-03-31
https://www.govinfo.gov/content/pkg/FR-2004-03-31/pdf/FR-2004-03-31.pdf
https://www.govinfo.gov/content/pkg/FR-2004-03-31/xml/FR-2004-03-31.xml
fdlp
16769
17032
DGPO
2010-09-23
2023-05-04
FR-2004-03-31
machine generated
eng
FR
FR-2004-03-31
69
62