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2010-09-24
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Airworthiness Directives; Airbus Model A300-600 Series Airplanes
Rules and Regulations
D09002ee1bdff5f79
D09002ee1bdff5ff0
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 all Airbus Model A300-600 series airplanes, that requires inspections of the areas behind the scuff plates below the passenger/ crew doors and bulk cargo door to detect cracks and corrosion, and repair, if necessary. This amendment also requires inspections to detect cracking of the holes of the corner doublers, the fail-safe ring, and the door frames of the door structures; and repair, if necessary. In addition, this amendment provides for optional terminating action for certain inspections. This amendment is prompted by reports indicating that corrosion was found behind the scuff plates at exit and cargo doors, and fatigue cracks originated from certain fastener holes located in adjacent structure. The actions specified by this AD are intended to detect and correct such corrosion and fatigue cracking, which could result in reduced structural integrity of the door surroundings.
63 FR 40812
https://www.govinfo.gov/app/details/FR-1998-07-31/98-20337
98-20337
fr31jy98-5
RIN 2120-AA64
4910-13-U
Docket No. 96-NM-42-AD
Amendment 39-10680
AD 98-16-05
https://www.govinfo.gov/app/details/FR-1998-07-31/98-20337
https://www.govinfo.gov/content/pkg/FR-1998-07-31/html/98-20337.htm
https://www.govinfo.gov/content/pkg/FR-1998-07-31/pdf/98-20337.pdf
3 p.
40812
40814
63 FR 40812
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Airbus Model A300-600 Series Airplanes; Federal Register Vol. 63, Issue
RULE
98-20337
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
1998-09-04
Docket No. 96-NM-42-AD
Amendment 39-10680
AD 98-16-05
4910-13-U
98-20337
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A300-600 series airplanes, that requires inspections of the areas behind the scuff plates below the passenger/ crew doors and bulk cargo door to detect cracks and corrosion, and repair, if necessary. This amendment also requires inspections to detect cracking of the holes of the corner doublers, the fail-safe ring, and the door frames of the door structures; and repair, if necessary. In addition, this amendment provides for optional terminating action for certain inspections. This amendment is prompted by reports indicating that corrosion was found behind the scuff plates at exit and cargo doors, and fatigue cracks originated from certain fastener holes located in adjacent structure. The actions specified by this AD are intended to detect and correct such corrosion and fatigue cracking, which could result in reduced structural integrity of the door surroundings.
Effective September 4, 1998.
Norman B. Martenson, Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2110; fax (425) 227-1149.
Federal Register
Vol. 63, no. 147
Office of the Federal Register, National Archives and Records Administration
1998-07-31
continuing
daily
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378 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-1998-07-31
P0b002ee180a78689
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr31jy98
https://www.govinfo.gov/app/details/FR-1998-07-31
https://www.govinfo.gov/content/pkg/FR-1998-07-31/pdf/FR-1998-07-31.pdf
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2010-09-24
2023-05-06
FR-1998-07-31
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FR
FR-1998-07-31
63
147