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2010-09-23
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Airworthiness Directives; Airbus Model A310-200 and -300 Series Airplanes
Proposed Rules
D09002ee1bde29ec2
D09002ee1bde29f1f
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
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A310-200 and -300 series airplanes. This proposed AD would require repetitive inspections for cracks and corrosion of the areas behind the scuff plates below the passenger/crew doors and bulk cargo door, and repair of any cracked or corroded part. This proposed AD also would require repetitive inspections for cracks of the holes of the corner doublers, the fail-safe ring, and the door frames of the passenger/crew door structures. This proposed AD is prompted by reports of corrosion behind the scuff plates at passenger/ crew doors and the bulk cargo door and fatigue cracks on the corner doublers of the forward and aft passenger/crew door frames. We are proposing this AD to prevent such corrosion and fatigue cracking, which could result in reduced structural integrity of the door surroundings.
70 FR 70048
https://www.govinfo.gov/app/details/FR-2005-11-21/05-22971
05-22971
fr21no05-12
RIN 2120-AA64
4910-13-P
Docket No. FAA-2005-23007
Directorate Identifier 2005-NM-013-AD
https://www.govinfo.gov/app/details/FR-2005-11-21/05-22971
https://www.govinfo.gov/content/pkg/FR-2005-11-21/html/05-22971.htm
https://www.govinfo.gov/content/pkg/FR-2005-11-21/pdf/05-22971.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
5 p.
70048
70052
70 FR 70048
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Airbus Model A310-200 and -300 Series Airplanes; Federal Register Vol. 70, Issue
PRORULE
05-22971
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2005-12-21
Docket No. FAA-2005-23007
Directorate Identifier 2005-NM-013-AD
4910-13-P
05-22971
Notice of proposed rulemaking (NPRM).
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A310-200 and -300 series airplanes. This proposed AD would require repetitive inspections for cracks and corrosion of the areas behind the scuff plates below the passenger/crew doors and bulk cargo door, and repair of any cracked or corroded part. This proposed AD also would require repetitive inspections for cracks of the holes of the corner doublers, the fail-safe ring, and the door frames of the passenger/crew door structures. This proposed AD is prompted by reports of corrosion behind the scuff plates at passenger/ crew doors and the bulk cargo door and fatigue cracks on the corner doublers of the forward and aft passenger/crew door frames. We are proposing this AD to prevent such corrosion and fatigue cracking, which could result in reduced structural integrity of the door surroundings.
We must receive comments on this proposed AD by December 21, 2005.
Rosanne Ryburn, Aerospace Engineer, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2139; fax (425) 227-1149.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Airbus,
http://dms.dot.gov
http://www.regulations.gov
Federal Register
Vol. 70, no. 223
Office of the Federal Register, National Archives and Records Administration
2005-11-21
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465 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2005-11-21
P0b002ee180995320
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr21no05
https://www.govinfo.gov/app/details/FR-2005-11-21
https://www.govinfo.gov/content/pkg/FR-2005-11-21/pdf/FR-2005-11-21.pdf
https://www.govinfo.gov/content/pkg/FR-2005-11-21/xml/FR-2005-11-21.xml
fdlp
70031
70481
DGPO
2010-09-23
2023-05-03
FR-2005-11-21
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FR
FR-2005-11-21
70
223