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2010-09-24
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Airworthiness Directives; Airbus Model A300 B2 and A300 B4 Series Airplanes, and Model A300 B4-600, A300 B4-600R, and A300 F4-600R (A300-600) Series Airplanes
Proposed Rules
D09002ee1bdf9a030
D09002ee1bdf9a0a9
United States
Department of Transportation
originator
org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all Airbus Model A300 B2 and A300 B4 series airplanes, and all A300 B4-600, A300 B4-600R, and A300 F4- 600R (A300-600) series airplanes. For certain airplanes, this proposal would require modifying the frame 40 aft fittings. For all airplanes, this proposal would require repetitive nondestructive test inspections to detect cracking of the frame 40 aft fittings; a modification would be required as corrective action for cracking or provided as optional terminating action for the repetitive inspections. This proposal is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by the proposed AD are intended to detect and correct propagation of cracks on the frame 40 aft fittings due to local stress concentrations at the frame 40 upper flange runout, which could result in reduced structural integrity of the airplane.
66 FR 1612
https://www.govinfo.gov/app/details/FR-2001-01-09/01-511
01-511
fr09ja01-23
RIN 2120-AA64
4910-13-U
Docket No. 99-NM-86-AD
https://www.govinfo.gov/app/details/FR-2001-01-09/01-511
https://www.govinfo.gov/content/pkg/FR-2001-01-09/html/01-511.htm
https://www.govinfo.gov/content/pkg/FR-2001-01-09/pdf/01-511.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
5 p.
1612
1616
66 FR 1612
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 B2 and A300 B4 Series Airplanes, and Model A300 B4-600, A300 B4-600R, and A300 F4-600R (A300-600) Series Airplanes; Federal Register Vol. 66, Issue
PRORULE
01-511
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2001-02-08
Docket No. 99-NM-86-AD
4910-13-U
01-511
Notice of proposed rulemaking (NPRM).
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all Airbus Model A300 B2 and A300 B4 series airplanes, and all A300 B4-600, A300 B4-600R, and A300 F4- 600R (A300-600) series airplanes. For certain airplanes, this proposal would require modifying the frame 40 aft fittings. For all airplanes, this proposal would require repetitive nondestructive test inspections to detect cracking of the frame 40 aft fittings; a modification would be required as corrective action for cracking or provided as optional terminating action for the repetitive inspections. This proposal is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by the proposed AD are intended to detect and correct propagation of cracks on the frame 40 aft fittings due to local stress concentrations at the frame 40 upper flange runout, which could result in reduced structural integrity of the airplane.
Comments must be received by February 8, 2001.
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.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Airbus,
Federal Register
Vol. 66, no. 6
Office of the Federal Register, National Archives and Records Administration
2001-01-09
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Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2001-01-09
P0b002ee180a0c88e
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr09ja01
https://www.govinfo.gov/app/details/FR-2001-01-09
https://www.govinfo.gov/content/pkg/FR-2001-01-09/pdf/FR-2001-01-09.pdf
https://www.govinfo.gov/content/pkg/FR-2001-01-09/xml/FR-2001-01-09.xml
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2010-09-24
2023-05-05
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FR-2001-01-09
66
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