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Airworthiness Directives; Airbus Model A300 B2, A300 B4, A300 B4-600, and A300 B4-600R Series Airplanes; and Model A300 F4-605R Airplanes
Rules and Regulations
D09002ee1bdeffb65
D09002ee1bdeffbff
United States
Department of Transportation
originator
org
United States Government Agency or Subagency
United States
Federal Aviation Administration
originator
org
United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A300 B2, A300 B4, A300 B4-600, and A300 B4-600R series airplanes, and Model A300 F4-605R airplanes. This AD requires repetitive inspections for cracking of certain fittings, corrective action if necessary, and, for certain airplanes, a modification. This AD also provides an optional terminating action for the repetitive inspections. The actions specified by this AD are intended to detect and correct propagation of cracks on the frame 40 aft fittings due to local stress concentrations at the upper flange runout of frame 40, which could result in reduced structural integrity of the airplane. This action is intended to address the identified unsafe condition.
67 FR 16983
https://www.govinfo.gov/app/details/FR-2002-04-09/02-8278
02-8278
fr09ap02-5
RIN 2120-AA64
4910-13-P
Docket No. 99-NM-86-AD
Amendment 39-12699
AD 2002-07-05
https://www.govinfo.gov/app/details/FR-2002-04-09/02-8278
https://www.govinfo.gov/content/pkg/FR-2002-04-09/html/02-8278.htm
https://www.govinfo.gov/content/pkg/FR-2002-04-09/pdf/02-8278.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
5 p.
16983
16987
67 FR 16983
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, A300 B4, A300 B4-600, and A300 B4-600R Series Airplanes; and Model A300 F4-605R Airplanes; Federal Register Vol. 67, Issue
RULE
02-8278
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2002-05-14
Docket No. 99-NM-86-AD
Amendment 39-12699
AD 2002-07-05
4910-13-P
02-8278
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A300 B2, A300 B4, A300 B4-600, and A300 B4-600R series airplanes, and Model A300 F4-605R airplanes. This AD requires repetitive inspections for cracking of certain fittings, corrective action if necessary, and, for certain airplanes, a modification. This AD also provides an optional terminating action for the repetitive inspections. The actions specified by this AD are intended to detect and correct propagation of cracks on the frame 40 aft fittings due to local stress concentrations at the upper flange runout of frame 40, which could result in reduced structural integrity of the airplane. This action is intended to address the identified unsafe condition.
Effective May 14, 2002.
Dan Rodina, Aerospace Engineer, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2125; fax (425) 227-1149.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Airbus,
Federal Register
Vol. 67, no. 68
Office of the Federal Register, National Archives and Records Administration
2002-04-09
continuing
daily
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319 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2002-04-09
P0b002ee1809b44e8
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr09ap02
https://www.govinfo.gov/app/details/FR-2002-04-09
https://www.govinfo.gov/content/pkg/FR-2002-04-09/pdf/FR-2002-04-09.pdf
https://www.govinfo.gov/content/pkg/FR-2002-04-09/xml/FR-2002-04-09.xml
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16969
17278
DGPO
2010-09-23
2023-05-04
FR-2002-04-09
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FR
FR-2002-04-09
67
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