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FR
Regulatory Information
2012_register
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2012-02-27
article
Airworthiness Directives; Airbus Airplanes
Proposed Rules
D09002ee1bdcbfaa7
D09002ee1bdcbfb3d
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
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A300 B4-103, B4-203, and B4-2C airplanes, and Model B4-600, B4-600R, and F4-600R series airplanes, and Model C4-605R Variant F airplanes (collectively called A300-600 series airplanes). This proposed AD was prompted by reports of cracking in the forward lug of the main landing gear (MLG) rib 5 aft bearing attachment. This proposed AD would require repetitive inspections for cracking of the left-hand (LH) and right-hand (RH) wing MLG rib 5 aft bearing forward lugs and repair if necessary. We are proposing this AD to detect and correct cracking of the LH and RH wing MLG rib 5 aft bearing forward lugs which, if not corrected, could affect the structural integrity of the MLG attachment, which could result in MLG collapse during landing or rollout with consequent damage to the airplane and injury to occupants.
77 FR 11793
https://www.govinfo.gov/app/details/FR-2012-02-28/2012-4644
2012-4644
fr28fe12-20
RIN 2120-AA64
4910-13-P
Docket No. FAA-2012-0185
Directorate Identifier 2011-NM-001-AD
https://www.govinfo.gov/app/details/FR-2012-02-28/2012-4644
https://www.govinfo.gov/content/pkg/FR-2012-02-28/html/2012-4644.htm
https://www.govinfo.gov/content/pkg/FR-2012-02-28/pdf/2012-4644.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
4 p.
11793
11796
77 FR 11793
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Airbus Airplanes; Federal Register Vol. 77, Issue
PRORULE
2012-4644
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2012-04-13
Docket No. FAA-2012-0185
Directorate Identifier 2011-NM-001-AD
4910-13-P
2012-4644
Notice of proposed rulemaking (NPRM).
We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A300 B4-103, B4-203, and B4-2C airplanes, and Model B4-600, B4-600R, and F4-600R series airplanes, and Model C4-605R Variant F airplanes (collectively called A300-600 series airplanes). This proposed AD was prompted by reports of cracking in the forward lug of the main landing gear (MLG) rib 5 aft bearing attachment. This proposed AD would require repetitive inspections for cracking of the left-hand (LH) and right-hand (RH) wing MLG rib 5 aft bearing forward lugs and repair if necessary. We are proposing this AD to detect and correct cracking of the LH and RH wing MLG rib 5 aft bearing forward lugs which, if not corrected, could affect the structural integrity of the MLG attachment, which could result in MLG collapse during landing or rollout with consequent damage to the airplane and injury to occupants.
We must receive comments on this proposed AD by April 13, 2012.
Dan Rodina, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 227-2125; fax (425) 227-1149.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
Airbus Airplanes
,
9-ANM-116-AMOC-REQUESTS@faa.gov
account.airworth-eas@airbus.com
sb.reporting@airbus.com
http://www.airbus.com
http://www.regulations.gov
Federal Register
Vol. 77, no. 39
Office of the Federal Register, National Archives and Records Administration
2012-02-28
continuing
daily
deposited
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430 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2012-02-28
P0b002ee181f3d0ca
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr28fe12
https://www.govinfo.gov/app/details/FR-2012-02-28
https://www.govinfo.gov/content/pkg/FR-2012-02-28/pdf/FR-2012-02-28.pdf
https://www.govinfo.gov/content/pkg/FR-2012-02-28/xml/FR-2012-02-28.xml
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2012-02-27
2023-04-30
FR-2012-02-28
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FR-2012-02-28
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