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2013-05-02
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Airworthiness Directives; Airbus Airplanes
Proposed Rules
D09002ee1bdca45ba
D09002ee1bdca4623
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
We propose to supersede an existing airworthiness directive (AD) that applies to all Airbus Model A318, A319, A320, and A321 series airplanes. The existing AD currently requires revising the airplane flight manual (AFM) to advise the flightcrew of emergency procedures for addressing angle of attack (AoA) sensor blockage. The existing AD also provides for optional terminating action for the AFM revision, which involves replacing AoA sensor conic plates with AoA sensor flat plates. Since we issued that AD, we have determined that the replacement of AoA sensor conic plates is necessary to address the identified unsafe condition. This proposed AD would mandate the installation of AoA sensor flat plates and removal of the AFM revision. We are proposing this AD to prevent reduced control of the airplane.
78 FR 25666
https://www.govinfo.gov/app/details/FR-2013-05-02/2013-10361
2013-10361
fr02my13-20
RIN 2120-AA64
4910-13-P
Docket No. FAA-2013-0360
Directorate Identifier 2013-NM-033-AD
https://www.govinfo.gov/app/details/FR-2013-05-02/2013-10361
https://www.govinfo.gov/content/pkg/FR-2013-05-02/html/2013-10361.htm
https://www.govinfo.gov/content/pkg/FR-2013-05-02/pdf/2013-10361.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
4 p.
25666
25669
78 FR 25666
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. 78, Issue
PRORULE
2013-10361
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2013-06-17
Docket No. FAA-2013-0360
Directorate Identifier 2013-NM-033-AD
4910-13-P
2013-10361
Notice of proposed rulemaking (NPRM).
We propose to supersede an existing airworthiness directive (AD) that applies to all Airbus Model A318, A319, A320, and A321 series airplanes. The existing AD currently requires revising the airplane flight manual (AFM) to advise the flightcrew of emergency procedures for addressing angle of attack (AoA) sensor blockage. The existing AD also provides for optional terminating action for the AFM revision, which involves replacing AoA sensor conic plates with AoA sensor flat plates. Since we issued that AD, we have determined that the replacement of AoA sensor conic plates is necessary to address the identified unsafe condition. This proposed AD would mandate the installation of AoA sensor flat plates and removal of the AFM revision. We are proposing this AD to prevent reduced control of the airplane.
We must receive comments on this proposed AD by June 17, 2013.
Sanjay Ralhan, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone (425) 227-1405; 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
http://www.airbus.com
http://www.regulations.gov
Federal Register
Vol. 78, no. 85
Office of the Federal Register, National Archives and Records Administration
2013-05-02
continuing
daily
deposited
born digital
230 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2013-05-02
P0b002ee1849b514e
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr02my13
https://www.govinfo.gov/app/details/FR-2013-05-02
https://www.govinfo.gov/content/pkg/FR-2013-05-02/pdf/FR-2013-05-02.pdf
https://www.govinfo.gov/content/pkg/FR-2013-05-02/xml/FR-2013-05-02.xml
fdlp
25565
25785
DGPO
2013-05-02
2023-04-30
FR-2013-05-02
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FR
FR-2013-05-02
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