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2010-09-22
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Airworthiness Directives; Airbus Models A330-202, -203, -223, -243, and -300 Series Airplanes
Proposed Rules
D09002ee1bdea8f9f
D09002ee1bdea903f
United States
Department of Transportation
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United States Government Agency or Subagency
United States
Federal Aviation Administration
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United States Government Agency or Subagency
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A330-202, - 203, -223, -243, and -300 series airplanes. This proposal would require modification of the control box of the auxiliary power unit (APU). This action is necessary to prevent uncommanded in-flight shutdown of the APU, which could result in loss of critical electrical systems when the airplane is operated in emergency electrical configuration, and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
69 FR 10369
https://www.govinfo.gov/app/details/FR-2004-03-05/04-4926
04-4926
fr05mr04-24
RIN 2120-AA64
4910-13-P
Docket No. 2003-NM-272-AD
https://www.govinfo.gov/app/details/FR-2004-03-05/04-4926
https://www.govinfo.gov/content/pkg/FR-2004-03-05/html/04-4926.htm
https://www.govinfo.gov/content/pkg/FR-2004-03-05/pdf/04-4926.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
2 p.
10369
10370
69 FR 10369
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Airbus Models A330-202, -203, -223, -243, and -300 Series Airplanes; Federal Register Vol. 69, Issue
PRORULE
04-4926
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2004-04-05
Docket No. 2003-NM-272-AD
4910-13-P
04-4926
Notice of proposed rulemaking (NPRM).
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A330-202, - 203, -223, -243, and -300 series airplanes. This proposal would require modification of the control box of the auxiliary power unit (APU). This action is necessary to prevent uncommanded in-flight shutdown of the APU, which could result in loss of critical electrical systems when the airplane is operated in emergency electrical configuration, and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
Comments must be received by April 5, 2004.
Tim Backman, Aerospace Engineer, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2797; fax (425) 227-1149.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Airbus,
9-anm-nprmcomment@faa.gov
Federal Register
Vol. 69, no. 44
Office of the Federal Register, National Archives and Records Administration
2004-03-05
continuing
daily
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291 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-03-05
P0b002ee18096e745
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr05mr04
https://www.govinfo.gov/app/details/FR-2004-03-05
https://www.govinfo.gov/content/pkg/FR-2004-03-05/pdf/FR-2004-03-05.pdf
https://www.govinfo.gov/content/pkg/FR-2004-03-05/xml/FR-2004-03-05.xml
fdlp
10313
10594
DGPO
2010-09-22
2023-05-04
FR-2004-03-05
machine generated
eng
FR
FR-2004-03-05
69
44