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2010-09-24
article
Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes
Proposed Rules
D09002ee1bdfa8439
D09002ee1bdfa84b0
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
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Boeing Model 737-100, - 200, -300, -400, and -500 series airplanes. This proposal would require inspection of wire bundles in two junction boxes in the main wheel well to detect chafing or damage, and follow-on actions. This action is necessary to prevent wire damage, which could result in arcing and consequent fire in the main wheel well or passenger cabin, or inability to stop the flow of fuel to an engine or to the auxiliary power unit in the event of a fire. This action is intended to address the identified unsafe condition.
65 FR 39574
https://www.govinfo.gov/app/details/FR-2000-06-27/00-16237
00-16237
fr27jn00-27
RIN 2120-AA64
4910-13-P
Docket No. 2000-NM-146-AD
https://www.govinfo.gov/app/details/FR-2000-06-27/00-16237
https://www.govinfo.gov/content/pkg/FR-2000-06-27/html/00-16237.htm
https://www.govinfo.gov/content/pkg/FR-2000-06-27/pdf/00-16237.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
3 p.
39574
39576
65 FR 39574
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes; Federal Register Vol. 65, Issue
PRORULE
00-16237
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2000-08-11
Docket No. 2000-NM-146-AD
4910-13-P
00-16237
Notice of proposed rulemaking (NPRM).
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Boeing Model 737-100, - 200, -300, -400, and -500 series airplanes. This proposal would require inspection of wire bundles in two junction boxes in the main wheel well to detect chafing or damage, and follow-on actions. This action is necessary to prevent wire damage, which could result in arcing and consequent fire in the main wheel well or passenger cabin, or inability to stop the flow of fuel to an engine or to the auxiliary power unit in the event of a fire. This action is intended to address the identified unsafe condition.
Comments must be received by August 11, 2000.
Stephen Oshiro, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Transport Airplane Directorate, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-2793; fax (425) 227-1181.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Boeing,
9-anm-nprmcomment@faa.gov
Federal Register
Vol. 65, no. 124
Office of the Federal Register, National Archives and Records Administration
2000-06-27
continuing
daily
deposited
born digital
280 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2000-06-27
P0b002ee180a03126
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr27jn00
https://www.govinfo.gov/app/details/FR-2000-06-27
https://www.govinfo.gov/content/pkg/FR-2000-06-27/pdf/FR-2000-06-27.pdf
https://www.govinfo.gov/content/pkg/FR-2000-06-27/xml/FR-2000-06-27.xml
fdlp
39507
39778
DGPO
2010-09-24
2023-05-05
FR-2000-06-27
machine generated
eng
FR
FR-2000-06-27
65
124