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2010-09-24
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Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes
Rules and Regulations
D09002ee1bdfa2e79
D09002ee1bdfa2f30
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) that is applicable to certain Boeing Model 737-100, -200, and -200C series airplanes. This action requires repetitive inspections to detect discrepancies in the upper and lower skins of the fuselage lap joint, and repair, if necessary. This action is necessary to detect and correct such discrepancies, which could result in sudden fracture and failure of a lap joint and rapid decompression of the airplane fuselage.
65 FR 51750
https://www.govinfo.gov/app/details/FR-2000-08-25/00-21615
00-21615
fr25au00-3
RIN 2120-AA64
4910-13-U
Docket No. 2000-NM-288-AD
Amendment 39-11878
AD 2000-17-04
https://www.govinfo.gov/app/details/FR-2000-08-25/00-21615
https://www.govinfo.gov/content/pkg/FR-2000-08-25/html/00-21615.htm
https://www.govinfo.gov/content/pkg/FR-2000-08-25/pdf/00-21615.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
51750
51752
65 FR 51750
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, and -200C Series Airplanes; Federal Register Vol. 65, Issue
RULE
00-21615
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2000-09-11
Docket No. 2000-NM-288-AD
Amendment 39-11878
AD 2000-17-04
4910-13-U
00-21615
Final rule; request for comments.
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Boeing Model 737-100, -200, and -200C series airplanes. This action requires repetitive inspections to detect discrepancies in the upper and lower skins of the fuselage lap joint, and repair, if necessary. This action is necessary to detect and correct such discrepancies, which could result in sudden fracture and failure of a lap joint and rapid decompression of the airplane fuselage.
Effective September 11, 2000.
Scott Fung, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Transport Airplane Directorate, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 227-1221; fax (425) 227-1181.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Boeing,
9-anm-iarcomment@faa.gov
Federal Register
Vol. 65, no. 166
Office of the Federal Register, National Archives and Records Administration
2000-08-25
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261 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2000-08-25
P0b002ee180a010b6
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr25au00
https://www.govinfo.gov/app/details/FR-2000-08-25
https://www.govinfo.gov/content/pkg/FR-2000-08-25/pdf/FR-2000-08-25.pdf
https://www.govinfo.gov/content/pkg/FR-2000-08-25/xml/FR-2000-08-25.xml
fdlp
51747
51996
DGPO
2010-09-24
2023-05-05
FR-2000-08-25
machine generated
eng
FR
FR-2000-08-25
65
166