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Regulatory Information
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2010-09-23
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Airworthiness Directives; Boeing Model 747 Series Airplanes
Proposed Rules
D09002ee1bdec45b6
D09002ee1bdec4654
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 747 series airplanes. This proposal would require repetitive inspections for discrepancies of certain areas of the forward and aft sides of the body station 2598 bulkhead, and repair if necessary. This action is necessary to find and fix such discrepancies of the bulkhead structure, which could result in failure of the structure to carry flight loads of the horizontal stabilizer, and consequent loss of controllability of the airplane. This action is intended to address the identified unsafe condition.
68 FR 18908
https://www.govinfo.gov/app/details/FR-2003-04-17/03-9432
03-9432
fr17ap03-20
RIN 2120-AA64
4910-13-P
Docket No. 2001-NM-324-AD
https://www.govinfo.gov/app/details/FR-2003-04-17/03-9432
https://www.govinfo.gov/content/pkg/FR-2003-04-17/html/03-9432.htm
https://www.govinfo.gov/content/pkg/FR-2003-04-17/pdf/03-9432.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
3 p.
18908
18910
68 FR 18908
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Boeing Model 747 Series Airplanes; Federal Register Vol. 68, Issue
PRORULE
03-9432
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2003-06-02
Docket No. 2001-NM-324-AD
4910-13-P
03-9432
Notice of proposed rulemaking (NPRM).
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Boeing Model 747 series airplanes. This proposal would require repetitive inspections for discrepancies of certain areas of the forward and aft sides of the body station 2598 bulkhead, and repair if necessary. This action is necessary to find and fix such discrepancies of the bulkhead structure, which could result in failure of the structure to carry flight loads of the horizontal stabilizer, and consequent loss of controllability of the airplane. This action is intended to address the identified unsafe condition.
Comments must be received by June 2, 2003.
Rick Kawaguchi, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6434; fax (425) 917-6590.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Boeing,
9-anm-nprmcomment@faa.gov
Federal Register
Vol. 68, no. 74
Office of the Federal Register, National Archives and Records Administration
2003-04-17
continuing
daily
deposited
born digital
313 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2003-04-17
P0b002ee1809cd0a0
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr17ap03
https://www.govinfo.gov/app/details/FR-2003-04-17
https://www.govinfo.gov/content/pkg/FR-2003-04-17/pdf/FR-2003-04-17.pdf
https://www.govinfo.gov/content/pkg/FR-2003-04-17/xml/FR-2003-04-17.xml
fdlp
18833
19133
DGPO
2010-09-23
2023-05-04
FR-2003-04-17
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eng
FR
FR-2003-04-17
68
74