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2010-09-23
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Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747SR, and 747SP Series Airplanes
Rules and Regulations
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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 amendment adopts a new airworthiness directive (AD), applicable to certain Boeing airplane models, that requires a one-time inspection to identify all H-11 steel bolts installed in the latch fittings of the cargo doors, repetitive inspections for cracked or broken H-11 steel bolts, and follow-on and corrective actions if necessary. This amendment also requires eventual replacement of all H- 11 steel bolts in the latch fittings of the cargo doors with Inconel bolts. This action is necessary to prevent broken bolts in the latch fittings, which could reduce the capability of the door latch to keep the door closed, and result in loss of a cargo door and consequent rapid depressurization of the airplane. This action is intended to address the identified unsafe condition.
68 FR 74167
https://www.govinfo.gov/app/details/FR-2003-12-23/03-31195
03-31195
fr23de03-6
RIN 2120-AA64
4910-13-P
Docket No. 2001-NM-180-AD
Amendment 39-13394
AD 2003-25-11
https://www.govinfo.gov/app/details/FR-2003-12-23/03-31195
https://www.govinfo.gov/content/pkg/FR-2003-12-23/html/03-31195.htm
https://www.govinfo.gov/content/pkg/FR-2003-12-23/pdf/03-31195.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
74167
74169
68 FR 74167
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747SR, and 747SP Series Airplanes; Federal Register Vol. 68, Issue
RULE
03-31195
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2004-01-27
Docket No. 2001-NM-180-AD
Amendment 39-13394
AD 2003-25-11
4910-13-P
03-31195
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing airplane models, that requires a one-time inspection to identify all H-11 steel bolts installed in the latch fittings of the cargo doors, repetitive inspections for cracked or broken H-11 steel bolts, and follow-on and corrective actions if necessary. This amendment also requires eventual replacement of all H- 11 steel bolts in the latch fittings of the cargo doors with Inconel bolts. This action is necessary to prevent broken bolts in the latch fittings, which could reduce the capability of the door latch to keep the door closed, and result in loss of a cargo door and consequent rapid depressurization of the airplane. This action is intended to address the identified unsafe condition.
Effective January 27, 2004.
Nick Kusz, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6432; fax (425) 917-6590.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Boeing,
Federal Register
Vol. 68, no. 246
Office of the Federal Register, National Archives and Records Administration
2003-12-23
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311 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2003-12-23
P0b002ee1809e43d7
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr23de03
https://www.govinfo.gov/app/details/FR-2003-12-23
https://www.govinfo.gov/content/pkg/FR-2003-12-23/pdf/FR-2003-12-23.pdf
https://www.govinfo.gov/content/pkg/FR-2003-12-23/xml/FR-2003-12-23.xml
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2010-09-23
2023-05-04
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FR-2003-12-23
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