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2010-09-23
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Airworthiness Directives; McDonnell Douglas Model DC-8-70 and -70F Series Airplanes
Rules and Regulations
D09002ee1bdea7817
D09002ee1bdea789e
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 amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-8-70 and -70F series airplanes, that requires repetitive inspections for cracking of the lower cargo doorjamb corners, and corrective action if necessary. For certain airplanes, this AD provides for optional terminating action for certain repetitive inspections. For certain other airplanes, this AD requires modification of the lower cargo doorjamb corners. This action is necessary to detect and correct cracking in the lower cargo doorjamb corners, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane. This action is intended to address the identified unsafe condition.
69 FR 15234
https://www.govinfo.gov/app/details/FR-2004-03-25/04-6500
04-6500
fr25mr04-2
RIN 2120-AA64
4910-13-P
Docket No. 2001-NM-133-AD
Amendment 39-13532
AD 2004-06-06
https://www.govinfo.gov/app/details/FR-2004-03-25/04-6500
https://www.govinfo.gov/content/pkg/FR-2004-03-25/html/04-6500.htm
https://www.govinfo.gov/content/pkg/FR-2004-03-25/pdf/04-6500.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
15234
15236
69 FR 15234
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; McDonnell Douglas Model DC-8-70 and -70F Series Airplanes; Federal Register Vol. 69, Issue
RULE
04-6500
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2004-04-29
Docket No. 2001-NM-133-AD
Amendment 39-13532
AD 2004-06-06
4910-13-P
04-6500
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model DC-8-70 and -70F series airplanes, that requires repetitive inspections for cracking of the lower cargo doorjamb corners, and corrective action if necessary. For certain airplanes, this AD provides for optional terminating action for certain repetitive inspections. For certain other airplanes, this AD requires modification of the lower cargo doorjamb corners. This action is necessary to detect and correct cracking in the lower cargo doorjamb corners, which could result in rapid decompression of the fuselage and consequent reduced structural integrity of the airplane. This action is intended to address the identified unsafe condition.
Effective April 29, 2004.
Jon Mowery, Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5322; fax (562) 627-5210.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
McDonnell Douglas,
Federal Register
Vol. 69, no. 58
Office of the Federal Register, National Archives and Records Administration
2004-03-25
continuing
daily
deposited
born digital
428 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-03-25
P0b002ee18097fc81
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr25mr04
https://www.govinfo.gov/app/details/FR-2004-03-25
https://www.govinfo.gov/content/pkg/FR-2004-03-25/pdf/FR-2004-03-25.pdf
https://www.govinfo.gov/content/pkg/FR-2004-03-25/xml/FR-2004-03-25.xml
fdlp
15233
15652
DGPO
2010-09-23
2023-05-04
FR-2004-03-25
machine generated
eng
FR
FR-2004-03-25
69
58