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2010-09-23
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Airworthiness Directives; Allison Engine Company, Inc. AE 3007A and AE 3007C Series Turbofan Engines
Rules and Regulations
D09002ee1bdfa7e5f
D09002ee1bdfa7f28
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) that is applicable to Allison Engine Company, Inc. AE 3007A and AE 3007C series turbofan engines. This AD requires the removal from service of certain turbine wheels before exceeding new, reduced cyclic life limits. This amendment is prompted by a refined life analysis that was performed by the manufacturer. The actions specified by this AD are intended to prevent an uncontained turbine wheel failure, which could result in damage to the airplane.
65 FR 40981
https://www.govinfo.gov/app/details/FR-2000-07-03/00-16232
00-16232
fr03jy00-7
RIN 2120-AA64
4910-13-U
Docket No. 99-NE-15-AD
Amendment 39-11800
AD 2000-13-01
https://www.govinfo.gov/app/details/FR-2000-07-03/00-16232
https://www.govinfo.gov/content/pkg/FR-2000-07-03/html/00-16232.htm
https://www.govinfo.gov/content/pkg/FR-2000-07-03/pdf/00-16232.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
40981
40983
65 FR 40981
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Allison Engine Company, Inc. AE 3007A and AE 3007C Series Turbofan Engines; Federal Register Vol. 65, Issue
RULE
00-16232
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2000-09-01
Docket No. 99-NE-15-AD
Amendment 39-11800
AD 2000-13-01
4910-13-U
00-16232
Final rule.
This amendment adopts a new airworthiness directive (AD) that is applicable to Allison Engine Company, Inc. AE 3007A and AE 3007C series turbofan engines. This AD requires the removal from service of certain turbine wheels before exceeding new, reduced cyclic life limits. This amendment is prompted by a refined life analysis that was performed by the manufacturer. The actions specified by this AD are intended to prevent an uncontained turbine wheel failure, which could result in damage to the airplane.
Effective date September 1, 2000. The incorporation by reference of certain publications listed in the rule is approved by the Director of the Federal Register as of September 1, 2000.
John Tallarovic, Aerospace Engineer, Chicago Aircraft Certification Office, FAA, Small Airplane Directorate, 2300 East Devon Avenue, Des Plaines, IL 60018; telephone (847) 294- 8180, fax (847) 294-7834.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Allison Engine Co.,
Federal Register
Vol. 65, no. 128
Office of the Federal Register, National Archives and Records Administration
2000-07-03
continuing
daily
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365 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2000-07-03
P0b002ee1809efb9e
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr03jy00
https://www.govinfo.gov/app/details/FR-2000-07-03
https://www.govinfo.gov/content/pkg/FR-2000-07-03/pdf/FR-2000-07-03.pdf
https://www.govinfo.gov/content/pkg/FR-2000-07-03/xml/FR-2000-07-03.xml
fdlp
40967
41319
DGPO
2010-09-23
2023-05-05
FR-2000-07-03
machine generated
eng
FR
FR-2000-07-03
65
128