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2010-09-23
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Airworthiness Directives; Rolls-Royce Corporation AE 3007A1E and AE 1107C Turbofan/Turboshaft Engines
Rules and Regulations
D09002ee1bdd7aaac
D09002ee1bdd7ab6c
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
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Corporation (RRC) AE 3007A1E and AE 1107C turbofan/ turboshaft engines. This AD requires removal from service of certain 2nd stage, 3rd stage, and 4th stage compressor wheels, compressor cone shaft assemblies, and 1st to 2nd-stage turbine spacers at new, reduced, published life limits. This AD results from RRC applying an updated lifing methodology to the affected parts. We are issuing this AD to prevent low-cycle-fatigue failure of the parts listed in Table 1 of this AD, which could result in an uncontained engine failure and damage to the aircraft.
74 FR 7309
https://www.govinfo.gov/app/details/FR-2009-02-17/E9-3027
E9-3027
FR17FE09-5
RIN 2120-AA64
4910-13-P
Docket No. FAA-2008-0230
Directorate Identifier 2007-NE-24-AD
Amendment 39-15809
AD 2009-04-03
https://www.govinfo.gov/app/details/FR-2009-02-17/E9-3027
https://www.govinfo.gov/content/pkg/FR-2009-02-17/html/E9-3027.htm
https://www.govinfo.gov/content/pkg/FR-2009-02-17/pdf/E9-3027.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
2 p.
7309
7310
74 FR 7309
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce Corporation AE 3007A1E and AE 1107C Turbofan/Turboshaft Engines; Federal Register Vol. 74, Issue
RULE
E9-3027
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2009-03-24
Docket No. FAA-2008-0230
Directorate Identifier 2007-NE-24-AD
Amendment 39-15809
AD 2009-04-03
4910-13-P
E9-3027
Final rule.
The FAA is adopting a new airworthiness directive (AD) for Rolls-Royce Corporation (RRC) AE 3007A1E and AE 1107C turbofan/ turboshaft engines. This AD requires removal from service of certain 2nd stage, 3rd stage, and 4th stage compressor wheels, compressor cone shaft assemblies, and 1st to 2nd-stage turbine spacers at new, reduced, published life limits. This AD results from RRC applying an updated lifing methodology to the affected parts. We are issuing this AD to prevent low-cycle-fatigue failure of the parts listed in Table 1 of this AD, which could result in an uncontained engine failure and damage to the aircraft.
This AD becomes effective March 24, 2009.
Michael Downs, Aerospace Engineer, Chicago Aircraft Certification Office, Small Airplane Directorate, FAA, 2300 E. Devon Ave., Des Plaines, IL 60018; telephone (847) 294-7870; fax (847) 294-7834.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness Directives:
Rolls-Royce Corporation AE 3007A1E and AE 1107C Turbofan/Turboshaft Engines
,
www.regulations.gov
Federal Register
Vol. 74, no. 30
Office of the Federal Register, National Archives and Records Administration
2009-02-17
continuing
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275 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2009-02-17
P0b002ee1809a7886
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:FR17FE09
https://www.govinfo.gov/app/details/FR-2009-02-17
https://www.govinfo.gov/content/pkg/FR-2009-02-17/pdf/FR-2009-02-17.pdf
https://www.govinfo.gov/content/pkg/FR-2009-02-17/xml/FR-2009-02-17.xml
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2010-09-23
2023-05-02
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