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2011-04-27
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Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 501-D Series Turboprop Engines
Rules and Regulations
D09002ee1bdec5488
D09002ee1bdec59ae
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), that is applicable to Rolls-Royce Corporation (formerly Allison Engine Company) 501-D series turboprop engines. This amendment requires removal from service of certain turbine rotor components at reduced life limits. This amendment is prompted by the result of recalculated material properties by the manufacturer. The actions specified by this AD are intended to prevent uncontained turbine rotor failure resulting in in-flight engine shutdown and possible damage to the airplane.
68 FR 15937
https://www.govinfo.gov/app/details/FR-2003-04-02/03-7743
03-7743
fr02ap03-4
RIN 2120-AA64
4910-13-P
Docket No. 2001-NE-01-AD
Amendment 39-13098
AD 2003-07-02
https://www.govinfo.gov/app/details/FR-2003-04-02/03-7743
https://www.govinfo.gov/content/pkg/FR-2003-04-02/html/03-7743.htm
https://www.govinfo.gov/content/pkg/FR-2003-04-02/pdf/03-7743.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
3 p.
15937
15939
68 FR 15937
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 (Formerly Allison Engine Company) 501-D Series Turboprop Engines; Federal Register Vol. 68, Issue
RULE
03-7743
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2003-05-07
Docket No. 2001-NE-01-AD
Amendment 39-13098
AD 2003-07-02
4910-13-P
03-7743
Final rule.
This amendment adopts a new airworthiness directive (AD), that is applicable to Rolls-Royce Corporation (formerly Allison Engine Company) 501-D series turboprop engines. This amendment requires removal from service of certain turbine rotor components at reduced life limits. This amendment is prompted by the result of recalculated material properties by the manufacturer. The actions specified by this AD are intended to prevent uncontained turbine rotor failure resulting in in-flight engine shutdown and possible damage to the airplane.
Effective May 7, 2003.
Michael Downs, Aerospace Engineer, Chicago Aircraft Certification Office, FAA, 2300 East Devon Avenue, Des Plaines, IL 60018; telephone (847) 294-7870; fax (847) 294-7834.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Rolls-Royce Corp.,
Federal Register
Vol. 68, no. 63
Office of the Federal Register, National Archives and Records Administration
2003-04-02
continuing
daily
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253 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2003-04-02
P0b002ee180ce0f1a
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr02ap03
https://www.govinfo.gov/app/details/FR-2003-04-02
https://www.govinfo.gov/content/pkg/FR-2003-04-02/pdf/FR-2003-04-02.pdf
https://www.govinfo.gov/content/pkg/FR-2003-04-02/xml/FR-2003-04-02.xml
fdlp
15921
16163
DGPO
2011-04-27
2023-05-04
FR-2003-04-02
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eng
FR
FR-2003-04-02
68
63