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2010-09-22
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Airworthiness Directives; Rolls-Royce Corporation (RRC) AE 3007A Series Turbofan Engines
Rules and Regulations
D09002ee1bdd7edc4
D09002ee1bdd7f11d
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 superseding emergency airworthiness directive (AD) 2008-19-51 that we sent previously to all known U.S. owners and operators of RRC AE 3007A series turbofan engines. That AD requires performing initial and repetitive eddy current inspections (ECIs) on the high-pressure turbine (HPT) stage 2 wheel for cracks. This AD continues to require those same inspections, but revises the compliance schedule for the initial inspection and specifies the affected HPT stage 2 wheels by part number (P/N). This AD results from reports of cracked HPT stage 2 wheels. We are issuing this AD to detect cracks in the HPT stage 2 wheel, which could result in a possible uncontained failure of the HPT stage 2 wheel and damage to the airplane.
73 FR 78927
https://www.govinfo.gov/app/details/FR-2008-12-24/E8-30051
E8-30051
fr24de08-3
RIN 2120-AA64
4910-13-P
Docket No. FAA-2008-0975
Directorate Identifier 2008-NE-29-AD
Amendment 39-15772
AD 2008-26-06
https://www.govinfo.gov/app/details/FR-2008-12-24/E8-30051
https://www.govinfo.gov/content/pkg/FR-2008-12-24/html/E8-30051.htm
https://www.govinfo.gov/content/pkg/FR-2008-12-24/pdf/E8-30051.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
3 p.
78927
78929
73 FR 78927
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 (RRC) AE 3007A Series Turbofan Engines; Federal Register Vol. 73, Issue
RULE
E8-30051
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2009-01-08
Docket No. FAA-2008-0975
Directorate Identifier 2008-NE-29-AD
Amendment 39-15772
AD 2008-26-06
4910-13-P
E8-30051
Final rule; request for comments.
The FAA is superseding emergency airworthiness directive (AD) 2008-19-51 that we sent previously to all known U.S. owners and operators of RRC AE 3007A series turbofan engines. That AD requires performing initial and repetitive eddy current inspections (ECIs) on the high-pressure turbine (HPT) stage 2 wheel for cracks. This AD continues to require those same inspections, but revises the compliance schedule for the initial inspection and specifies the affected HPT stage 2 wheels by part number (P/N). This AD results from reports of cracked HPT stage 2 wheels. We are issuing this AD to detect cracks in the HPT stage 2 wheel, which could result in a possible uncontained failure of the HPT stage 2 wheel and damage to the airplane.
Effective January 8, 2009.
Kyri Zaroyiannis, Aerospace Engineer, Chicago Aircraft Certification Office, Small Airplane Directorate, FAA, 2300 E. Devon Ave., Des Plaines, IL 60018; e-mail: kyri.zaroyiannis@faa.gov; telephone (847) 294-7836; fax (847) 294-7834.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness Directives:
Rolls-Royce Corp. (RRC) AE 3007A Series Turbofan Engines,
indy.pubs.services@rolls-royce.com
kyri.zaroyiannis@faa.gov
http://www.regulations.gov
royce.com
Federal Register
Vol. 73, no. 248
Office of the Federal Register, National Archives and Records Administration
2008-12-24
continuing
daily
deposited
born digital
363 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2008-12-24
P0b002ee18093a954
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr24de08
https://www.govinfo.gov/app/details/FR-2008-12-24
https://www.govinfo.gov/content/pkg/FR-2008-12-24/pdf/FR-2008-12-24.pdf
https://www.govinfo.gov/content/pkg/FR-2008-12-24/xml/FR-2008-12-24.xml
fdlp
78917
79265
DGPO
2010-09-22
2023-05-02
FR-2008-12-24
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eng
FR
FR-2008-12-24
73
248