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2017-02-25
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Airworthiness Directives; Rolls-Royce plc Turbofan Engines
Rules and Regulations
D09002ee1bdbf1a08
D09002ee1bdbf1a9b
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
We are adopting a new airworthiness directive (AD) for certain Rolls-Royce plc (RR) Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H turbofan engines. This AD requires initial and repetitive inspections of affected high-pressure turbine (HPT) blades for cracks. This AD was prompted by high engine vibration due to HPT blade deterioration resulting in operational disruptions. We are issuing this AD to correct the unsafe condition on these products.
82 FR 11801
https://www.govinfo.gov/app/details/FR-2017-02-27/2017-03739
2017-03739
fr27fe17-5
RIN 2120-AA64
4910-13-P
Docket No. FAA-2016-9510
Directorate Identifier 2016-NE-28-AD
Amendment 39-18780
AD 2017-02-01
https://www.govinfo.gov/app/details/FR-2017-02-27/2017-03739
https://www.govinfo.gov/content/pkg/FR-2017-02-27/html/2017-03739.htm
https://www.govinfo.gov/content/pkg/FR-2017-02-27/pdf/2017-03739.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
11801
11803
82 FR 11801
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce plc Turbofan Engines; Federal Register Vol. 82, Issue
RULE
2017-03739
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2017-03-14
Docket No. FAA-2016-9510
Directorate Identifier 2016-NE-28-AD
Amendment 39-18780
AD 2017-02-01
4910-13-P
2017-03739
Final rule; request for comments.
We are adopting a new airworthiness directive (AD) for certain Rolls-Royce plc (RR) Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H turbofan engines. This AD requires initial and repetitive inspections of affected high-pressure turbine (HPT) blades for cracks. This AD was prompted by high engine vibration due to HPT blade deterioration resulting in operational disruptions. We are issuing this AD to correct the unsafe condition on these products.
This AD becomes effective March 14, 2017.
Robert Green, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7754; fax: 781- 238-7199; email: robert.green@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
Rolls-Royce plc Turbofan Engines
,
ANE-AD-AMOC@faa.gov
robert.green@faa.gov
http://www.archives.gov/federal-register/cfr/ibr-locations.html
http://www.regulations.gov
http://www.rolls-royce.com/contact/civil_team.jsp
https://customers.rolls-royce.com/public/rollsroycecare
Federal Register
Vol. 82, no. 37
Office of the Federal Register, National Archives and Records Administration
2017-02-27
continuing
daily
deposited
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284 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2017-02-27
P0b002ee193d2952a
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr27fe17
https://www.govinfo.gov/app/details/FR-2017-02-27
https://www.govinfo.gov/content/pkg/FR-2017-02-27/pdf/FR-2017-02-27.pdf
https://www.govinfo.gov/content/pkg/FR-2017-02-27/xml/FR-2017-02-27.xml
fdlp
11789
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DGPO
2017-02-25
2023-04-28
FR-2017-02-27
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FR-2017-02-27
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