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2010-09-24
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Airworthiness Directives; Rolls-Royce, plc Models Tay 650-15 and 651-54 Turbofan Engines
Rules and Regulations
D09002ee1bdf4c485
D09002ee1bdf4d28f
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 Rolls-Royce, plc models Tay 650-15 and 651-54 turbofan engines. This amendment requires initial and repetitive visual and ultrasonic inspections of fan blades for cracks, and, if necessary, replacement with serviceable parts. In addition, this AD requires recording instances when engines are operated in a stabilized manner in newly prohibited ranges. This amendment is prompted by reports of fan blade failures. The actions specified by this AD are intended to prevent fan blade failures, which can result in an uncontained engine failure, engine fire, and damage to the airplane.
66 FR 56755
https://www.govinfo.gov/app/details/FR-2001-11-13/01-28024
01-28024
fr13no01-2
RIN 2120-AA64
4910-13-P
Docket No. 98-ANE-68-AD
Amendment 39-12497
AD 2001-22-18
https://www.govinfo.gov/app/details/FR-2001-11-13/01-28024
https://www.govinfo.gov/content/pkg/FR-2001-11-13/html/01-28024.htm
https://www.govinfo.gov/content/pkg/FR-2001-11-13/pdf/01-28024.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
56755
56757
66 FR 56755
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 Models Tay 650-15 and 651-54 Turbofan Engines; Federal Register Vol. 66, Issue
RULE
01-28024
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2001-12-18
Docket No. 98-ANE-68-AD
Amendment 39-12497
AD 2001-22-18
4910-13-P
01-28024
Final rule.
This amendment adopts a new airworthiness directive (AD), that is applicable to Rolls-Royce, plc models Tay 650-15 and 651-54 turbofan engines. This amendment requires initial and repetitive visual and ultrasonic inspections of fan blades for cracks, and, if necessary, replacement with serviceable parts. In addition, this AD requires recording instances when engines are operated in a stabilized manner in newly prohibited ranges. This amendment is prompted by reports of fan blade failures. The actions specified by this AD are intended to prevent fan blade failures, which can result in an uncontained engine failure, engine fire, and damage to the airplane.
Effective date December 18, 2001. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of December 18, 2001.
Richard Woldan, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7136; fax (781) 238-7199.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Rolls-Royce, plc,
Federal Register
Vol. 66, no. 219
Office of the Federal Register, National Archives and Records Administration
2001-11-13
continuing
daily
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born digital
229 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2001-11-13
P0b002ee180a105bd
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr13no01
https://www.govinfo.gov/app/details/FR-2001-11-13
https://www.govinfo.gov/content/pkg/FR-2001-11-13/pdf/FR-2001-11-13.pdf
https://www.govinfo.gov/content/pkg/FR-2001-11-13/xml/FR-2001-11-13.xml
fdlp
56753
56966
DGPO
2010-09-24
2023-05-04
FR-2001-11-13
machine generated
eng
FR
FR-2001-11-13
66
219