Published 2002-07-03 · Federal Register document 02-16534
Airworthiness Directives; Rolls-Royce plc. Tay Model 650-15 and 651-54 Turbofan Engines; Correction
Publication summary
This document makes a correction to Airworthiness Directive (AD) 2002-09-02, applicable to Rolls-Royce plc. (RR) Tay Model 650-15 and 651-54 turbofan engines. AD 2002-09-02 was published in the Federal Register on May 2, 2002 (67 FR 21979). Note 3 in the Alternative Method of Compliance section is incorrect. This document corrects Note 3. In all other respects, the original document remains the same.
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Correction notice · separate source edition
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- 2002-09-02
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Official source · 2002-07-03
Publication text
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Read the complete official publication text
[Federal Register Volume 67, Number 128 (Wednesday, July 3, 2002)]
[Rules and Regulations]
[Pages 44526-44527]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-16534]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-NE-36-AD; Amendment 39-12735; AD 2002-09-02]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce plc. Tay Model 650-15 and
651-54 Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2002-09-02, applicable to Rolls-Royce plc. (RR) Tay Model 650-15
and 651-54 turbofan engines. AD 2002-09-02 was published in the Federal
Register on May 2, 2002 (67 FR 21979). Note 3 in the Alternative Method
of Compliance section is incorrect. This document corrects Note 3. In
all other respects, the original document remains the same.
EFFECTIVE DATE: June 6, 2002.
FOR FURTHER INFORMATION CONTACT: Keith Mead, Aerospace Engineer, Engine
Certification Office, FAA, Engine and Propeller Directorate, 12 New
England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-
7744; fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: A final rule airworthiness directive FR DOC.
02-10549, applicable to RR Tay Model 650-15 and 651-54 turbofan
engines, was published in the Federal Register on May 2, 2002 (67 FR
21979). The following correction is needed:
[[Page 44527]]
Sec. 39.13 [Corrected]
On page 21981, in the first column, in AD 2002-09-02, in the
ALTERNATIVE METHOD OF COMPLIANCE Section, ``Note 3: These record
keeping requirements apply only to the records used to document the
mandatory inspections required as a result of revising the ALS and the
MSS of the Instructions for Continued Airworthiness in the Time Limits
Manual (Chapter 05-10-00) of the Engine Manuals as provided in
paragraph (a) of this AD, and do not alter or amend the record keeping
requirements for any other AD or regulatory requirement'' is corrected
to read ``Note 3: The requirements of this AD have been met when the
engine shop manual changes are made and air carriers have modified
their continuous airworthiness maintenance plans to reflect the
requirements in the engine shop manuals''.
Issued in Burlington, MA, on June 20, 2002.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 02-16534 Filed 7-2-02; 8:45 am]
BILLING CODE 4910-13-P
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