AD 2002-09-02

final rule

Airworthiness Directives; Rolls-Royce plc. Tay Model 650-15 and 651-54 Turbofan Engines; Correction

AD Number
2002-09-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NE-36-AD
FR Citation
67 FR 44526
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Deutschland Ltd & Co KG TAY 650-15 Airworthiness Directives; Rolls-Royce plc. Tay Model 650-15 and 651-54 Turbofan Engines
engine Rolls-Royce Deutschland Ltd & Co KG TAY 651-54 Airworthiness Directives; Rolls-Royce plc. Tay Model 650-15 and 651-54 Turbofan Engines

Unsafe Condition

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.

Required Actions

Correct Note 3 in the Alternative Method of Compliance section.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Rolls-Royce plc. Tay Model 650-15 and 651-54 turbofan engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

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.

Document Text

Show stored source text (verify against official source)
[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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