Published 2001-12-26 · Federal Register document 01-31327

Airworthiness Directives: Rolls-Royce Corporation (formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines, Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2001-24-12 applicable to Rolls-Royce Corporation (formerly Allison Engine Company) 250-C20 series turboshaft and 250-B17 series turboprop engines, that was published in the Federal Register on December 4, 2001 (66 FR 62915). The AD number being superseded was inadvertently omitted under the PART 39--AIRWORTHINESS DIRECTIVES amendatory instruction 2 in the heading of the AD. This document corrects that omission. In all other respects, the original document remains the same.

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Source revision: federal_register_ad_metadata_2001-8d66ddb74aa17366
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Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 2001-24-12
Effective date printed in this edition: Unknown

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Official source · 2001-12-26

Publication text

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Read the complete official publication text

[Federal Register Volume 66, Number 247 (Wednesday, December 26, 2001)]
[Rules and Regulations]
[Page 66296]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 01-31327]



[[Page 66296]]

=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2001-NE-38-AD; Amendment 39-12529; AD 2001-24-12]
RIN 2120-AA64


Airworthiness Directives: Rolls-Royce Corporation (formerly 
Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series 
Turboprop Engines, Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2001-24-12 applicable to Rolls-Royce Corporation (formerly Allison 
Engine Company) 250-C20 series turboshaft and 250-B17 series turboprop 
engines, that was published in the Federal Register on December 4, 2001 
(66 FR 62915). The AD number being superseded was inadvertently omitted 
under the PART 39--AIRWORTHINESS DIRECTIVES amendatory instruction 2 in 
the heading of the AD. This document corrects that omission. In all 
other respects, the original document remains the same.

EFFECTIVE DATE: December 19, 2001.

FOR FURTHER INFORMATION CONTACT: John Tallarovic, Aerospace Engineer, 
Chicago Aircraft Certification Office, FAA, Small Airplane Directorate, 
2300 East Devon Avenue, Des Plaines, IL 60018; telephone (847) 294-
8180, fax (847) 294-7834.

SUPPLEMENTARY INFORMATION: A final rule; request for comments 
airworthiness directive applicable to Rolls-Royce Corporation (formerly 
Allison Engine Company) 250-C20 series turboshaft and 250-B17 series 
turboprop engines was published in the Federal Register on December 4, 
2001 (66 FR 62915). The following correction is needed:


Sec. 39.13  [Corrected]

    On page 62916, in the first column, under PART 39--AIRWORTHINESS 
DIRECTIVES, amendatory instruction 2, the heading of the AD is 
corrected to read as follows:

2001-24-12  Rolls-Royce Corporation (formerly Allison Engine 
Company): Amendment 39-12529. Docket No. 2001-NE-38-AD. Supersedes 
AD 2001-20-51.


    Issued in Burlington, Massachusetts, on December 14, 2001.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 01-31327 Filed 12-21-01; 8:45 am]
BILLING CODE 4910-13-U

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