Published 2003-07-16 · Federal Register document 03-17950

Airworthiness Directives; Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) Models 250-C30R/3, -C30R/3M, -C47B, and -C47M Turboshaft Engines; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2003-13-10, applicable to Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) Models 250-C30R/3, -C30R/3M, -C47B, and -C47M turboshaft engines. AD 2003-13-10 was published in the Federal Register on June 30, 2003 (68 FR 38590). In the compliance section, paragraph (f) incorrectly references a compliance date of July 15, 2003 and should reference a compliance date of July 31, 2003. This document corrects that date. In all other respects, the original document remains the same.

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Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 2003-13-10
Effective date printed in this edition: Unknown

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Official source · 2003-07-16

Publication text

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[Federal Register Volume 68, Number 136 (Wednesday, July 16, 2003)]
[Rules and Regulations]
[Page 41906]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 03-17950]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-23-AD; Amendment 39-13210; AD 2003-13-10]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce Corporation (formerly 
Allison Engine Company, Allison Gas Turbine Division, and Detroit 
Diesel Allison) Models 250-C30R/3, -C30R/3M, -C47B, and -C47M 
Turboshaft Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; request for comments, correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2003-13-10, applicable to Rolls-Royce Corporation (formerly 
Allison Engine Company, Allison Gas Turbine Division, and Detroit 
Diesel Allison) Models 250-C30R/3, -C30R/3M, -C47B, and -C47M 
turboshaft engines. AD 2003-13-10 was published in the Federal Register 
on June 30, 2003 (68 FR 38590). In the compliance section, paragraph 
(f) incorrectly references a compliance date of July 15, 2003 and 
should reference a compliance date of July 31, 2003. This document 
corrects that date. In all other respects, the original document 
remains the same.

EFFECTIVE DATE: July 15, 2003.

FOR FURTHER INFORMATION CONTACT: Khailaa Hosny, Aerospace Engineer, 
Chicago Aircraft Certification Office, FAA, 2300 East Devon Avenue, Des 
Plaines, IL 60018-4696; telephone (847) 294-7134; fax (847) 294-7834.

SUPPLEMENTARY INFORMATION: A final rule; request for comments 
airworthiness directive FR DOC. 03-15993, applicable to Rolls-Royce 
Corporation (formerly Allison Engine Company, Allison Gas Turbine 
Division, and Detroit Diesel Allison) Models 250-C30R/3, -C30R/3M, -
C47B, and -C47M turboshaft engines, was published in the Federal 
Register on June 30, 2003 (68 FR 38590). The following correction is 
needed:
    On page 38592, in the first column, under Initial Inspection 
heading, paragraph (f), fifth line, which reads ``no later than July 
15, 2003, in accordance * * * '' is corrected to read ``no later than 
July 31, 2003, in accordance * * * ''.

    Issued in Burlington, MA, on July 10, 2003.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 03-17950 Filed 7-15-03; 8:45 am]
BILLING CODE 4910-13-P

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Source SHA-256: 77beef197b1d28392a99406f03295dc06eda40cb467ddfead77128d635b89c02
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