Rules and Regulations. Final rule; request for comments, correction
/register/2003/07/16/03-17950·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
Agency: Federal Aviation Administration, DOT
Action: Final rule; request for comments, correction
Citation: FR Doc. 03-17950 · RIN 2120-AA64 · Docket No. 2003-NE-23-AD; Amendment 39-13210; AD 2003-13-10 · 14 CFR 39
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.
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]
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- 14 CFR 39