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
airworthiness · Rule · Final rule; request for comments, correction. · Published 2003-07-16 · 68 FR 41906
Document
Document number
03-17950
Federal Register citation
68 FR 41906
Type
Rule
Action
Final rule; request for comments, correction.
Category
airworthiness
Manufacturer
Rolls-Royce Corporation (formerly Allison
Publication date
2003-07-16
FAA docket
Docket No. 2003-NE-23-AD
Abstract
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.