Airworthiness Directives; Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) Models 250-C28, -C28B, and -C28C Turboshaft Engines; Correction
airworthiness · Rule · Final rule; correction. · Published 2005-08-11 · Effective 2005-08-11 · 70 FR 46754
Document
Document number
05-15896
Federal Register citation
70 FR 46754
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Manufacturer
Rolls-Royce Corporation (formerly Allison
Publication date
2005-08-11
Effective date
2005-08-11
FAA docket
Docket No. FAA-2004-18538
Abstract
This document makes a correction to Airworthiness Directive (AD) 2004-14-02. That AD applies to Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) models 250-C28, -C28B, and -C28C turboshaft engines with certain serial number (SN) third-stage turbine wheels, part number (P/N) 6899383. We published AD 2004-14-02 in the Federal Register on July 9, 2004 (69 FR 41389). The SUMMARY and the SUPPLEMENTAL INFORMATION paragraphs each have a sentence that is not clear. This document corrects these two sentences. In all other respects, the original document remains the same.