Airworthiness Directives: Rolls-Royce Corporation (formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines, Correction
airworthiness · Rule · Final rule; correction. · Published 2001-12-26 · 66 FR 66296
Document
Document number
01-31327
Federal Register citation
66 FR 66296
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Publication date
2001-12-26
FAA docket
Docket No. 2001-NE-38-AD
Abstract
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 The AD number being superseded was inadvertently omitted under the PART 39--AIRWORTHINESS DIRECTIVES amendatory instruction 2 in the heading of the AD.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.