AD 2001-24-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Rolls-Royce Corporation | 250-B17 | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-B17C | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-B17D | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-B17E | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-B17F | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-B17F/1 | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-B17F/2 | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20 | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20B | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20F | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20J | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20R | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20R/1 | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20R/2 | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20S | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
| engine | Rolls-Royce Corporation | 250-C20W | [Correction] Airworthiness Directives; Rolls-Royce Corporation (Formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines |
Unsafe Condition
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 resp...
Affected Aircraft
Rolls-Royce Corporation (formerly Allison Engine Company) 250-C20 series turboshaft and 250-B17 series turboprop engines
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register 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.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 66, Number 247 (Wednesday, December 26, 2001)]
[Rules and Regulations]
[Page 66296]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 01-31327]
[[Page 66296]]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-NE-38-AD; Amendment 39-12529; AD 2001-24-12]
RIN 2120-AA64
Airworthiness Directives: Rolls-Royce Corporation (formerly
Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series
Turboprop Engines, Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: 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.
EFFECTIVE DATE: December 19, 2001.
FOR FURTHER INFORMATION CONTACT: John Tallarovic, Aerospace Engineer,
Chicago Aircraft Certification Office, FAA, Small Airplane Directorate,
2300 East Devon Avenue, Des Plaines, IL 60018; telephone (847) 294-
8180, fax (847) 294-7834.
SUPPLEMENTARY INFORMATION: A final rule; request for comments
airworthiness directive applicable to Rolls-Royce Corporation (formerly
Allison Engine Company) 250-C20 series turboshaft and 250-B17 series
turboprop engines was published in the Federal Register on December 4,
2001 (66 FR 62915). The following correction is needed:
Sec. 39.13 [Corrected]
On page 62916, in the first column, under PART 39--AIRWORTHINESS
DIRECTIVES, amendatory instruction 2, the heading of the AD is
corrected to read as follows:
2001-24-12 Rolls-Royce Corporation (formerly Allison Engine
Company): Amendment 39-12529. Docket No. 2001-NE-38-AD. Supersedes
AD 2001-20-51.
Issued in Burlington, Massachusetts, on December 14, 2001.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 01-31327 Filed 12-21-01; 8:45 am]
BILLING CODE 4910-13-U
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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