AD 2001-24-12

final rule

Airworthiness Directives: Rolls-Royce Corporation (formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines, Correction

AD Number
2001-24-12
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2001-NE-38-AD
FR Citation
66 FR 66296
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
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]]

=======================================================================
-----------------------------------------------------------------------

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.