66 FR 247 pg. 66296 - Airworthiness Directives: Rolls-Royce Corporation (formerly Allison Engine Company) 250-C20 Series Turboshaft and 250-B17 Series Turboprop Engines, Correction
Type: RULEVolume: 66Number: 247Page: 66296
Docket number: [Docket No. 2001-NE-38-AD; Amendment 39-12529; AD 2001-24-12]
FR document: [FR Doc. 01-31327 Filed 12-21-01; 8:45 am]
Agency: Transportation Department
Sub Agency: Federal Aviation Administration
Official PDF Version: PDF Version
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 The AD number being superseded was inadvertently omitted under the PART 39-AIRWORTHINESS DIRECTIVES amendatory instruction 2 in the heading of the AD.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:
§ 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:
2001-24-12Rolls-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]
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