[Federal Register Volume 65, Number 213 (Thursday, November 2, 2000)]
[Rules and Regulations]
[Page 65731]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-28090]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98-ANE-43-AD; Amendment 39-11939; AD 2000-21-07]
RIN 2120-AA64


Airworthiness Directives; Pratt & Whitney JT8D-200 Series 
Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2000-21-07 applicable to Pratt & Whitney JT8D-200 series turbofan 
engines that was published in the Federal Register on October 24, 2000 
(65 FR 63540). The statement identifying AD 2000-21-07 as superseding 
AD 99-12-04, Amendment 39-11188 (64 FR 30382, dated June 8, 1999), was 
inadvertently omitted from the AD. This document corrects that 
statement. In all other respects, the original document remains the 
same.

EFFECTIVE DATE: April 23, 2001.

FOR FURTHER INFORMATION CONTACT: Christopher Spinney, Aerospace 
Engineer, Engine Certification Office, FAA, Engine and Propeller 
Directorate, 12 New England Executive Park, Burlington, MA 01803; 
telephone 781-238-7175, fax 781-238-7199.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive (FR 
Doc. 00-26970) applicable to Pratt & Whitney JT8D-200 series turbofan 
engines was published in the Federal Register on October 24, 2000 (65 
FR 63540). The following correction is needed:


Sec. 39.13  [Corrected]

    On page 63541, in the first column, the AD heading is corrected to 
read ``AD 2000-21-07 Pratt & Whitney: Amendment 39-11939. Docket 98-
ANE-43-AD. Supersedes AD 99-12-04, Amendment 39-11188.''

    Issued in Burlington, MA, on October 26, 2000.
David A. Downey,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 00-28090 Filed 11-1-00; 8:45 am]
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