Rules and Regulations. Final rule; correction
/register/2000/11/02/00-28091·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
Agency: Federal Aviation Administration, DOT
Action: Final rule; correction
Citation: FR Doc. 00-28091 · RIN 2120-AA64 · Docket No. 98-ANE-48-AD; Amendment 39-11940; AD 2000-21-08 · 14 CFR 39
Summary
This document makes a correction to Airworthiness Directive (AD) 2000-21-08 applicable to Pratt & Whitney JT8D series turbofan engines that was published in the Federal Register on October 24, 2000 (65 FR 63537). The statement identifying AD 2000-21-08 as superseding AD 99-12-03, Amendment 39-11187 (64 FR 30379, 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.
Supplementary Information
A final rule airworthiness directive (FR Doc. 00-26971) applicable to Pratt & Whitney JT8D series turbofan engines was published in the Federal Register on October 24, 2000 (65 FR 63537). The following correction is needed: § 39.13 [Corrected] On page 63539, in the first column, the AD heading is corrected to read “AD 2000-21-08 Pratt & Whitney: Amendment 39-11940. Docket 98-ANE-48-AD. Supersedes AD 99-12-03, Amendment 39-11187.”. Issued in Burlington, MA, on October 26, 2000. David A. Downey, Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 00-28091 Filed 11-1-00; 8:45 am]
Connections1 off-index
- 14 CFR 39