Back to publication catalog

Published 2000-11-02 · Federal Register document 00-28090

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

Publication 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.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:00.616356+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2000-18aee3630151116d
Source row
results[488]
Raw source SHA-256
18aee3630151116d2fb3a6893673332fd0937cde18bc691722f3a802a62279eb

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2000-21-07
Effective date printed in this edition
Unknown

This correction is a separate source edition; it is not counted as a new adopted rule.

No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2000-21-07 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 712035f719958da18355270ffb4c8420e4851a3d9e23d8461f4472ca6da5b463. Source manifest: 60be6b64b2029f9434833d38c9d584e9e9625b74d86cb871e9e0534e8cf44e00.

Official source · 2000-11-02

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[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]


-----------------------------------------------------------------------

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.

-----------------------------------------------------------------------

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]
BILLING CODE 4910-13-P


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T04:35:23.959732+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
48e06de47a3d745b48aa684fb07a74679d6ae236c8493c9c7bfcb400ffdef209
Text SHA-256
712035f719958da18355270ffb4c8420e4851a3d9e23d8461f4472ca6da5b463

Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence

Coverage and limits

These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.