Published 1996-05-06 · Federal Register document 96-11172

Airworthiness Directives; Pratt and Whitney JT8D Series Turbofan Engines

Publication summary

This document makes a correction to Airworthiness Directive (AD) 95-26-03 applicable to Pratt & Whitney (PW) JT8D series turbofan engines that was published in the Federal Register on December 27, 1995 (60 FR 66872). An engine model was omitted from the Applicability paragraph. This document adds the omitted engine model. In all other respects, the original document remains the same.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:47.711690+00:00. The title, summary and date are source facts.

Source revision: federal_register_ad_metadata_1996-de90a15e77992e3a
Source row: results[43]
Raw source SHA-256: de90a15e77992e3af396b1c6f02ea423ac0c6519413e915acf4d797175e81157

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 95-26-03
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Find all recorded historical references to AD 95-26-03 · 0 printed reference observations in this pinned collection.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: 542a0d001011baa6baf3c204b1538ee2777ec464352a28495469d46ef3f5a24c. Source manifest: 4c207761e2849ab2603864150a67e2b465fd93652388d821552dd8ca4e81a650.

Official source · 1996-05-06

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 61, Number 88 (Monday, May 6, 1996)]
[Rules and Regulations]
[Page 20125]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-11172]



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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 95-ANE-58; Amendment 39-9461; AD 95-26-03]


Airworthiness Directives; Pratt and Whitney JT8D Series Turbofan 
Engines

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 95-26-03 applicable to Pratt & Whitney (PW) JT8D series turbofan 
engines that was published in the Federal Register on December 27, 1995 
(60 FR 66872). An engine model was omitted from the Applicability 
paragraph. This document adds the omitted engine model. In all other 
respects, the original document remains the same.

DATES: Effective May 6, 1996.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive 
applicable to Pratt & Whitney (PW) JT8D series turbofan engines, was 
published in the Federal Register on December 27, 1995 (60 FR 66872). 
The following correction is needed:
    On page 66874, in the first column, in the Compliance Section, in 
the Applicability paragraph, in the second line, ``Models JT8D-1, -1A, 
-1B, -7, -7A, -9, -9A `` should read ``Models JT8D-1, -1A, -1B, -7, -
7A, -7B. -9, -9A.''

    Issued in Burlington, MA, on April 17, 1996.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 96-11172 Filed 5-3-96; 8:45 am]
BILLING CODE 4910-13-U

Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T05:14:41.614696+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256: 347a08e436eb9b95a34a1771f854a419ef628e92714b7c88733fa5b58a783231
Text SHA-256: 542a0d001011baa6baf3c204b1538ee2777ec464352a28495469d46ef3f5a24c

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.