Published 1995-06-29 · Federal Register document 95-15557

Airworthiness Directives; Pratt & Whitney JT8D Series Turbofan Engines

Publication summary

This document makes a correction to Airworthiness Directive (AD) 95-10-10 applicable to certain Pratt & Whitney (PW) JT8D series turbofan engines that was published in the Federal Register on May 22, 1995 (60 FR 27020). The complete listing of affected PW JT8D series turbofan engines in the Applicability paragraph was inadvertently omitted. This document corrects the Applicability paragraph. In all other respects, the original document remains the same.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:45.181447+00:00. The title, summary and date are source facts.

Source revision: federal_register_ad_metadata_1995-d388da652c36fb86
Source row: results[71]
Raw source SHA-256: d388da652c36fb862a990338aa93565a36590a27a9a9051dd7d67a85eb7db2e9

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 95-10-10
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Find all recorded historical references to AD 95-10-10 · 0 printed reference observations in this pinned collection.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: 17a5e54d5e54377b21e23fe36b7f95e768837a47b589340487b47b69493366fa. Source manifest: f2793e53477e1f688868fd3929a11756c10527567ad84a521809a7a38a9ec480.

Official source · 1995-06-29

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 60, Number 125 (Thursday, June 29, 1995)]
[Rules and Regulations]
[Page 33683]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 95-15557]



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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 94-ANE-21; Amendment 39-9227; AD 95-10-10]


Airworthiness Directives; Pratt & Whitney JT8D Series Turbofan 
Engines

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 95-10-10 applicable to certain Pratt & Whitney (PW) JT8D series 
turbofan engines that was published in the Federal Register on May 22, 
1995 (60 FR 27020). The complete listing of affected PW JT8D series 
turbofan engines in the Applicability paragraph was inadvertently 
omitted. This document corrects the Applicability paragraph. In all 
other respects, the original document remains the same.

DATES: Effective July 21, 1995.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive 
applicable to Pratt & Whitney (PW) JT8D series turbofan engines, was 
published in the Federal Register on May 22, 1995 (60 FR 27020). The 
following correction is needed:
    On page 27021, in the third column, in the Applicability paragraph, 
in the third paragraph, third line, that begins with ``-17, and -17AR 
turbofan engines. ``, it should read ``-17, and -17AR turbofan engines 
containing front compressor fan hub Part Number (P/N) 817401 with the 
following serial numbers: J78892 through J80538, K32019 through K34018, 
L32197 through L34133, or M05722 through M07296; and all serial numbers 
of fan hubs P/N 594301, 640601, 743301, 749801, 750101, 791801, and 
806001. These engines are installed on but not limited to Boeing 727 
and 737 series, and McDonnell Douglas DC-9 series aircraft.''

    Issued in Burlington, MA, on June 14, 1995.
Robert Guyotte,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 95-15557 Filed 6-28-95; 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 2026-10-09T05:16:21.086993+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256: 74bec3a512729c4ac696ab7d116d1cd8665dabacdbb5c099a2a31d2e23a5cd1c
Text SHA-256: 17a5e54d5e54377b21e23fe36b7f95e768837a47b589340487b47b69493366fa

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.