Back to publication catalog

Published 2005-01-24 · Federal Register document 05-1215

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

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2004-26-04. That AD applies to Pratt & Whitney (PW) JT8D-200 series turbofan engines. That AD was published in the Federal Register on January 5, 2005 (70 FR 677). This document corrects a compliance time in Table 1 of the AD. In all other respects, the original document remains the same.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:17.300228+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2005-5d43d153038ee1c1
Source row
results[38]
Raw source SHA-256
5d43d153038ee1c1c214f5c3688e38e25e37b832227fe65d52f7420a65ee20f2

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2004-26-04
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Find all recorded historical references to AD 2004-26-04 · 0 printed reference observations in this pinned collection.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: 93a6db1425ddd309df0a5a91acbdfb1e6b85aeeca466c2ddfbc6e3b3380212e0. Source manifest: 0a01d95b7401146b926940014d377f1c86593aae0e885f12f4d551c87186fd80.

Official source · 2005-01-24

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 70, Number 14 (Monday, January 24, 2005)]
[Rules and Regulations]
[Page 3299]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-1215]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 92-ANE-15-AD; Amendment 39-13916; AD 2004-26-04]
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) 2004-26-04. That AD applies to Pratt & Whitney (PW) JT8D-200 
series turbofan engines. That AD was published in the Federal Register 
on January 5, 2005 (70 FR 677). This document corrects a compliance 
time in Table 1 of the AD. In all other respects, the original document 
remains the same.

DATES: Effective February 9, 2005.

FOR FURTHER INFORMATION CONTACT: Keith Lardie, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803-5299; telephone (781) 
238-7189; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 05-84, that applies 
to PW JT8D-200 series turbofan engines, was published in the Federal 
Register on January 5, 2005 (70 FR 677). The following correction is 
needed:


Sec.  39.13  [Corrected]

0
On page 678, in Table 1, right-hand column, ``At the next engine shop 
visit after the effective date of this AD, but no later than December 
31, 2004'' is corrected to read ``Before further flight''.

    Issued in Burlington, MA, on January 14, 2005.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 05-1215 Filed 1-21-05; 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 2026-10-09T03:59:17.597007+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
6f64932eedf4eb268cfd095d3eb79668f575df2037fa85580d996aecde105058
Text SHA-256
93a6db1425ddd309df0a5a91acbdfb1e6b85aeeca466c2ddfbc6e3b3380212e0

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.