Published 2002-03-06 · Federal Register document 02-5260
Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan Engines, Correction
Publication summary
This document makes a correction to Airworthiness Directive (AD) 2002-03-08, applicable to Pratt & Whitney (PW) PW4000 series turbofan engines, that was published in the Federal Register on February 15, 2002 (67 FR 7061). An engine model number was inadvertently omitted from the regulatory information. This document corrects that omission. In all other respects, the original document remains the same.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:07.262592+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2002-c8c2ee537a56d16c
- Source row
- results[98]
- Raw source SHA-256
- c8c2ee537a56d16c3d3246bbaa55e183792a136494260623f45827707b4e2a64
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2002-03-08
- 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Find all recorded historical references to AD 2002-03-08 · 0 printed reference observations in this pinned collection.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: e188f18060a6ca616edd52c6d81e69c238f7ceab0de30c48168728d11ded4205. Source manifest: a4f932f14dc673910b53bea9d326d9b064e01e8d64d7c14afefd8a779f466ed7.
Official source · 2002-03-06
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 67, Number 44 (Wednesday, March 6, 2002)]
[Rules and Regulations]
[Page 10099]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-5260]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
Prices of new books are listed in the first FEDERAL REGISTER issue of each
week.
========================================================================
Federal Register / Vol. 67, No. 44 / Wednesday, March 6, 2002 / Rules
and Regulations
[[Page 10099]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-ANE-66; Amendment 39-12649; AD 2002-03-08]
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney PW4000 Series Turbofan
Engines, Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule, correction.
-----------------------------------------------------------------------
SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2002-03-08, applicable to Pratt & Whitney (PW) PW4000 series
turbofan engines, that was published in the Federal Register on
February 15, 2002 (67 FR 7061). An engine model number was
inadvertently omitted from the regulatory information. This document
corrects that omission. In all other respects, the original document
remains the same.
EFFECTIVE DATE: April 16, 2002.
FOR FURTHER INFORMATION CONTACT: Robert McCabe, Aerospace Engineer,
Engine Certification Office, FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803-5299; telephone (781)
238-7138, fax (781) 238-7199.
SUPPLEMENTARY INFORMATION: A final rule AD applicable to Pratt &
Whitney (PW) Model PW4050, PW4052, PW4056, PW4060, PW4060A, PW4060C,
PW4062, PW4152, PW4156, PW4156A, PW4158, PW4160, PW4460, PW4462,
PW4650, PW4164, PW4168, PW4168A, PW4074, PW4074D, PW4077, PW4077D,
PW4084, PW4084D, PW4090, PW4090D, and PW4098 turbofan engines,
installed on but not limited to Airbus A300, A310, and A330 series,
Boeing 747, 767, and 777 series, and McDonnell Douglas MD-11 series
airplanes was published in the Federal Register on February 15, 2002
(67 FR 7061). This AD superseded an AD that applied to the PW4090-3
model as well. The PW4090-3 model was included in the Notice of
Proposed Rulemaking and inadvertently left out of the final rule. The
following correction is needed:
Sec. 39.13 [Corrected]
On page 7062, in the Regulatory Information, in the sixth line of
the third column, the engine model applicability is corrected to read
``PW4090, PW4090-3, PW4090D, and PW4098 turbofan.'' Also, on page 7062,
in the Regulatory Information, in the third column, the thirteenth line
of paragraph (a) is corrected to read ``PW4090-3, PW4090D, and PW4098
series turbofan.''
Issued in Burlington, MA, on February 25, 2002.
Thomas A. Boudreau,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 02-5260 Filed 3-5-02; 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 2026-10-09T04:22:07.294724+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 5b26800e503206d4d8766e022951d60368c34071cf799858ed845e7b70f7f584
- Text SHA-256
- e188f18060a6ca616edd52c6d81e69c238f7ceab0de30c48168728d11ded4205
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.