Published 2002-12-11 · Federal Register document 02-31173

Airworthiness Directives; General Electric Company CF34-8C1 Turbofan Engines, Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2002-23-09 applicable to General Electric Company CF34-8C1 turbofan engines that was published in the Federal Register on November 20, 2002 (67 FR 70004). Table 801 was incorrectly numbered in three locations in the AD. This document corrects that number. 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[427]
Raw source SHA-256: c8c2ee537a56d16c3d3246bbaa55e183792a136494260623f45827707b4e2a64

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition: 2002-23-02
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Find all recorded historical references to AD 2002-23-02 · 0 printed reference observations in this pinned collection.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: 3ebc05606b932e3efb642e378bbf73a251af119a4cd711839a85456aae96881e. Source manifest: 2b511aad818f897fe92fa1f6918a75789b7b902fc94a90f5eb4da7f0d3768b7d.

Official source · 2002-12-11

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 238 (Wednesday, December 11, 2002)]
[Rules and Regulations]
[Pages 76111-76112]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-31173]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2002-NE-13-AD; Amendment 39-12946; AD 2002-23-02]
RIN 2120-AA64


Airworthiness Directives; General Electric Company CF34-8C1 
Turbofan Engines, Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2002-23-09 applicable to General Electric Company CF34-8C1 
turbofan engines that was published in the Federal Register on November 
20, 2002 (67 FR 70004). Table 801 was incorrectly numbered in three 
locations in the AD. This document corrects that number. In all other 
respects, the original document remains the same.

EFFECTIVE DATE: December 26, 2002.

FOR FURTHER INFORMATION CONTACT: Keith Mead, Aerospace Engineer, Engine 
Certification Office, FAA, Engine and Propeller Directorate, 12 New 
England Executive Park, Burlington, MA

[[Page 76112]]

01803-5299; telephone (781) 238-7744; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc, 02-29355 applicable 
to General Electric Company CF34-8C1 turbofan engines was published in 
the Federal Register on November 20, 2002 (67 FR 70004). The following 
correction is needed:


Sec.  39.13  [Corrected]

    On page 70005, in the first column, in the Comments Section, in the 
fourth paragraph, in the eighth and again in the thirteenth lines, 
``Table 805'' is corrected to read ``Table 801''. Also on page 70005, 
in the third column in the ninth paragraph, ``Table 805'' is corrected 
to read ``Table 801''.

    Dated: Issued in Burlington, MA, on December 4, 2002.
Francis A. Favara,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 02-31173 Filed 12-10-02; 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 2026-10-09T04:16:38.550410+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256: 71f6c58f2f864a332ef9cff6e7eb236b8fe8778917dfa94508a6dd0c2bacf6be
Text SHA-256: 3ebc05606b932e3efb642e378bbf73a251af119a4cd711839a85456aae96881e

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.