Aerovidence
Menu
Back to publication catalog

Published 2000-03-23 · Federal Register document 00-6489

Airworthiness Directives; General Electric Company (GE) CF34 Series Turbofan Engines; Correction

Publication summary

This document makes a correction to Airworthiness Directive (AD) 2000-03-03 that is applicable to certain General Electric Company CF34 series turbofan engines that was published in the Federal Register on February 7, 2000 (65 FR 5759). Two subpart names and two mandatory inspections were inadvertently omitted from the Mandatory Inspection Requirements of Table 804. This document corrects this Table by adding the subparts and inspections.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:00.616356+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2000-18aee3630151116d
Source row
results[160]
Raw source SHA-256
18aee3630151116d2fb3a6893673332fd0937cde18bc691722f3a802a62279eb

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2000-03-03
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Find all recorded historical references to AD 2000-03-03 · 0 printed reference observations in this pinned collection.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: 2c6e61ea039194df67f443e4d4a2979b9bb9543123c7428592e7d9e6f403f01a. Source manifest: d8869b75077d5552b2e49a819c90406946148eac12ce198393af11cebde72fca.

Official source · 2000-03-23

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 65, Number 57 (Thursday, March 23, 2000)]
[Rules and Regulations]
[Pages 15536-15537]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-6489]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-NE-49-AD; Amendment 39-11560; AD 2000-03-03]
RIN 2120-AA64


Airworthiness Directives; General Electric Company (GE) CF34 
Series Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2000-03-03 that is applicable to certain General Electric Company 
CF34 series turbofan engines that was published in the Federal Register 
on February 7, 2000 (65 FR 5759). Two subpart names and two mandatory 
inspections were inadvertently omitted from the Mandatory Inspection 
Requirements of Table 804. This document corrects this Table by adding 
the subparts and inspections.

EFFECTIVE DATE: March 23, 2000.

FOR FURTHER INFORMATION CONTACT: Kevin Donovan, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803-5299; telephone (781) 
238-7743, fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive 
applicable to General Electric Company CF34 series turbofan engines, 
was published in the Federal Register on February 7, 2000 (65 FR 5759). 
In the compliance section, an omission was made in Table 804 of the 
Mandatory Inspection Requirements. This correction adds necessary 
subpart names and inspections to the mandatory inspection requirements:


Sec. 39.13  [Corrected]

    1. On page 5760, in AD 2000-03-03, table 804 is corrected to read 
as follows:
* * * * *

[[Page 15537]]



              Table 804.--Mandatory Inspection Requirements
------------------------------------------------------------------------
                                    Chapter/section         Mandatory
      Part name/part No.                subject            inspection
------------------------------------------------------------------------
Fan Disk (all)................  72-21-00, INSPECTION..  All Areas (FPI)
                                                         \1\
                                                        Bores (ECI) \2\
Stage 1 HPT Rotor Disk (all)..  72-46-00, INSPECTION..  All Areas (FPI)
                                                         \1\
                                                        Bores (ECI) \2\
                                                        Boltholes (ECI)
                                                         \2\
                                                        Air Holes (ECI)
                                                         \2\
Stage 2 HPT Rotor Disk (all)..  72-46-00, INSPECTION..  All Areas (FPI)
                                                         \1\
                                                        Bores (ECI) \2\
(a) Boltless Rim Configuration  ......................  Boltholes (FPI)
                                                         \1\
                                                        Air Holes (FPI)
                                                         \1\
(b) Bolted Rim Configuration..  ......................  Boltholes (ECI)
                                                         \2\
                                                        Air Holes (ECI)
                                                         \2\
HPT Rotor Outer Torque........  72-46-00, INSPECTION..  All Areas (FPI)
                                                         \1\
Coupling (all)................  ......................   Bores (ECI) \2\
 
------------------------------------------------------------------------
\1\ FPI = Fluorescent Penetrant Inspection Method.
\2\ ECI = Eddy Current Inspection Method.

---------------------------------------------------------------------------
* * * * *

David A. Downey,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 00-6489 Filed 3-22-00; 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 2026-10-09T04:41:18.034704+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
0b4e710366340d3f14a566d72f1948100c6185aad2d3d5e590d193206431f9ae
Text SHA-256
2c6e61ea039194df67f443e4d4a2979b9bb9543123c7428592e7d9e6f403f01a

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.