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Published 2010-04-30 · Federal Register document 2010-9962

Airworthiness Directives; General Electric Company (GE) CF34-1A, CF34-3A, and CF34-3B Series Turbofan Engines; Correction

Publication summary

The FAA is correcting airworthiness directive (AD) 2010-01-04, which published in the Federal Register. That AD applies to GE CF34-1A, CF34-3A, and CF34-3B series turbofan engines. The docket number is incorrect in all three of its locations. This document corrects those references. In all other respects, the original document remains the same.

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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:33.146842+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2010-a7267cd3a71dbd26
Source row
results[126]
Raw source SHA-256
a7267cd3a71dbd2645583c8a673df65e4a7fa9360a96e3be0de5b81f9d68c9a0

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2010-01-04
Effective date printed in this edition
Unknown

This correction is a separate source edition; it is not counted as a new adopted rule.

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Find all recorded historical references to AD 2010-01-04 · 0 printed reference observations in this pinned collection.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.

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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: 89bdda36439f9a4051ea949b3ca223747cb94f782964405bb5c25f101cf429fa. Source manifest: 9e78f02d5da7e6aaad98d2f5919eea697d8b441fb9a71286ea6b314a3331a5d8.

Official source · 2010-04-30

Publication text

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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 75, Number 83 (Friday, April 30, 2010)]
[Rules and Regulations]
[Page 22693]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-9962]



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Rules and Regulations
                                                Federal Register
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having general applicability and legal effect, most of which are keyed 
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under 50 titles pursuant to 44 U.S.C. 1510.

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Federal Register / Vol. 75, No. 83 / Friday, April 30, 2010 / Rules 
and Regulations

[[Page 22693]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-0328; Directorate Identifier 2008-NE-44-AD; 
Amendment 39-16161; AD 2010-01-04]
RIN 2120-AA64


Airworthiness Directives; General Electric Company (GE) CF34-1A, 
CF34-3A, and CF34-3B Series Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting airworthiness directive (AD) 2010-01-04, 
which published in the Federal Register. That AD applies to GE CF34-1A, 
CF34-3A, and CF34-3B series turbofan engines. The docket number is 
incorrect in all three of its locations. This document corrects those 
references. In all other respects, the original document remains the 
same.

DATES: Effective April 30, 2010.

FOR FURTHER INFORMATION CONTACT: John Frost, Aerospace Engineer, Engine 
Certification Office, FAA, Engine & Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; phone: (781) 238-7756; 
fax: (781) 238-7199.

SUPPLEMENTARY INFORMATION: On January 8, 2010 (75 FR 1017), we 
published a final rule AD, FR Doc. E9-31274, in the Federal Register. 
That AD applies to GE CF34-1A, CF34-3A, and CF34-3B series turbofan 
engines. We need to make the following correction:


Sec.  39.13  [Corrected]

    On page 1017, in the first column, under 14 CFR Part 39, ``Docket 
No. FAA-2008-0328'' is corrected to read ``Docket No. FAA-2009-0328''.
    On page 1018, in the first column, under Comments Invited, starting 
in the ninth line, ``Docket No. FAA-2008-0328'' is corrected to read 
``Docket No. FAA-2009-0328''.
    On page 1018, in the third column, under Sec.  39.13 [Amended], 
starting in the eighth line, ``Docket No. FAA-2008-0328'' is corrected 
to read ``Docket No. FAA-2009-0328''.

    Issued in Burlington, Massachusetts, on April 23, 2010.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 2010-9962 Filed 4-29-10; 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 2026-10-09T03:16:21.328658+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
ec99e3ef55f61527f261571c271e6796ef0e5466188dc058f4f83f1f58d91739
Text SHA-256
89bdda36439f9a4051ea949b3ca223747cb94f782964405bb5c25f101cf429fa

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