AD 2006-20-06

final rule

Airworthiness Directives; General Electric Company CF34-10E Series Turbofan Engines; Correction

AD Number
2006-20-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25896
FR Citation
71 FR 60663
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
engine General Electric Company CF34-10E Series Airworthiness Directives; General Electric Company CF34-10E Series Turbofan Engines; Correction

Unsafe Condition

This document makes a correction to Airworthiness Directive (AD) 2006-20-06. That AD applies to General Electric Company (GE) CF34- 10E series turbofan engines. We published AD 2006-20-06 in the Federal Register on September 29, 2006 (71 FR 57403). The issue date of the AD was inadvertently omitted. This document adds the AD issue date. In all other respects, the original document remains the same.

Affected Aircraft

General Electric Company CF34-10E series turbofan engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

This document makes a correction to Airworthiness Directive (AD) 2006-20-06. That AD applies to General Electric Company (GE) CF34- 10E series turbofan engines. We published AD 2006-20-06 in the Federal Register on September 29, 2006 (71 FR 57403). The issue date of the AD was inadvertently omitted. This document adds the AD issue date. In all other respects, the original document remains the same.

Document Text

Show stored source text (verify against official source)
[Federal Register Volume 71, Number 199 (Monday, October 16, 2006)]
[Rules and Regulations]
[Page 60663]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E6-17007]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-25896; Directorate Identifier 2006-NE-33-AD; 
Amendment 39-14775; AD 2006-20-06]
RIN 2120-AA64


Airworthiness Directives; General Electric Company CF34-10E 
Series Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2006-20-06. That AD applies to General Electric Company (GE) CF34-
10E series turbofan engines. We published AD 2006-20-06 in the Federal 
Register on September 29, 2006 (71 FR 57403). The issue date of the AD 
was inadvertently omitted. This document adds the AD issue date. In all 
other respects, the original document remains the same.

DATES: Effective Date: Effective October 16, 2006.

FOR FURTHER INFORMATION CONTACT: Tara Fitzgerald, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803; telephone (781) 238-
7130; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 06-8284, that 
applies to GE CF34-10E series turbofan engines was published in the 
Federal Register on September 29, 2006 (71 FR 57403). The following 
correction is needed:


Sec.  39.13  [Corrected]

0
On page 57405, in the first column, after compliance paragraph (q), add 
``Issued in Burlington, Massachusetts, on September 21, 2006.''

    Issued in Burlington, MA, on October 6, 2006.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. E6-17007 Filed 10-13-06; 8:45 am]
BILLING CODE 4910-13-P

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.