AD 2005-07-09

Recurring final rule
Data completeness: 80%

Airworthiness Directives; General Electric Company CF34-8E Series Turbofan Engines

AD Number
2005-07-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2004-NE-06-AD
FR Citation
70 FR 17199

Applicability

TypeManufacturerModelDetails
engine General Electric Company CF34-8E Series Airworthiness Directives; General Electric Company CF34-8E Series Turbofan Engines

Unsafe Condition

Dual-channel electrical signal faults in the master variable geometry (VG) actuator, caused by LVDT coil wire deformation and breakage due to thermal expansion of potting material, leading to an uncommanded reduction of thrust to idle and loss of ability to advance thrust above idle. This could result in multiengine loss of thrust if faults occur simultaneously on more than one engine.

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

Required Actions

Initial review within 10 days after the effective date of the AD, of the airplane computer systems for fault messages, and replacement of actuators reported faulty by the FADEC. Repetitive reviews at intervals not to exceed 10 days are also required. Actuator hardware troubleshooting may be required to identify faulty actuators. Replacement of faulty actuators is required either before further flight or within 10 days of the first fault occurrence.

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

Compliance Time

Within 10 days after the effective date of the AD for initial review and repetitive reviews. Replacement of faulty actuators is required either before further flight or within 10 days of the first fault occurrence.

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

Affected Aircraft

General Electric Company CF34-8E series turbofan engines with master VG actuators, part number 4120T02P02, and PMA actuators identified by P/N 1211508-002, SN 238AE, and SNs 241AE and up.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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