AD 97-06-14

final rule
Data completeness: 70%

Airworthiness Directives; General Electric Company CF34 Series Turbofan Engines

AD Number
97-06-14
Status
final_rule
Effective Date
Product Category
engine
Docket
95-ANE-19
FR Citation
Federal Register: March 26, 1997 (Volume 62, Number 58)

Applicability

TypeManufacturerModelDetails
engine General Electric Aircraft Engines CF34-1A Airworthiness Directives; General Electric Company CF34 Series Turbofan Engines
engine General Electric Aircraft Engines CF34-3A Airworthiness Directives; General Electric Company CF34 Series Turbofan Engines
engine General Electric Aircraft Engines CF34-3A2 Airworthiness Directives; General Electric Company CF34 Series Turbofan Engines

Unsafe Condition

Fan disk rupture, engine failure, and damage to the aircraft due to exceeding the allowable operating cyclic life limit for affected fan disks.

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

Required Actions

Remove from service fan disks with part numbers 6020T62G04, 6020T62G05, 6078T00G01, or 5921T54G01 prior to accumulating 9,000 cycles in service (CIS) since new. Replace with a serviceable part (fan disk with less than 9,000 CIS).

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

Compliance Time

Required as indicated, unless accomplished previously.

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

Affected Aircraft

General Electric Company CF34-1A, -3A, and -3A2 turbofan engines with fan disk part numbers 6020T62G04, 6020T62G05, 6078T00G01, or 5921T54G01 installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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