AD 94-07-04

final rule
Data completeness: 70%

Airworthiness Directives; General Electric Company CF6 Series Turbofan Engines

AD Number
94-07-04
Status
final_rule
Effective Date
Product Category
engine
Docket
91-ANE-45
FR Citation
Federal Register: April 21, 1994 (Volume 59, Number 77)

Applicability

TypeManufacturerModelDetails
engine General Electric Company CF6-80A Airworthiness Directives; General Electric Company CF6 Series Turbofan Engines
engine General Electric Company CF6-80A1 Airworthiness Directives; General Electric Company CF6 Series Turbofan Engines
engine General Electric Company CF6-80A2 Airworthiness Directives; General Electric Company CF6 Series Turbofan Engines
engine General Electric Company CF6-80A3 Airworthiness Directives; General Electric Company CF6 Series Turbofan Engines

Unsafe Condition

An uncontained stage 1 high pressure turbine (HPT) disk failure due to cracks in the stage 1 HPT disk rim bolt holes, which could result in an inflight engine shutdown, rejected takeoff, or damage to the aircraft.

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Required Actions

Eddy current inspect (ECI) stage 1 HPT disk rim bolt holes in accordance with GE CF6-80A SB No. 72-604, Revision 3, dated April 8, 1993. Remove and replace cracked disks, and inspect replacements if applicable. Compliance must follow specific cycle thresholds and shop visit requirements outlined in the service bulletin.

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Compliance Time

Compliance required as indicated, with inspections due at next engine shop visit after specific cycle thresholds (e.g., 3,000 cycles since new) or by July 20, 1994, depending on current cycles at AD effective date (May 23, 1994).

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Affected Aircraft

General Electric Company CF6-80A series turbofan engines (models CF6-80A, CF6-80A1, CF6-80A2, CF6-80A3) installed on Boeing 767 and Airbus A310 series aircraft.

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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