AD 96-04-01

final rule
Data completeness: 70%

Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines

AD Number
96-04-01
Status
final_rule
Effective Date
Product Category
engine
Docket
95-ANE-54
FR Citation
Federal Register: February 29, 1996 (Volume 61, Number 41)

Applicability

TypeManufacturerModelDetails
engine Honeywell International Inc. TFE731-2 Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-2A Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-2B Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-2BR Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-2C Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-3 Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-3A Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-3AR Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-3B Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines
engine Honeywell International Inc. TFE731-3BR Airworthiness Directives; AlliedSignal Inc. TFE731 Series Turbofan Engines

Unsafe Condition

Fatigue cracking in the dovetail slots of fan rotor disks due to undetected cracks during eddy current inspections, which can result in uncontained failure, inflight engine shutdowns, severe secondary damage, and fan rotor assembly separation from the engine.

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

Required Actions

Reinspect 33 additional fan rotor disks beyond those required by AD 93-25-16 using improved eddy current inspection procedures per AlliedSignal Alert Service Bulletin TFE731-A72-3578. Replace cracked disks with serviceable parts.

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

AlliedSignal Inc. TFE731-2, -2A, -3, -3R series turbofan engines with fan rotor disks part numbers 3072162-1 through -4, 3073436-1 through -4, 3073539-2, and 3074529-2 installed on specified aircraft models.

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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