AD Amdt-39-9998

final rule
Data completeness: 70%

Airworthiness Directives; CFM International CFM56-5C Series Turbofan Engines

AD Number
Amdt-39-9998
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 95-ANE-64
FR Citation
62 FR 23642

Applicability

TypeManufacturerModelDetails
engine CFM International CFM56-5C Series Airworthiness Directives; CFM International CFM56-5C Series Turbofan Engines

Unsafe Condition

A low cycle fatigue (LCF) failure of the HPTR front shaft, HPTR front air seal, HPTR disk, booster spool, and LPTR stage 3 disk could result in an uncontained engine failure and damage to the aircraft.

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

Required Actions

Reduce the low cycle fatigue (LCF) retirement lives for certain high pressure turbine rotor (HPTR) front shafts, HPTR front air seals, HPTR disks, booster spools, and low pressure turbine rotor (LPTR) stage 3 disks.

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

Affected Aircraft

CFM International CFM56-5C series turbofan engines with specific components subject to the refined life analysis.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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