AD 96-26-01

final rule
Data completeness: 70%

Airworthiness Directives; General Electric Aircraft Engines CT7 Series Turboprop Engines

AD Number
96-26-01
Status
final_rule
Effective Date
Product Category
engine
Docket
96-ANE-06
FR Citation
Federal Register: January 08, 1997 (Volume 62, Number 5)

Applicability

TypeManufacturerModelDetails
engine General Electric Company CT7-5A2 Airworthiness Directives; General Electric Aircraft Engines CT7 Series Turboprop Engines
engine General Electric Company CT7-7A Airworthiness Directives; General Electric Aircraft Engines CT7 Series Turboprop Engines
engine General Electric Company CT7-9B Airworthiness Directives; General Electric Aircraft Engines CT7 Series Turboprop Engines
engine General Electric Company CT7-9C Airworthiness Directives; General Electric Aircraft Engines CT7 Series Turboprop Engines

Unsafe Condition

Gas generator turbine stage 2 forward cooling plate failure, which could result in an uncontained engine failure.

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

Required Actions

Replace gas generator turbine stage 2 forward cooling plates prior to reaching new reduced cyclic life limits specified in GE SB A72-381. Establish new cyclic life limits of 8,000 cycles since new (CSN) for P/N 6064T10P01 with specific serial numbers, 12,000 CSN for P/N 6064T10P01 and 5086T91P02 on CT7-5A2/-7A engines, and 9,000 CSN for P/N 6064T10P01 and 5086T91P02 on CT7-9B/-9C engines.

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

Compliance Time

Within 30 days after the effective date of this AD, or prior to reaching the new, reduced cyclic life limits listed in GE SB A72-381, whichever occurs later.

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

Affected Aircraft

General Electric Aircraft Engines CT7-5A2, -7A, -9B, and -9C turboprop engines with gas generator turbine stage 2 forward cooling plates P/N 6064T10P01 and P/N 5086T91P02 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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