AD 2002-01-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | GE | Various | Airworthiness Directives; GE Aircraft Engines CT7 Series Turboprop Engines |
Unsafe Condition
Stage 2 turbine aft cooling plate cracking, resulting in an uncontained engine failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove stage 2 turbine aft cooling plates of a certain part number (P/N) and install cooling plates of a new design.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
GE Aircraft Engines CT7 series turboprop engines with specific stage 2 turbine aft cooling plates.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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