AD 2004-04-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Company CT58 Series and T58 Series | Airworthiness Directives; General Electric Company CT58 Series and T58 Series Turboshaft Engines |
Unsafe Condition
A certain population of fuel flow divider end caps could crack, causing large volumes of fuel leakage, which could lead to an engine fire, in-flight engine shutdown, and forced landing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove from service certain fuel flow divider assemblies. Inspect and replace cracked fuel flow divider end caps as necessary.
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
General Electric Company CT58-100-2, CT58-140-1, CT58-140-2, and T58-GE-1, T58-GE-3, T58-GE-5, T58-GE-8E, T58-GE-8F, T58-GE-10, T58-GE-100, and T58-GE-402 turboshaft engines.
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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