AD 2000-15-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | CFM | International CFM56-2 | Airworthiness Directives; CFM International CFM56-2, -2A, -2B, -3, -3B, -3C, -5, -5A, -5B, -5C Series Turbofan Engines |
Unsafe Condition
Fuel pump filter cover helicoil inserts have loosened or pulled out, potentially causing fuel leakage between the fuel pump filter cover and gear housing, which could result in an engine fire and damage to the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Initial and repetitive visual inspections of the fuel pump filter cover helicoil inserts and bolts for damage, repair or replacement with serviceable parts if necessary, and installation of new or reworked fuel pumps with an improved filter cover retention design (D-bolts) or an on-wing repair of existing fuel pumps as terminating action.
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Compliance Time
Within 5 years of the effective date or at the next shop visit, whichever occurs first.
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Affected Aircraft
CFM International CFM56-2, -2A, -2B, -3, -3B, -3C, -5, -5A, -5B, -5C series turbofan 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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