AD 2008-24-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat | Various | Airworthiness Directives; Pratt & Whitney Canada Corp. JT15D-5; -5B; -5F; and -5R Turbofan Engines |
| engine | Pratt & Whitney | Canada Corp | Airworthiness Directives; Pratt & Whitney Canada Corp. JT15D-5; -5B; -5F; and -5R Turbofan Engines |
Unsafe Condition
Excessive moisture and freezing in the Fuel Control Hydro Mechanical Unit (HMU) P3 servo during certain flight conditions can lead to engine flameouts of one or both engines.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and revise the compressor air to HMU delivery tube as specified in the AD. Operators should also refer to the Hawker Beechcraft Service Bulletin (SB) No. SB 73-3888, Revision 1, for instructions to re-route and secure the throttle solenoid wire harness.
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Compliance Time
Within 200 flight hours after the effective date of this AD or within 30 days after the effective date of this AD, whichever occurs first.
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Affected Aircraft
Pratt & Whitney Canada Corp. JT15D-5, -5B, -5F, and -5R Turbofan Engines.
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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