AD 99-06-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Pilatus Aircraft Limited | PC-12 | Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes |
| aircraft | Pilatus Aircraft Limited | PC-12/45 | Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes |
Unsafe Condition
Damage to electrical components because incorrectly connected cables or broken or damaged wires cause excessive voltages to the second generator, which could result in loss of electrical power during any phase of flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install a support bracket and a cut-out relay for the second generator control unit, and make all necessary wiring additions and adjustments. Use Pilatus Service Bulletin No. 24-009 for instructions. Special flight permits may be obtained to operate to a location where AD requirements can be met.
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Compliance Time
Within the next 50 hours time-in-service after the effective date (June 16, 1999).
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Affected Aircraft
Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 airplanes with manufacturer serial numbers 101 through 180.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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