AD Amdt-39-11081

final rule
Data completeness: 70%

Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes

AD Number
Amdt-39-11081
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-CE-03-AD
FR Citation
64 FR 13882

Applicability

TypeManufacturerModelDetails
aircraft Pilatus Aircraft Ltd Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes

Unsafe Condition

Incorrectly connected cables or broken/damaged wires cause excessive voltages to the second generator, potentially leading to loss of electrical power during 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. Make all necessary wiring additions and adjustments for the installations.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Not specified in the source.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 airplanes.

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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