AD Amdt-39-11069

final rule
Data completeness: 70%

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

AD Number
Amdt-39-11069
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-CE-73-AD
FR Citation
64 FR 12241

Applicability

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

Unsafe Condition

Improper use of the 'Alternate Flap System' could result in flap asymmetry, leading to reduced or loss of control of the airplane.

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

Required Actions

Remove the 'Alternate Flap System' from the airplane flight controls. Insert a temporary revision specifying this change in SECTION 2--LIMITATIONS of the PC-12 Pilot's Operating Handbook.

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

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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