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FAA
Federal Aviation Administration Department of Transportation
Aviation Safety
AIRWORTHINESS DIRECTIVE
Generated by Aircraft-logs.com — March 22, 2026

AD 69-05-05 ACTIVE

Power Lever Travel
Key Information
AD Number 69-05-05 Status Active
Effective Date March 12, 1969 Issue Date Not specified
Docket Number Unknown Amendment 39-732
Product Type ["Aircraft"] Product Subtype ["Small Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Pilatus Aircraft Limited
Model(s) PC-6/B-H2 PC-6/B1-H2
Regulatory Text

69-05-05 PILATUS: Amdt. 39-732. Applies to Model PC-6/B-H2 and PC-6/B1-H2 airplanes.
Compliance required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished.
Check the travel of the knurled friction nut on the power control lever assembly to determine if it exceeds 3/4 of a turn. If travel exceeds 3/4 of a turn, install shim(s) of adequate thickness, or drill a new hole and insert a new cotter pin, in accordance with Pilatus Service Bulletin No. 85 dated July 1968 or later Swiss Federal Air Office-approved issue or an FAA- approved equivalent.
This amendment becomes effective March 12, 1969.

AD 69-05-05 — Power Lever Travel
Printed from Aircraft-logs.com — 03/22/2026