AD 92-18-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-46-310P | Airworthiness Directives; BENDIX/KING KAP 150/KFC 150 Flight Control Systems installed on Piper Models PA-46-310P and PA-46-350P Airplanes |
| aircraft | Piper Aircraft Inc. | PA-46-350P | Airworthiness Directives; BENDIX/KING KAP 150/KFC 150 Flight Control Systems installed on Piper Models PA-46-310P and PA-46-350P Airplanes |
Unsafe Condition
Moisture entering the electronic circuit board through the pitch servo could possibly lead to undesired movement of the elevator.
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Required Actions
Install a pitch servo cover kit (part number 050-03007-0000) following Bendix/King Installation Bulletin No. 312. Special flight permits may be issued under FAR 21.197 and 21.199 to operate to a location where AD requirements can be accomplished.
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Compliance Time
within the next 90 calendar days after the effective date of this AD, unless already accomplished
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Affected Aircraft
BENDIX/KING KAP 150/KFC 150 Flight Control Systems installed on Piper Models PA-46-310P and PA-46-350P airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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