AD 92-13-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-46-310P | Airworthiness Directives; PIPER AIRCRAFT CORPORATION Models PA-46-310P and PA-46-350P Airplanes |
| aircraft | Piper Aircraft Inc. | PA-46-350P | Airworthiness Directives; PIPER AIRCRAFT CORPORATION Models PA-46-310P and PA-46-350P Airplanes |
Unsafe Condition
Sudden pitch change related to a jammed trim tab, which could result in loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect the elevator trim cable guide tube for severance. If severance is found, splice the tube and install an external sleeve per Piper Part Number 766-272. Use special flight permits under FAR 21.197/21.199 to operate to a location where AD requirements can be met.
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Compliance Time
within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished
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Affected Aircraft
Models PA-46-310P (serials 46-8408001 through 46-8608067 and 4608001 through 4608140) and PA-46-350P (serials 4622001 through 4622117)
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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