AD 72-22-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-24 | Airworthiness Directives; Piper Models PA-24, PA-24-250, and PA-24-260 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-24-250 | Airworthiness Directives; Piper Models PA-24, PA-24-250, and PA-24-260 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-24-260 | Airworthiness Directives; Piper Models PA-24, PA-24-250, and PA-24-260 Airplanes |
Unsafe Condition
Possible adverse airplane vibration effects due to exceeding airspeed limitations.
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Required Actions
Attach an operating limitation placard near the airspeed indicator within 10 flight hours after the effective date. Within three months, alter the airspeed indicator or rudder per FAA-approved methods. PA-24-250/260 may use higher Vne with stabilator alteration per Piper Service Kit 760747.
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Compliance Time
Within the next 10 hours in service after the effective date and within three (3) months after the effective date.
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Affected Aircraft
Piper Models PA-24, PA-24-250, and PA-24-260 airplanes certificated in all categories.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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