AD 2024-10-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper | Aircraft | Airworthiness Directives; Piper Aircraft, Inc. Airplanes |
Unsafe Condition
A double-drilled bolt hole of the rear wing spar attachment fitting reduces its strength below its limit load, and, if not addressed, could result in separation of the wing and loss of control of the airplane.
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Required Actions
Inspect the rear wing spar attachment fitting and, if discrepancies are found, inspect the forward wing spar attachment fitting, accomplish corrective actions as required, and report to the FAA when corrective actions are required.
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Compliance Time
Before further flight
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Affected Aircraft
Piper Model PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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