AD 75-10-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-32-260 | Airworthiness Directives; Piper Model PA-32-260 and PA-32-300 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-32-300 | Airworthiness Directives; Piper Model PA-32-260 and PA-32-300 Airplanes |
Unsafe Condition
Delamination of the forward baggage door along the hinge, leading edge, and inner stiffening sections due to cracks or delamination of the fiberglass.
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Required Actions
Examine the inside and outside of the forward baggage door along the hinge, leading edge, and inner stiffening sections for cracks or delamination. If found, install Piper Kit #760-972V or an equivalent approved by the FAA before further flight. The examination may be performed by the pilot.
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Compliance Time
Before further flight after the effective date of this AD, unless already accomplished within the last ten hours time in service, and thereafter at intervals not to exceed ten hours time in service from the last examination.
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Affected Aircraft
Piper Model PA-32-260 (serial numbers 32-01 through 32-7500039) and PA-32-300 (serial numbers 32-40001 through 32-7540147) 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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