AD 92-15-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-36-300 | Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-36-300 and PA-36-375 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-36-375 | Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-36-300 and PA-36-375 Airplanes |
Unsafe Condition
Separation of the engine from the airplane because of cracks at the engine mount attach points.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the welds and adjacent areas at each engine mount attach point for cracks within 100 hours time-in-service after the effective date. If cracks are found, install gusset attachments prior to further flight. If no cracks, reinspect at intervals not exceeding 100 hours TIS.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 100 hours time-in-service after the effective date of this AD
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Affected Aircraft
Piper Aircraft Corporation Model PA-36-300 (serial numbers 36-7760001 through 36-8160023) and Model PA-36-375 (serial numbers 36-7802001 through 36-8302025)
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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