AD 81-23-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-38-112 | Airworthiness Directives; Piper Model PA-38-112 Airplanes |
Unsafe Condition
Nose-gear failure associated with weakening of the engine-mount assembly.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and replace, if required, the engine mount within the next 50 hours in service after the effective date of this AD. Repeat inspections at intervals not to exceed 50 hours until 1000 hours in service from modification or until replacement with Piper Part Number 77651-02. Replace engine mount with Piper Part No. 77651-02 if applicable.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 50 hours in service after the effective date of this AD
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Affected Aircraft
Piper Model PA-38-112 Serial Nos. 38-78A0001 thru 38-78A0678 certificated in all categories except aircraft incorporating engine mount assembly Piper Part Number 77651-02.
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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