AD 65-15-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lavia Argentina S.A. (Laviasa) | PA-25 | Airworthiness Directives; Piper Models PA-25 and PA-25-235 Aircraft |
| aircraft | Lavia Argentina S.A. (Laviasa) | PA-25-235 | Airworthiness Directives; Piper Models PA-25 and PA-25-235 Aircraft |
Unsafe Condition
Worn clevis bolts, AN-24-14, on the elevator cable link assembly, P/N 81352-15, could result in loss of the elevator control system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the clevis bolt AN-24-14 for wear where it contacts the link assembly P/N 81352-15. Replace worn clevis bolts with new AN-24-14 bolts. Replace link assemblies P/N 81352-15 and spacer P/N 61402-5 with P/N 64748 and bushing P/N 64749 per Piper Service Letter 455 or approved equivalent.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before the accumulation of 260 hours' time in service for aircraft with less than 250 hours' time in service on the effective date, or within the next 10 hours' time in service for those with 250 or more hours. Thereafter, inspections at intervals not exceeding 250 hours' time in service until modified per (d).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Piper Models PA-25 (Serial Numbers 25-1 through 25-731) and PA-25-235 (Serial Numbers 25-2000 through 25-3565).
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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