AD 95-12-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lavia Argentina S.A. (Laviasa) | PA-25 | Airworthiness Directives; Piper Aircraft Corporation PA-25 Series Airplanes |
| aircraft | Lavia Argentina S.A. (Laviasa) | PA-25-235 | Airworthiness Directives; Piper Aircraft Corporation PA-25 Series Airplanes |
| aircraft | Lavia Argentina S.A. (Laviasa) | PA-25-260 | Airworthiness Directives; Piper Aircraft Corporation PA-25 Series Airplanes |
Unsafe Condition
Cracks or corrosion in the wing forward spar fuselage attachment assembly could lead to in-flight wing separation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect the wing forward spar fuselage attachment assembly using ultrasonic and dye penetrant procedures, replace or repair any cracked or corroded parts, and report inspection results to the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Effective July 7, 1995.
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Affected Aircraft
Piper Aircraft Corporation PA-25 series airplanes including models PA-25, PA-25-235, PA-25-260.
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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