AD 83-14-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Vulcanair S.p.A. | P 68 | Airworthiness Directives; Partenavia Models P68 and P68B Series Airplanes |
| aircraft | Vulcanair S.p.A. | P 68B | Airworthiness Directives; Partenavia Models P68 and P68B Series Airplanes |
Unsafe Condition
Failure of the fin rear spar
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install fin spar reinforcement in accordance with Partenavia Costruzioni Aeronautiche S.p.A. Service Bulletin No. 34, Rev. 1, dated February 15, 1978, and Drawing No. R.0007, dated December 23, 1977. Aircraft may be flown under Federal Aviation Regulation 21.197 to a location where this AD can be accomplished. Equivalent methods of compliance must be approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 100 hours after the effective date of this Airworthiness Directive (AD), unless already accomplished
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Affected Aircraft
Vulcanair S.p.A. Models P68 and P68B (all serial numbers up to 128, excluding SNs 40, 112, 125, 126, and 127)
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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