AD 69-12-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Alexandria Aircraft, LLC | 14-19-3A | Airworthiness Directives; Bellanca Model 14-19-3A and 17-30 Airplanes |
| aircraft | Alexandria Aircraft, LLC | 17-30 | Airworthiness Directives; Bellanca Model 14-19-3A and 17-30 Airplanes |
Unsafe Condition
Failures of the stabilizer rear strut clevises
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Required Actions
Perform either a magnetic particle inspection of both P/N 193101-9 rear strut attach clevises within 25 hours' time-in-service after the effective date and at intervals not exceeding 25 hours' time-in-service, or replace both clevises with redesigned P/N 193130 within the same timeframe. If a crack is found during inspection, replace the clevises before further flight.
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Compliance Time
Within 25 hours' time-in-service after the effective date of this airworthiness directive
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Affected Aircraft
Bellanca Model 14-19-3A (Serial Numbers 4229 thru 4342) and 17-30 (Serial Numbers 30001 thru 30164) Airplanes
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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