AD 63-20-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 190 | Airworthiness Directives; CESSNA Model 190 and 195 Series Airplanes |
| aircraft | Cessna Aircraft Company | 195 | Airworthiness Directives; CESSNA Model 190 and 195 Series Airplanes |
| aircraft | Cessna Aircraft Company | 195A | Airworthiness Directives; CESSNA Model 190 and 195 Series Airplanes |
| aircraft | Cessna Aircraft Company | 195B | Airworthiness Directives; CESSNA Model 190 and 195 Series Airplanes |
Unsafe Condition
Fatigue failure of the front wing spar fuselage carry through lower cap.
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Required Actions
Conduct visual and X-ray inspections for cracks in the lower cap of the front spar carry through member, inspect rear spar to fuselage attachment bolts and fittings for wear or damage, inspect steel plates for cracks, replace defective parts or make FAA-approved repairs, and accomplish the fuselage front spar modification with NAS 464P7-A64 bolts and reinforcement bars. Subsequent inspections must check for cracks in the lower spar cap and reinforcement bars.
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Compliance Time
Within 10 hours' time in service after the effective date of this AD
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Affected Aircraft
Cessna Model 190 and 195 Series Aircraft, all serial numbers
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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