AD Amdt-39-11184
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna | Aircraft Company Model 402C | Airworthiness Directives; Cessna Aircraft Company Model 402C Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Cessna Aircraft Company Model 402C Airplanes |
Unsafe Condition
Fatigue cracking of the forward main spar that initiates at the edge of the front spar forward lower spar cap, which could lead to reduced or loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the forward, aft, and auxiliary wing spars for cracks. Repair any cracks found. Report the results of the inspection to the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Aircraft Company Model 402C airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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