AD 2000-23-01
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
Spar cap cracking in the forward, aft, and auxiliary wing spars is not an isolated condition and could continue to develop over the life of the affected airplanes, potentially resulting in 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 in accordance with Cessna Service Bulletin MEB99-3. Repair any cracks found in accordance with an FAA-approved repair scheme. Report the results of the inspection to the FAA. Repeat the inspection every 100 flight hours time-in-service (TIS).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 flight hours time-in-service (TIS) after the effective date.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.