AD 81-23-03 R2
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | P210N | Airworthiness Directives; Cessna Model P210N Airplanes |
Unsafe Condition
Cracks in the engine exhaust system components attached to and between the two forward most (Nr. 5 and Nr. 6) cylinders could result in exhaust leaks, leading to potential fire hazards or engine failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the entire engine exhaust system for cracks and bulges in exhaust stacks, manifold, turbocharger, and wastegate assemblies per Cessna SIL SE82-3. Replace any cracked or bulged components with serviceable parts. Initial inspection must be done before further flight if the airplane has 25 or more hours time-in-service. Subsequent inspections at 50-hour intervals, with a 25-hour reinspection if components were replaced or repaired by welding.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to further flight for airplanes with 25 hours or more time-in-service unless previously accomplished. Subsequent inspections within the next 10 hours time-in-service after November 15, 1982, and every 50 hours thereafter, except for reinspection within 25 hours if components were replaced or repaired.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Model P210N (Serial Numbers P21000001 through P21000811) airplanes certificated in any category with 25 or more total hours time-in-service.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.