AD 91-22-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 210 | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210-5 (205) | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210-5A (205A) | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210A | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210B | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210C | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210D | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210E | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210F | Airworthiness Directives; CESSNA Model 210 Airplanes |
| aircraft | Cessna Aircraft Company | 210G | Airworthiness Directives; CESSNA Model 210 Airplanes |
Unsafe Condition
Fuel leakage caused by damaged fuel lines, which could result in an in-flight fire.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect electrical wires in the nose gear tunnel area and the fuel line to the engine-driven fuel pump for cracks or chafing. If any cracked or chafed components are found, replace them with new parts and ensure a .25 inches clearance between the wire bundle and fuel line. If no damage is found, bundle and route or clamp the wires to maintain the .25 inches clearance.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 50 hours time-in-service
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Model 210 airplanes with serial numbers 21059062 through 21064535, T210-0393 through T210-0454, and P21000001 through P21000760
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
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