AD 85-03-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 206 | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 207 | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210-5 (205) | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210B | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210C | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210D | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210E | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210F | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210G | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210H | Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes |
Unsafe Condition
Failure of engine throttle and mixture control cables due to sleeve and bushing not secured by a drive screw, leading to loss of engine power control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect the ends of the engine throttle and mixture control cables to determine if the sleeve and bushing are secured by a drive screw. If present, inspect, modify, and/or replace the controls per Cessna Service Letter SE69-16. Allow ferry flight under FAR 21.197 if controls function properly and reduced mixture selection is avoided.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 100 hours time-in-service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Models 205 (S/Ns 205-0001 thru 205-0479); 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D (S/Ns 206-0001 thru U206-1444); P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D (S/Ns P206-0001 thru P206-0603); 207 and T207 (S/Ns 20700001 thru 20700148); 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J (S/Ns 21057841 thru 21059199); T210F, T210G, T210H, T210J (S/Ns T210-O001 thru T210-0454)
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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