TCDS 2A2
Current · Aircraft · Small Airplane · Rev 6 (06/01/1969) · FAA TCDS database
Camair Aircraft Corporation drs.faa.gov ↗
The TCDS PDF on drs.faa.gov is authoritative for design-as-certified weight limits, performance, equipment and operating limitations.
Models covered (1)
Airworthiness directives (3) · mandatory: an aircraft out of compliance is not airworthy
- 03-15991 Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) Series and HA-A2V20-1B Series Propellers with Aluminum Blades 2003-06-26
- 02-33074 Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) Series and HA-A2V20-1B Series Propellers with Aluminum Blades 2003-01-02
- 97-22677 Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)(X,V)( )-( ) Series and HA-A2V20-1B Series Propellers With Aluminum Blades 1997-08-27
SAIBs (1)
Special conditions + ELOS findings
- ELOS AT09299CH-R-P-1 Equivalent Level of Safety (ELOS) Finding for Crash Resistance Fuel System Components
Former holders
- Universal\Ryan\J. Thompson Enterprise\Camair\Camair Aircraft Corporation -- Fred Garcia
- Universal\Ryan\J. Thompson Enterprise
Fleet view · 8 registered tails · FAA registry, median and p10–p90
- Seats
- 4
- n=8
- Horsepower
- 230
- 230–260
- Cruise (kts)
- 135
- 135–135
- Year of mfr
- 1955
- 1946–1956
Engines on the type, by tail count
- CONT MOTOR O-470 SERIES 7
- CONT MOTOR I0-470 SERIES 1
- NTSB events
- 3
- across all model variants
- Applicable ADs
- 3
- FAA airworthiness directives
- Per-tail rate
- 0.38 events / tail · 0.38 ADs / tail