FAA · Type Certificate Data Sheet
TCDS 2A2
Camair Aircraft Corporation
Models covered (1)
Special Airworthiness Information Bulletins (1)
Advisory bulletins on these airframes. Not mandatory like ADs — but operators tracking AD compliance often miss the SAIB on the same component.
Special Conditions + ELOS findings
Certification-time deviations: SCs add requirements where the design is novel; ELOS allows alternative compliance. Most modern types have both.
- 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
Engineering specs aggregated from the FAA Aircraft Registry — what every actually-flying tail under this TCDS reports. Median + 10th–90th-percentile range across the active fleet.
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
The TCDS PDF on drs.faa.gov is the authoritative document for design-as-certified weight limits, performance, equipment, AD compliance times, and operating limitations. Open on drs.faa.gov ↗ DRS frequently breaks — when it does, the fleet view above and the cross-links below are usually what you actually need.