Camair Twin Navion

Airplanes

Length

8.5344 m

Flat Wing Span

10.3632 m

Height

3.048 m

Flat Wing Area

17.122 m²

Max Seating

Cruise Speed

308.994 km/h

Max Ceiling

6400.8 m

Number of Engines

Aircraft Engine

First Flight

1953-01-01

Number Built

Total Fuel Capacity

412.6099

Maximum Range

1448.41 km

Pictures

No pictures yet for this family.

Aircraft	Total Fuel Capacity	Maximum Range (km)
Camair Twin Navion	412.6099	1448.41

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Cessna A-37 Dragonfly	General Electric J85	8.5344	10.668		Compare
Italair Pegaso		8.2	10.34	5	Compare
Temco D-16	Lycoming O-320	8.28	10.16		Compare
Gulfstream American GA-7 Cougar	Lycoming O-320	8.5344	10.9728		Compare
Atlas H-10	Continental O-300	8.64	10.9		Compare
Boulton Paul P.92	De Havilland Gipsy Major	8.2296	10.0584		Compare

All data (24 fields)

Name: Camair Twin Navion
Manufacturer: Camair Aircraft Corp
Description: The Camair Twin Navion was a civil utility aircraft produced in the United States in the 1950s by converting single-engine Ryan Navions to twin-engine power.
ICAO Code: TNAV
First Flight: 1953-01-01
Designer: Camair Aircraft Corp
Type: Utility aircraft
Length (m): 8.5344
Height (m): 3.048
Cockpit Crew: 2
Max Seating: 2
Cruise Speed (km/h): 308.994
Min Speed (km/h): 99.7793
Max Ceiling (m): 6400.8
Rate of Climb (m/s): 8.89
Capacity Description: 2 passengers
Number Built: 33
Powerplant Description: 2 × Continental O-470-3 air-cooled flat-six engines, 179 kW (240 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Camair_Twin_Navion
Flat Wing Span (m): 10.3632
Flat Wing Area (m²): 17.122
Wake Category: L
Aircraft Engine: Continental O-470
Number of Engines: 2