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T-32 Condor II
The Curtiss T-32 Condor II was a 1930s American biplane airliner and bomber aircraft built by the Curtiss Aeroplane and Motor Company. It was used by the United States Army Air Corps as an executive transport.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Curtiss-Wright
- Category
- Airliners
- First flight
- 1933-01-30
- Length
- 586 m
- Wingspan
- 984 m
Specifications
- Cruise speed
- 126 kt
- Max speed
- 150 kt
- Range
- 500 nm
- Service ceiling
- 15,500 ft
- Rate of climb
- 850 ft/min
- Max takeoff weight
- 16,800 lb
- Empty weight
- 11,235 lb
- Fuel capacity
- 300 US gal
- Powerplant
- 2 × Wright GR-1820-F11 Cyclone
- Engines
- 2
- Seats
- 17
- Length
- 48.8 ft
- Wingspan
- 82 ft
- Height
- 16.8 ft
- Number built
- 45
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.