Cessna AT-17 Bobcat

Airplanes

Length

9.98 m

Flat Wing Span

12.78 m

Height

3.02 m

Flat Wing Area

27.4064 m²

Cruise Speed

281.6352 km/h

Max Speed

313.8221 km/h

Max Ceiling

6705.6 m

Number of Engines

Aircraft Engine

First Flight

1939-03-26

Number Built

5422

Maximum Take-Off Weight

2.7497 t (paragliders: kg)

Maximum Range

1207.008 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Cessna AT-17 Bobcat	2.7497	1207.008

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Helio Twin Courier	Lycoming O-540	9.7536	12.4968	5	Compare
Eclipse 500	Pratt & Whitney Canada PW600	10.2108	11.5519	6	Compare
Eclipse 550		10.2108	11.5519	5	Compare
Piper PA-31 Navajo	Lycoming O-540	9.7536	12.192	5	Compare
Cessna 340	Continental IO-520	10.3632	11.5824		Compare
Cessna 411	Continental IO-520	10.0584	11.8872		Compare

All data (25 fields)

Name: Cessna AT-17 Bobcat
Manufacturer: Cessna Aircraft Company
Description: The Cessna AT-17 Bobcat or Cessna Crane is a twin-engine advanced trainer aircraft designed and made in the United States, and used during World War II to bridge the gap between single-engine trainers and larger multi-engine combat aircraft.
ICAO Code: T50
First Flight: 1939-03-26
Production End: 1944-01-01
Designer: Cessna Aircraft Company
Type: Trainer, five-seat light transport and utility aircraft
Length (m): 9.98
Height (m): 3.02
Max Speed (km/h): 313.8221
Cruise Speed (km/h): 281.6352
Min Speed (km/h): 101.3887
Max Ceiling (m): 6705.6
Rate of Climb (m/s): 5.842
Number Built: 5422
Powerplant Description: 2 × Jacobs R-755-9 seven-cylinder, air-cooled, radial piston engine, 183 kW (245 hp) each
Primary Users: United States Army Air Forces, Royal Canadian Air Force, United States Navy
Status: Retired, some examples in private use
Wikipedia Article (URL): en.wikipedia.org/wiki/Cessna_AT-17_Bobcat
Flat Wing Span (m): 12.78
Flat Wing Area (m²): 27.4064
Wake Category: L
Aircraft Engine: Jacobs R-755
Number of Engines: 2