Length
21.58 m
Flat Wing Span
22.81 m
Height
7.21 m
Flat Wing Area
42.09 m²
Max Seating
36
Cruise Speed
333.3597 km/h
Max Speed
404 km/h
Max Ceiling
6096 m
Number of Engines
2
Aircraft Engine
First Flight
1981-06-01
Entry Into service
1982-11-01
Number Built
165
Maximum Take-Off Weight
12.292 t (paragliders: kg)
Total Fuel Capacity
2182
Maximum Range
1594.572 km

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Short 360 12.292 2182 1594.572

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
AIDC XC-2 Lycoming T53 20.1 24.9 38 Compare
Mitsubishi G4M 19.97 24.89 Compare
Saab 340 General Electric T700 19.73 21.44 34 Compare
Dornier 328 21.28 20.98 Compare
Blohm & Voss BV 144 BMW 801 21.8 27 Compare
Saab 340 AEW&C General Electric T700 20.57 21.44 Compare
All data (28 fields)
Name
Short 360
Manufacturer
Short Brothers
Description
The Short 360 (also SD3-60; also Shorts 360) is a commuter aircraft that was built by UK manufacturer Short Brothers during the 1980s.
ICAO Code
SH36
First Flight
1981-06-01
Entry Into service
1982-11-01
Production End
1991-01-01
Designer
Short Brothers
Type
Transport aircraft
Length (m)
21.58
Height (m)
7.21
Max Seating
36
Max Speed (km/h)
404
Cruise Speed (km/h)
333.3597
Max Ceiling (m)
6096
Rate of Climb (m/s)
4.8362
Capacity Description
36 passengers
National Origin
United Kingdom
Number Built
165
Powerplant Description
2 × Pratt & Whitney Canada PT6A-65AR turboprop, 1062 kW (1424 hp) each
Primary Users
Air Cargo Carriers, TransAir , Skyway Enterprises , Air Flamenco
Status
In limited service
Wikipedia Article (URL)
en.wikipedia.org/wiki/Short_360
Flat Wing Span (m)
22.81
Flat Wing Area (m²)
42.09
Wake Category
M
Aircraft Engine
Pratt & Whitney Canada PT6
Number of Engines
2