Attribute | Short 360 × | Yakovlev Yak-40 × |
---|---|---|
General | ||
Manufacturer | Short Brothers | Yakovlev |
Model | Short 360 | Yakovlev Yak-40 |
Country | United Kingdom | Russia |
Manufactured from (year) | 1980 | 1967 |
Manufactured to (year) | 1991 | 1981 |
Type | Passenger Turbo Props | Light Passenger Jets |
Icao | SH36 | YK40 |
Performance | ||
Engine | 2x Pratt & Whitney Canada PT6A-65AR | 3x Ivchenko AI-25 |
Power, hp (hp) | 1,424 | 3,300 |
Max cruise speed (km/h) | 404 | 556 |
Approach speed (km/h) | 185 | 222 |
Travel range (km) | 1,056 | 1,796 |
Service ceiling (m) | 6,096 | 7,925 |
Rate of climb (m/sec) | 4.84 | 8 |
Take off distance (m) | 1,300 | 1,000 |
Landing distance (m) | 1,100 | 640 |
Weights | ||
Max take off weight (kg) | 12,300 | 16,000 |
Max landing weight (kg) | 12,020 | 15,500 |
1↓Max payload (kg) | 3,500 | 2,700 |
Fuel tank capacity (l) | 2,180 | 3,899 |
Dimensions | ||
Seats | 39 | 32 |
Cabin height (m) | 1.88 | 1.85 |
Cabin width (m) | 1.85 | 2.15 |
Cabin length (m) | 8.4 | 7.7 |
Exterior length (m) | 21.6 | 20.36 |
Tail height (m) | 7.27 | 6.5 |
Fuselage diameter (m) | 2.2 | 2.25 |
Wing span (m) | 22.8 | 25 |
Wing tips | No Winglets | No Winglets |