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