Credit
Kirill Naumenko - Moscow City Spotters · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Empty; An-72 · Empty weight
Single sourceGross; An-72 · Gross weight
Single source19,050 kg (42,000 lb)[source]
34,500 kg (76,058 lb)[source]
Empty; Hawker 800 · basic
Single sourceMaximum take-off; Hawker 800 · * Maximum landing weight
Single sourceMaximum take-off; Hawker 800 · Max takeoff weight
Single source15,600 lb (7,076 kg) basic[source]
27,400 lb (12,428 kg) * Maximum landing weight: 23,350 lb (10,591 kg)[source]
Maximum; An-72 · Maximum speed
Single source700 km/h (435 mph, 378 kn)[source]
Cruise; Hawker 800 · economical cruise at 39,000–43,000 ft (11,887–13,106 m)
Single sourceMaximum; Hawker 800 · max level speed and max cruising speed at 29,000 ft (8,839 m) / M0.87
Single source456 kn (525 mph, 845 km/h) max level speed and max cruising speed at 29,000 ft (8,839 m) / M0.87[source]
400 kn (460 mph, 740 km/h) economical cruise at 39,000–43,000 ft (11,887–13,106 m)[source]
An-72 · 2 × Lotarev D-36 series 1A Turbofan thrust each
Single source2 × Lotarev D-36 series 1A Turbofan, 63.9 kN (14,330 lbf) thrust each[source]
Hawker 800 · 2 × Honeywell TFE731-5BR turbofan engines thrust each
Single source2 × Honeywell TFE731-5BR turbofan engines, 4,300 lbf (19 kN) thrust each[source]
Hawker 800 · 3,100 ft/min (
Single source3,100 ft/min (16 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Antonov An-72 | Hawker 800 |
|---|---|---|
| Type | Transport aircraft[source] | Mid-size business jet[source] |
| National origin | Soviet Union[source] | United Kingdom[source] |
| Manufacturer | Antonov[source] | British Aerospace (BAe) (1983–1994) Raytheon (1994–2007) Hawker Beechcraft (2007–2013)[source] |
| Status | In service[source] | In service[source] |
| Primary users | Russian Aerospace Forces Russian Navy Angolan Air Force Soviet Air Force (historical)[source] | Japan Air Self-Defense Force Brazilian Air Force Royal Saudi Air Force[source] |
| Number built | 133[source] | 650[source] |
| Manufactured | 1977–2002[source] | 1983–2013[source] |
| First flight | 31 August 1977 ( 1977-08-31 )[source] | 26 June 1983[source] |
| Developed into | Antonov An-71 Antonov An-74[source] | — |
| Capacity | up to 52 passengers or 10 tonnes of cargo[source] | 8 / 2,000 lb (907 kg) maximum payload[source] |
| Developed from | — | British Aerospace 125[source] |
| Fuel capacity | — | 1,248 imp gal (1,499 US gal; 5,674 L) total; 1,060 imp gal (1,273 US gal; 4,819 L) in wing integral tanks + 188 imp gal (226 US gal; 855 L) in rear under-fuselage tank[source] |
| Operating weight empty | — | 16,000 lb (7,257 kg)[source] |
| Maximum ramp weight | — | 27,520 lb (12,483 kg)[source] |
| Maximum zero-fuel weight | — | 18,000 lb (8,165 kg)[source] |
| Stall speed | — | 92 kn (106 mph, 170 km/h) in landing configuration at typical landing weight[source] |
| Wing loading | — | 73.26 lb/sq ft (357.7 kg/m 2 )[source] |
| Thrust/weight | — | 0.313[source] |
| Take-off balanced field length | — | 5,620 ft (1,713 m) at MTOW[source] |
| Landing distance from 50 ft (15 m) | — | 4,500 ft (1,372 m) at typical landing weight and 6 pax[source] |
| Reported operators |
| — |