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
An-72 · Length
Single source28.07 m (92 ft 1 in)[source]
Length
Single sourceConfiguration
| Specification | Antonov An-72 | Gulfstream G550 |
|---|---|---|
| Type | Transport aircraft[source] | Business jet[source] |
| National origin | Soviet Union[source] | United States[source] |
| Manufacturer | Antonov[source] | Gulfstream Aerospace[source] |
| Status | In service[source] | In service[source] |
96 ft 5 in (29.39 m)[source]
Maximum; An-72 · Maximum speed
Single source700 km/h (435 mph, 378 kn)[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]
2 × Rolls-Royce BR710 C4-11 turbofan engines thrust each
Single source2 × Rolls-Royce BR710 C4-11 turbofan engines, 15,385 lbf (68.44 kN) thrust each[source]
An-72 · Wing area
Single source98.62 m 2 (1,062 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Russian Aerospace Forces Russian Navy Angolan Air Force Soviet Air Force (historical)[source] | United States Air Force United States Navy Israeli Air Force[source] |
|---|
| Number built | 133[source] | >600[source] |
|---|
| Manufactured | 1977–2002[source] | 2003–2021[source] |
|---|
| First flight | 31 August 1977 ( 1977-08-31 )[source] | 31 August 2001[source] |
|---|
| Developed into | Antonov An-71 Antonov An-74[source] | — |
|---|
| Capacity | up to 52 passengers or 10 tonnes of cargo[source] | 14–19 passengers / 6,200 lb (2,812 kg) payload[source] |
|---|
| Introduction date | — | 2004[source] |
|---|
| Developed from | — | Gulfstream V[source] |
|---|
| Variant | — | L3Harris EA-37B Compass Call[source] |
|---|
| Successors | — | Gulfstream G600[source] |
|---|
| Fuel capacity | — | 41,300 lb (18,733 kg)[source] |
|---|
| Cabin dimensions: height × width × length | — | 6 ft 2 in × 7 ft 4 in × 43 ft 11 in (1.88 m × 2.24 m × 13.39 m); total length including baggage hold: 50 ft 1 in (15.27 m)[source] |
|---|
| Cabin volume | — | 1,669 cu ft (47.26 m 3 ); usable baggage compartment volume: 170 cu ft (4.81 m 3 )[source] |
|---|
| Cabin altitude | — | 6,000 ft (1,829 m)[source] |
|---|
| Airfoil | — | root: NACA 0012; tip: NACA 0012[source] |
|---|
| Maximum landing weight | — | 75,300 lb (34,156 kg)[source] |
|---|
| High Speed Cruise | — | M0.85 at 41,000 ft (12,000 m)[source] |
|---|
| Long Range Cruise | — | M0.80 at 41,000 ft (12,000 m)[source] |
|---|
| Maximum Mach Operating (MMO) | — | M0.885 at 41,000 ft (12,000 m)[source] |
|---|
| Take-off run | — | 5,910 ft (1,800 m)[source] |
|---|
| Landing run | — | 2,770 ft (840 m)[source] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; Max takeoff weight