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At a glance
Measured figures
An-72 · Length
Single source28.07 m (92 ft 1 in)[source]
Phenom 100EV · Length
Single sourceConfiguration
| Specification | Antonov An-72 | Embraer Phenom 100 |
|---|---|---|
| Crew | five[source] | 1 or 2 pilots[source] |
| Type | Transport aircraft[source] | Very light business jet[source] |
| National origin | Soviet Union[source] | Brazil[source] |
| Manufacturer | Antonov[source] | Embraer[source] |
12.82 m (42 ft 1 in)[source]
An-72 · Range
Single source4,325 km (2,688 mi, 2,336 nmi)[source]
Phenom 100EV · alternate
Single sourcePhenom 100EV · LRC, four 91 kg (200 lb) occupants, NBAA IFR reserves with
Single source2,182 km (1,356 mi, 1,178 nmi) (LRC, four 91 kg (200 lb) occupants, NBAA IFR reserves with 185 km (115 mi; 100 nmi) alternate)[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]
Phenom 100EV · 2 × Pratt & Whitney Canada PW617F1-E turbofan engines thrust each at ISA + 8°C
Single source2 × Pratt & Whitney Canada PW617F1-E turbofan engines, 7.7 kN (1,730 lbf) thrust each at ISA + 8°C[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In production, in service[source] |
|---|
| Primary users | Russian Aerospace Forces Russian Navy Angolan Air Force Soviet Air Force (historical)[source] | — |
|---|
| Number built | 133[source] | 439 (H1 2026)[source] |
|---|
| Manufactured | 1977–2002[source] | December 2008–present[source] |
|---|
| First flight | 31 August 1977 ( 1977-08-31 )[source] | 26 July 2007[source] |
|---|
| Developed into | Antonov An-71 Antonov An-74[source] | — |
|---|
| Capacity | up to 52 passengers or 10 tonnes of cargo[source] | 4 or 5 passengers (standard configurations); 7 passengers maximum (with passenger in cockpit, optional side-facing seat, and optional belted lavatory)[source] |
|---|
| Variant | — | Embraer Phenom 300[source] |
|---|
| Fuel capacity | — | 1,272 kg (2,804 lb)[source] |
|---|
| Cabin height | — | 1.5 m (4 ft 11 in)[source] |
|---|
| Cabin length | — | 3.35 m (11 ft)[source] |
|---|
| Minimum control speed | — | 180 km/h (110 mph, 97 kn)[source] |
|---|
| Cabin altitude | — | 2,438 m (8,000 ft) at 12,497 m (41,000 ft)[source] |
|---|
| Take-off run | — | 975 m (3,199 ft) (MTOW, SL, ISA)[source] |
|---|
| Landing run | — | 741 m (2,431 ft) (SL, ISA, four 91 kg (200 lb) occupants, NBAA IFR reserves with 185 km (115 mi; 100 nmi) alternate)[source] |
|---|
| Hourly fuel burn | — | (1,111 km (690 mi; 600 nmi) trip, four 91 kg (200 lb) occupants, NBAA IFR Reserves. SL Takeoff, ISA) 1st hour – 414 L/h (109 gal/h; 91 imp gal/h) (take-off and climb to cruise) 2nd hour – 292 L/h (77 gal/h; 64 imp gal/h) (cruise)[source] |
|---|
| Reported operators |
| — |
|---|