Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Phenom 100EV · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Embraer Phenom 100 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | 1 or 2 pilots[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Very light business jet[source] |
| National origin | United States[source] | Brazil[source] |
| Manufacturer | Air Tractor[source] | Embraer |
12.82 m (42 ft 1 in)[source]
AT-802 · Range
Single source800 mi (1,300 km, 700 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]
AT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (
Single source1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)[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]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | In production, in service[source] |
|---|
| Manufactured | 1990–present[source] | December 2008–present[source] |
|---|
| First flight | 1990[source] | 26 July 2007[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | Embraer Phenom 300[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 4 or 5 passengers (standard configurations); 7 passengers maximum (with passenger in cockpit, optional side-facing seat, and optional belted lavatory)[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | — |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Number built | — | 439 (H1 2026)[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] |
|---|