Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
E-767 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Boeing E-767 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | Flight: 2; Mission: 8-10[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Airborne Warning and Control System (AWACS)[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Boeing Integrated Defense Systems |
159 ft 2 in (48.5 m)[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]
E-767 · 2 × General Electric CF6-80C2 turbofan thrust each
Single source2 × General Electric CF6-80C2 turbofan , 61,500 lbf (274 kN) thrust each[source]
AT-802 · Wing area
Single source401.0 sq ft (37.25 m 2 )[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
E-767 · at 300-nautical mile radius (no aerial refueling capability)
Single sourceE-767 · on station at 1,000 nautical-mile radius
Single source9.25 hours on station at 1,000 nautical-mile radius; 13 hours at 300-nautical mile radius (no aerial refueling capability).[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | In service[source] |
|---|
| Manufactured | 1990–present[source] | — |
|---|
| First flight | 1990[source] | 4 October 1994 (without rotodome) 9 August 1996 (with rotodome )[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[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] | — |
|---|
| Primary user | — | Japan Air Self-Defense Force[source] |
|---|
| Number built | — |
|---|
| Introduction date | — | 10 May 2000[source] |
|---|
| Developed from | — | Boeing 767[source] |
|---|
Maximum take-off; E-767 · Max takeoff weight
Single source