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]
Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Boeing C-40 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | Four, five or six: Pilot, co-pilot, crew chief and loadmaster, plus one 'second loadmaster' when carrying passengers or two when carrying over 100 passengers[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Military transport aircraft[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] |
110 ft 4 in (33.63 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]
2 × CFM International CFM56-7B turbofan engines thrust each
Single source2 × CFM International CFM56-7B turbofan engines, 27,300 lbf (121 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]
Payload
Single source40,000 lb (18,144 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Boeing[source] |
| Status | Active[source] | In service[source] |
|---|
| Manufactured | 1990–present[source] | 2001–2019[source] |
|---|
| First flight | 1990[source] | April 2000[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | C-40A passenger configuration: 121 passengers C-40A cargo configuration: 8 pallets C-40A combination configuration: 3 pallets, 70 passengers C-40B: 26 to 32 passengers C-40C: 42 to 111 passengers Payload: 40,000 lb (18,144 kg)[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root: BAC 449/450/451; tip: BAC 442 mod[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | United States Navy United States Air Force United States Marine Corps[source] |
|---|
| Number built | — | 28[source] |
|---|
| Introduction date | — | 21 April 2001[source] |
|---|
| Developed from | — | Boeing 737 Next Generation[source] |
|---|
| Fuel capacity | — | 6,875 US gal (26,020 L; 5,725 imp gal)[source] |
|---|
| Thrust/weight | — | 0.407[source] |
|---|