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]
VC-25A · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Boeing VC-25 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | 26: flight crew (pilot, co-pilot, flight engineer, navigator), cabin crew, communications, maintenance, and security[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Presidential transport[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] |
231 ft 10 in (70.66 m)[source]
Cruise; AT-802 · at 8,000 ft (2,440 m)
Single source221 mph (356 km/h, 192 kn) at 8,000 ft (2,440 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]
VC-25A · 4 × General Electric CF6-80C2B1 turbofan engines thrust each
Single source4 × General Electric CF6-80C2B1 turbofan engines, 56,700 lbf (252 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]
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] | 1986–1990; 2018–present[source] |
|---|
| First flight | 1990[source] | 16 May 1987[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | Boeing VC-25B Bridge[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 76 passengers[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 | — | United States Air Force[source] |
|---|
| Number built | — | 2 (VC-25A)[source] |
|---|
| Introduction date | — | 23 August 1990[source] |
|---|
| Developed from | — | VC-25A: Boeing 747-200B VC-25B: Boeing 747-8I[source] |
|---|