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]
E-6B · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Boeing E-6 Mercury |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Airborne command and control[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Boeing[source] |
| Status | Active[source] | In service[source] |
150 ft 4 in (45.82 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]
E-6B · Combat range
Single source6,350 nmi (7,310 mi, 11,760 km)[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]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
E-6B · maximum with multiple refuelings
Single sourceE-6B · on station at 1,000 nmi (1,200 mi; 1,900 km) unrefueled
Single sourceE-6B · with one refueling
Single sourceon station at 1,000 nmi (1,200 mi; 1,900 km) 10 hours 30 minutes unrefueled 28 hours 54 minutes with one refueling 72 hours maximum with multiple refuelings[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured |
|---|
1990–present[source] |
| — |
| First flight | 1990[source] | 19 February 1987[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 | — | United States Navy[source] |
|---|
| Number built | — | 16[source] |
|---|
| Introduction date | — | August 1989[source] |
|---|
| Developed from | — | Boeing 707[source] |
|---|
| Powerplant | — | 4 × CFM International CFM56-2A-2 turbofan engines[source] |
|---|
| Wing loading | — | 112.13 lb/sq ft (547.5 kg/m 2 )[source] |
|---|
| Thrust/weight | — | 0.281[source] |
|---|
| Critical field length | — | 6,700 ft (2,042 m)[source] |
|---|
| Max effort take-off run | — | 5,400 ft (1,646 m)[source] |
|---|
| Landing run at max landing weight | — | 2,600 ft (792 m)[source] |
|---|
| Country of origin | — | Vereinigte Staaten[source]Country of design · Entwurfsland |
|---|