Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Il-62M · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Ilyushin Il-62 |
|---|---|---|
| Crew | One or Two (AT-802A – single-seat)[source] | 5; 3 to 5 (a captain, a first officer, and a flight engineer, plus optionally a navigator and a radio officer on long overwater and/or VIP services to operator specification) plus a four to eight-person cabin crew to operator specifications[source] |
| Type | Agricultural / Fire-fighting aircraft[source] | Narrow-body jet airliner[source] |
| National origin | United States[source] | Soviet Union[source] |
| Manufacturer | Air Tractor[source] |
53.12 m (174 ft 3 in)[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]
Il-62M · 4 × Soloviev D-30KU turbofan engines thrust each
Single source4 × Soloviev D-30KU turbofan engines, 107.9 kN (24,300 lbf) thrust each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Ilyushin, Kazan Aircraft Production Association[source] |
| Status | Active[source] | In limited service[source] |
|---|
| Manufactured | 1990–present[source] | 1963–1995[source] |
|---|
| First flight | 1990[source] | 3 January 1963[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 168–186 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] | — |
|---|
| Designer | — | Ilyushin[source] |
|---|
| Built by | — | KAPO[source] |
|---|
| Primary users | — | Russian Air Force Air Koryo Rada Airlines Aeroflot (historical)[source] |
|---|
| Number built | — | 292 (5 prototypes; 94 Il-62; 193 Il-62M)[source] |
|---|
| Introduction date | — | Il-62 – 15 September 1967 Il-62M – 9 March 1974[source] |
|---|
| Fuel capacity | — | 105,300 L (27,800 US gal; 23,200 imp gal) / 84,240 kg (185,720 lb)[source] |
|---|