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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Tu-134A · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Tupolev Tu-134 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Airliner[source] |
| National origin | United States[source] | Soviet Union[source] |
| Manufacturer | Air Tractor[source] | Tupolev, KhAZ[source] |
| Status | Active[source] | In limited use |
37.1 m (121 ft 9 in)[source]
Tu-134A · fuselage diameter
Single source2.9 m (9 ft 6 in) fuselage diameter[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]
Tu-134A · 2 × Soloviev D-30-II turbofan engines thrust each
Single source2 × Soloviev D-30-II turbofan engines, 66.68 kN (14,990 lbf) thrust each[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.
| Manufactured | 1990–present[source] | 1966–1989[source] |
|---|
| First flight | 1990[source] | 29 July 1963[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 72–84 passengers / 8,200 kg (18,078 lb)[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root: PR-1-10S-9 (15.7%); tip: PR-1-10S-9 (12%)[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Designer | — | Tupolev[source] |
|---|
| Built by | — | Kharkiv State Aircraft Manufacturing Company[source] |
|---|
| Primary users | — | Aeroflot (historical) Soviet Air Force (historical) Russian Air Force Air Koryo[source] |
|---|
| Number built | — | 854 (852 + 2 prototypes)[source] |
|---|
| Introduction date | — | 9 September 1967[source] |
|---|
| Developed from | — | Tupolev Tu-124[source] |
|---|
| Fuel capacity | — | 13,200 L (3,500 US gal; 2,900 imp gal)[source] |
|---|
Maximum take-off; Tu-134A · Max takeoff weight
Single source