Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
340B · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Saab 340 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Turboprop regional airliner[source] |
| National origin | United States[source] | Sweden United States[source] |
| Manufacturer | Air Tractor[source] | Saab AB Fairchild Aircraft[source] |
| Status | Active[source] | In service |
19.73 m (64 ft 9 in)[source]
Empty; AT-802 · Empty weight
Single sourceMaximum take-off; AT-802 · Max takeoff weight
Single source6,505 lb (2,951 kg)[source]
16,000 lb (7,257 kg)[source]
Empty; 340B · average operational empty weight
Single sourceMaximum take-off; 340B · for 340B models by SAAB Service Bulletin (SB) 340-51-033 with Modification Number 3655
Single sourceAT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (
Single source1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)[source]
340B · 2 × General Electric CT7 -9B turboprop engines (1,870 shp) each for take-off (ISA, APR)
Single source2 × General Electric CT7 -9B turboprop engines, 1,390 kW (1,870 shp) each for take-off (ISA, APR)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 1983–1999[source] |
|---|
| First flight | 1990[source] | 25 January 1983[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | Saab 340 AEW&C[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 34 passengers, Maximum payload : 7500 lb / 3400 kg[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root: NASA MS(1)-0316 ; tip: NASA MS(1)-0312[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary user | — | Rex Airlines[source] |
|---|
| Number built | — | 459[source] |
|---|
| Introduction date | — | 1984[source] |
|---|
| Developed into | — | Saab 2000[source] |
|---|
| Fuel capacity | — | 5690 lb / 2580 kg[source] |
|---|
| Propellers | — | 4-bladed Hamilton Standard 14RF19 (or Dowty Rotol ), 3.35 m (11 ft 0 in) diameter four-blade constant speed, fully-feathering reversible propellers[source] |
|---|
| Fuel consumption | — | 0.94 kg/km (3.3 lb/mi)[source] |
|---|
| Take-off distance | — | 4220 ft / 1285 m[source] |
|---|
Maximum take-off; 340B · increased to
Single source