Air Tractor AT-802 vs Saab 2000: Specs Compared

Air Tractor AT-802 — licensed reference photograph

ASupport aircraft

Air Tractor AT-802

Agricultural / Fire-fighting aircraft

Credit

Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified

Saab 2000 — licensed reference photograph

BSupport aircraft

Saab 2000

Turboprop Regional airliner

Credit

ISORauscht · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Air Tractor AT-802AT-802 · Length

10.95 m

Length source ↗

Saab 2000Length

27.28 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

19 of 27 rows sourced on both sides

10.95mAT-802 · Length

27.28m

Length

All recorded figures & sources

10.95 m

AT-802 · Length

Single source

35 ft 11 in (10.95 m)^[source]

27.28 m

Length

Cross-checked

27.28 m

Official specification · length; 27,28 m

Manufacturer claim

27.28 m

Saab 2000 specs · Length

Cross-checked

27.28 m (89 ft 6 in)^[source]

27,28 m^[source]

27,28 m^[source]Saab 2000 specs

18.06mAT-802 · Wingspan

24.76mSaab 2000 specs · Wingspan

WingspanScopes differ

All recorded figures & sources

18.06 m

AT-802 · Wingspan

Single source

59 ft 3 in (18.06 m)^[source]

24.76 m

Saab 2000 specs · Wingspan

Cross-checked

24.76 m

Wingspan

Cross-checked

24.76 m (81 ft 3 in)^[source]

24,76 m^[source]Saab 2000 specs

3.89mAT-802 · Height

7.73m

Height

All recorded figures & sources

3.89 m

AT-802 · Height

Single source

12 ft 9 in (3.89 m)^[source]

7.73 m

Height

Cross-checked

7.73 m

Official specification · height; 7,73 m

Manufacturer claim

7.73 m

Saab 2000 specs · Height

Cross-checked

7.73 m (25 ft 4 in)^[source]

7,73 m^[source]

7,73 m^[source]Saab 2000 specs

7.3t

22.8tMaximum take-off; Max takeoff weight

MassScopes differ

All recorded figures & sources

2,951 kg

Empty; AT-802 · Empty weight

Single source

7,257 kg

Maximum take-off; AT-802 · Max takeoff weight

Single source

6,505 lb (2,951 kg)^[source]

16,000 lb (7,257 kg)^[source]

13,800 kg

Empty; Empty weight

Single source

22,800 kg

Maximum take-off; Max takeoff weight

Single source

One or Two (AT-802A – single-seat)

Crew

All recorded figures & sources

One or Two (AT-802A – single-seat)^[source]

2 people

Crew

Single source

2^[source]

356km/hCruise; AT-802 · at 8,000 ft (2,440 m)

685km/hMaximum; Maximum speed

SpeedScopes differ

All recorded figures & sources

356 km/h

Cruise; AT-802 · at 8,000 ft (2,440 m)

Single source

221 mph (356 km/h, 192 kn) at 8,000 ft (2,440 m)^[source]

665 km/h

Cruise; Cruise speed

Single source

685 km/h

Maximum; Maximum speed

Single source

685 km/h (426 mph, 370 kn)^[source]

665 km/h (413 mph, 359 kn)^[source]

1,300kmAT-802 · Range

2,869km

Range

All recorded figures & sources

1,300 km

AT-802 · Range

Single source

800 mi (1,300 km, 700 nmi)^[source]

2,869 km

Range

Single source

2,869 km (1,783 mi, 1,549 nmi)^[source]

1,010kW

3,096kW

PowerScopes differ

All recorded figures & sources

1,010 kW

AT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (

Single source

1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)^[source]

3,096 kW

2 × Rolls-Royce AE 2100P turboprop engines each

Single source

2 × Rolls-Royce AE 2100P turboprop engines, 3,096 kW (4,152 hp) each^[source]

37.3m²AT-802 · Wing area

55.7m²

Wing area

All recorded figures & sources

37.25 m²

AT-802 · Wing area

Single source

401.0 sq ft (37.25 m 2 )^[source]

55.7 m²

Wing area

Single source

55.7 m 2 (600 sq ft)^[source]

4,000mAT-802 · Service ceiling

9,450m

Service ceiling

All recorded figures & sources

4,000 m

AT-802 · Service ceiling

Single source

13,000 ft (4,000 m)^[source]

9,450 m

Service ceiling

Single source

9,450 m (31,000 ft)^[source]

4.3m/sAT-802 · 850 ft/min (

11m/s2,240 ft/min

Rate of climbScopes differ

All recorded figures & sources

4.3 m/s

AT-802 · 850 ft/min (

Single source

850 ft/min (4.3 m/s)^[source]

11.4 m/s

2,240 ft/min

Single source

11.4 m/s (2,240 ft/min)^[source]

Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.

Configuration

Details

Air Tractor AT-802 and Saab 2000 configuration
Specification	Air Tractor AT-802	Saab 2000
Type	Agricultural / Fire-fighting aircraft^[source]	Turboprop Regional airliner^[source]
National origin	United States^[source]	Sweden^[source]
Manufacturer	Air Tractor^[source]	Saab AB^[source]
Status	Active^[source]	In limited passenger service, in military service^[source]
Manufactured	1990–present^[source]	1992–1999^[source]
First flight	1990^[source]	26 March 1992^[source]
Variant	L3Harris OA-1K Skyraider II^[source]	—
Capacity	820 US gal (683 imp gal; 3,104 L)^[source]	50–58 passengers / 5,900 kg (13,007 lb) payload^[source] 4.250 kg^[source] 50–58 passengers / 5,900 kg (13,007 lb) payload^[source]
Aspect ratio	8.8:1^[source]	—
Airfoil	NACA 4415^[source]	root: NASA/Langley MS(1)-0316; tip: NASA/Langley MS(1)-0312^[source]
Stall speed	91 mph (146 km/h, 79 kn) (power off, flaps down)^[source]	—
Number built	—	63^[source]
Introduction date	—	30 August 1994^[source]
Developed from	—	Saab 340^[source]
Propellers	—	6-bladed Dowty Propellers constant-speed composite fully feathering and reversible-pitch propellers^[source]
Field length	—	1,200 m^[source]

FORCETALLY

Loading the evidence…

Preparing your view.

Air Tractor AT-802

Saab 2000

Type

Agricultural / Fire-fighting aircraft^[source]

Turboprop Regional airliner^[source]

National origin

United States^[source]

Sweden^[source]

Manufacturer

Air Tractor^[source]

Saab AB^[source]

Status

Active^[source]

In limited passenger service, in military service^[source]

Manufactured

1990–present^[source]

1992–1999^[source]

First flight

1990^[source]

26 March 1992^[source]

Variant

L3Harris OA-1K Skyraider II^[source]

—

Capacity

820 US gal (683 imp gal; 3,104 L)^[source]

50–58 passengers / 5,900 kg (13,007 lb) payload^[source]

4.250 kg^[source]

50–58 passengers / 5,900 kg (13,007 lb) payload^[source]

Aspect ratio

8.8:1^[source]

—

Airfoil

NACA 4415^[source]

root: NASA/Langley MS(1)-0316; tip: NASA/Langley MS(1)-0312^[source]

Stall speed

91 mph (146 km/h, 79 kn) (power off, flaps down)^[source]

—

Number built

—

63^[source]

Introduction date

—

30 August 1994^[source]

Developed from

—

Saab 340^[source]

Propellers

—

6-bladed Dowty Propellers constant-speed composite fully feathering and reversible-pitch propellers^[source]

Field length

—

1,200 m^[source]