Air Tractor AT-802 vs Antonov An-32: 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

Antonov An-32 — licensed reference photograph

BSupport aircraft

Antonov An-32

Military transport aircraft

Credit

Oleg Belyakov · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · 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 ↗

Antonov An-32An-32 · Length

23.78 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

17 of 28 rows sourced on both sides

10.95mAT-802 · Length

23.78mAn-32 · Length

LengthScopes differ

All recorded figures & sources

10.95 m

AT-802 · Length

Single source

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

23.78 m

An-32 · Length

Single source

23.78 m (78 ft 0 in)^[source]

18.06mAT-802 · Wingspan

29.2mAn-32 · Wingspan

WingspanScopes differ

All recorded figures & sources

18.06 m

AT-802 · Wingspan

Single source

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

29.2 m

An-32 · Wingspan

Single source

29.2 m (95 ft 10 in)^[source]

3.89mAT-802 · Height

8.75mAn-32 · Height

HeightScopes differ

All recorded figures & sources

3.89 m

AT-802 · Height

Single source

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

8.75 m

An-32 · Height

Single source

8.75 m (28 ft 8 in)^[source]

7.3t

27t

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]

16,800 kg

Empty; An-32 · Empty weight

Single source

27,000 kg

Maximum take-off; An-32 · Max takeoff weight

Single source

16,800 kg (37,038 lb)^[source]

27,000 kg (59,525 lb)^[source]

One or Two (AT-802A – single-seat)

4An-32 · Crew

Crew

All recorded figures & sources

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

4 people

An-32 · Crew

Single source

4^[source]

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

530km/hMaximum; An-32 · 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]

470 km/h

Cruise; An-32 · Cruise speed

Single source

530 km/h

Maximum; An-32 · Maximum speed

Single source

530 km/h (330 mph, 290 kn)^[source]

470 km/h (290 mph, 250 kn)^[source]

1,300kmAT-802 · Range

2,500km

RangeScopes differ

All recorded figures & sources

1,300 km

AT-802 · Range

Single source

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

2,500 km

An-32 · with 3,700 kg (8,160 lb) payload, no reserves

Single source

2,500 km (1,600 mi, 1,300 nmi) with 3,700 kg (8,160 lb) payload, no reserves^[source]

1,010kW

3,812kW

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]

3,812 kW

An-32 · 2 × ZMKB Progress AI-20DM turboprop engines each

Single source

2 × ZMKB Progress AI-20DM turboprop engines, 3,812 kW (5,112 hp) each^[source]

37.3m²AT-802 · Wing area

75m²An-32 · Wing area

Wing areaScopes differ

All recorded figures & sources

37.25 m²

AT-802 · Wing area

Single source

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

75 m²

An-32 · Wing area

Single source

75 m 2 (810 sq ft)^[source]

4,000mAT-802 · Service ceiling

9,500mAn-32 · Service ceiling

Service ceilingScopes differ

All recorded figures & sources

4,000 m

AT-802 · Service ceiling

Single source

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

9,500 m

An-32 · Service ceiling

Single source

9,500 m (31,200 ft)^[source]

4.3m/sAT-802 · 850 ft/min (

—

Rate of climb

All recorded figures & sources

4.3 m/s

AT-802 · 850 ft/min (

Single source

850 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.

Configuration

Details

Air Tractor AT-802 and Antonov An-32 configuration
Specification	Air Tractor AT-802	Antonov An-32
Type	Agricultural / Fire-fighting aircraft^[source]	Military transport aircraft^[source]
National origin	United States^[source]	Soviet Union / Russia / Ukraine^[source]
Manufacturer	Air Tractor^[source]	Antonov Serial Production Plant^[source]
Status	Active^[source]	In service^[source]
Manufactured	1990–present^[source]	1982–2012^[source]
First flight	1990^[source]	9 July 1976^[source]
Variant	L3Harris OA-1K Skyraider II^[source]	—
Capacity	820 US gal (683 imp gal; 3,104 L)^[source]	42 paratroopers/50 passengers/24 Casualties on stretcher with three medical personnel / 6,700 kg (14,771 lb) max payload^[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	—	Antonov^[source]
Primary users	—	Indian Air Force National Air Force of Angola Sri Lanka Air Force Ukrainian Air Force^[source]
Number built	—	373^[source]
Developed from	—	Antonov An-26^[source]
Developed into	—	Antonov/Taqnia An-132^[source]
Propellers	—	4-bladed constant speed propellers^[source]

FORCETALLY

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Air Tractor AT-802

Antonov An-32

Type

Agricultural / Fire-fighting aircraft^[source]

Military transport aircraft^[source]

National origin

United States^[source]

Soviet Union / Russia / Ukraine^[source]

Manufacturer

Air Tractor^[source]

Antonov Serial Production Plant^[source]

Status

Active^[source]

In service^[source]

Manufactured

1990–present^[source]

1982–2012^[source]

First flight

1990^[source]

9 July 1976^[source]

Variant

L3Harris OA-1K Skyraider II^[source]

—

Capacity

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

42 paratroopers/50 passengers/24 Casualties on stretcher with three medical personnel / 6,700 kg (14,771 lb) max payload^[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

—

Antonov^[source]

Primary users

—

Indian Air Force National Air Force of Angola Sri Lanka Air Force Ukrainian Air Force^[source]

Number built

—

373^[source]

Developed from

—

Antonov An-26^[source]

Developed into

—

Antonov/Taqnia An-132^[source]

Propellers

—

4-bladed constant speed propellers^[source]