Air Tractor AT-802 vs Antonov An-74: 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-74 — licensed reference photograph

BSupport aircraft

Antonov An-74

Transport aircraft

Credit

Dmitry A. Mottl · 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-74Length

28.07 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

16 of 28 rows sourced on both sides

10.95mAT-802 · Length

28.07m

Length

All recorded figures & sources

10.95 m

AT-802 · Length

Single source

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

28.07 m

Length

Single source

28.07 m (92 ft 1 in)^[source]

18.06mAT-802 · Wingspan

31.89m

Wingspan

All recorded figures & sources

18.06 m

AT-802 · Wingspan

Single source

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

31.89 m

Wingspan

Single source

31.89 m (104 ft 7.5 in)^[source]

3.89mAT-802 · Height

8.65m

Height

All recorded figures & sources

3.89 m

AT-802 · Height

Single source

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

8.65 m

Height

Single source

8.65 m (28 ft 4.5 in)^[source]

7.3t

34.5tGross; Gross 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]

19,050 kg

Empty; Empty weight

Single source

34,500 kg

Gross; Gross weight

Single source

19,050 kg (42,000 lb)^[source]

34,500 kg (76,058 lb)^[source]

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

700km/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]

600.285312 km/h

Cruise; 297 or

Single source

600 km/h

Cruise; 550 or 342 or

Single source

600.048 km/h

Cruise; Cruise speed

Single source

700 km/h

Maximum; Maximum speed

Single source

700 km/h (435 mph, 378 kn)^[source]

550 or 600 km/h (342 or 373 mph, 297 or 324 kn)^[source]

1,300kmAT-802 · Range

4,325km

Range

All recorded figures & sources

1,300 km

AT-802 · Range

Single source

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

4,325 km

Range

Single source

4,325 km (2,688 mi, 2,336 nmi)^[source]

1,010kW

—

Power

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]

—

63.9kN2 × Lotarev D-36 series 1A thrust each

Thrust

All recorded figures & sources

63.9 kN

2 × Lotarev D-36 series 1A thrust each

Single source

2 × Lotarev D-36 series 1A , 63.9 kN (14,330 lbf) thrust each^[source]

37.3m²AT-802 · Wing area

98.6m²

Wing area

All recorded figures & sources

37.25 m²

AT-802 · Wing area

Single source

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

98.62 m²

Wing area

Single source

98.62 m 2 (1,062 sq ft)^[source]

4,000mAT-802 · Service ceiling

10,100m

Service ceiling

All recorded figures & sources

4,000 m

AT-802 · Service ceiling

Single source

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

10,100 m

Service ceiling

Single source

10,100 m (33,136 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-74 configuration
Specification	Air Tractor AT-802	Antonov An-74
Crew	One or Two (AT-802A – single-seat)^[source]	five (captain, first officer, navigator, flight engineer, loadmaster)^[source]
Type	Agricultural / Fire-fighting aircraft^[source]	Transport aircraft^[source]
National origin	United States^[source]	Soviet Union / Ukraine^[source]
Manufacturer	Air Tractor^[source]	Antonov^[source]
Status	Active^[source]	In service^[source]
Manufactured	1990–present^[source]	1986–2004^[source]
First flight	1990^[source]	September 29, 1983^[source]
Variant	L3Harris OA-1K Skyraider II^[source]	—
Capacity	820 US gal (683 imp gal; 3,104 L)^[source]	up to 52 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]	—
Primary users	—	Islamic Revolutionary Guard Corps Aerospace Force Utair Egyptian Air Force Pouya Air^[source]
Number built	—	62^[source]
Introduction date	—	1983^[source]
Developed from	—	Antonov An-72^[source]

FORCETALLY

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Air Tractor AT-802

Antonov An-74

Crew

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

five (captain, first officer, navigator, flight engineer, loadmaster)^[source]

Type

Agricultural / Fire-fighting aircraft^[source]

Transport aircraft^[source]

National origin

United States^[source]

Soviet Union / Ukraine^[source]

Manufacturer

Air Tractor^[source]

Antonov^[source]

Status

Active^[source]

In service^[source]

Manufactured

1990–present^[source]

1986–2004^[source]

First flight

1990^[source]

September 29, 1983^[source]

Variant

L3Harris OA-1K Skyraider II^[source]

—

Capacity

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

up to 52 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]

—

Primary users

—

Islamic Revolutionary Guard Corps Aerospace Force Utair Egyptian Air Force Pouya Air^[source]

Number built

—

62^[source]

Introduction date

—

1983^[source]

Developed from

—

Antonov An-72^[source]