il2

A-20B

a20b

Description

Indicated stall speed in flight configuration: 161..193 km/h (100..120 mph)
Indicated stall speed in takeoff/landing configuration: 139..166 km/h (86..103 mph)

Dive speed limit: 665 km/h (412 mph)
Maximum load factor: 6.5 G
Stall angle of attack in flight configuration: 19.1 °
Stall angle of attack in landing configuration: 17.1 °

Maximum true air speed at sea level, engine mode - Combat: 505 km/h (314 mph)
Maximum true air speed at 1000 m, engine mode - Combat: 524 km/h (326 mph)
Maximum true air speed at 5000 m, engine mode - Combat: 544 km/h (338 mph)

Maximum true air speed at sea level, engine mode - Nominal: 467 km/h (290 mph)
Maximum true air speed at 2000 m, engine mode - Nominal: 500 km/h (311 mph)
Maximum true air speed at 5000 m, engine mode - Nominal: 525 km/h (326 mph)

Service ceiling: 8700 m (28540 ft)
Climb rate at sea level: 10.0 m/s (1969 ft/min)
Climb rate at 3000 m: 8.2 m/s (1614 ft/min)
Climb rate at 6000 m: 5.0 m/s (984 ft/min)

Maximum performance turn at sea level: 24.5 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 34.1 s, at 270 km/h IAS.

Flight endurance at 3000 m: 3.4 h, at 350 km/h IAS. Engine mode - Cruise, 1st supercharger stage

Takeoff speed: 170..195 km/h (105..120 mph)
Glideslope speed: 185..225 km/h (115..140 mph)
Landing speed: 150..170 km/h (95..105 mph)
Landing angle: 3.4 °

Note 1: the data provided is for international standard atmosphere (ISA).
Note 2: flight performance ranges are given for possible aircraft mass ranges.
Note 3: maximum speeds, climb rates and turn times are given for aircraft mass with 8 FAB-100 bombs.
Note 4: climb rates and turn times are given for Nominal power.

Engine:
Model: Wright R-2600-11
Maximum power in Cruise mode at 5500 ft: 810 HP
Maximum power in Cruise mode at 12000 ft: 765 HP
Maximum power in Nominal mode at 5500 ft: 1350 HP
Maximum power in Nominal mode at 12000 ft: 1275 HP
Maximum power in Combat mode at sea level: 1600 HP
Maximum power in Combat mode at 11500 ft: 1400 HP

Engine modes:
(boost value is listed for 1st and 2nd supercharger gears)
Cruise (unlimited time): 1705 RPM, 27,5 / 30,0 inch Hg, mixture “Auto Lean”
Nominal (unlimited time): 2300 RPM, 36,0 / 40,0 inch Hg, mixture “Auto Rich”
Combat (5 min limit): 2400 RPM, 43,0 / 41,0 inch Hg, mixture “Auto Rich”

Oil rated temperature in engine output: 80..95 °C
Oil maximum temperature in engine output: 105 °C
Cylinder head rated temperature: 140..240 °C
Cylinder head maximum temperature: 260 °C

Supercharger gear shift altitude: 2900 m (9500 ft)

Empty weight: 6781 kg
Minimum weight (no ammo, 10%25 fuel): 7359 kg
Standard weight: 8366 kg
Maximum takeoff weight: 10466 kg
Fuel load: 1057 kg / 1468 l / 388 gal
Useful load: 3665 kg

Forward-firing armament:
12.7mm machine gun ANM2 .50, 200 rounds, 850 rounds per minute, nose-mounted

Defensive armament:
Top: 12.7mm machine gun ANM2 .50, 390 rounds, 850 rounds per minute
Belly: 7.92mm machine gun ANM2 .30, 600 rounds, 1150 rounds per minute

Bombs:
Up to 20 x 104 kg general purpose bombs FAB-100M
Up to 4 x 254 kg general purpose bombs FAB-250ck

Length: 14.54 m
Wingspan: 18.69 m
Wing surface: 43.18 m²

Combat debut: spring 1942

Operation features:

Modifications

4 x FAB-250tsk bombs
4 x 254 kg General Purpose Bombs FAB-250tsk
Additional mass: 1016 kg
Ammunition mass: 1016 kg
Estimated speed loss before drop: 39 km/h
Estimated speed loss after drop: 16 km/h

20 x FAB-100M bombs
20 x 104 kg General Purpose Bombs FAB-100M
Additional mass: 2080 kg
Ammunition mass: 2080 kg
Estimated speed loss before drop: 39 km/h
Estimated speed loss after drop: 16 km/h

Bendix MN-26
Fixed loop radio compass for navigation with radio beacons
Additional mass: 20 kg
Estimated speed loss: 0 km/h