Indicated stall speed in flight configuration: 152..159 km/h
Indicated stall speed in takeoff/landing configuration: 147..146 km/h
Dive speed limit: 850 km/h
Maximum load factor: 11 G
Stall angle of attack in flight configuration: 20 °
Stall angle of attack in landing configuration: 16.6 °
Maximum true air speed at sea level, engine mode - Emergency: 477 km/h
Maximum true air speed at 2000 m, engine mode - Emergency: 520 km/h
Maximum true air speed at 5000 m, engine mode - Emergency: 564 km/h
Service ceiling: 10500 m
Climb rate at sea level: 14 m/s
Climb rate at 3000 m: 13.3 m/s
Climb rate at 6000 m: 7 m/s
Maximum performance turn at sea level: 20.5 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 25.5 s, at 270 km/h IAS.
Flight endurance at 3000 m: 2.2 h, at 350 km/h IAS.
Takeoff speed: 140..170 km/h
Glideslope speed: 180..190 km/h
Landing speed: 130..140 km/h
Landing angle: 14.3 °
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 standard aircraft mass.
Note 4: climb rates are given for Combat power, turn times are given for Boosted power.
Engine:
Model: DB-601A
Maximum power in Boosted mode at sea level: 1100 HP
Maximum power in Emergency mode at sea level: 990 HP
Maximum power in Emergency mode at 4500 m: 1020 HP
Maximum power in Combat mode at sea level: 910 HP
Maximum power in Combat mode at 5000 m: 960 HP
Engine modes:
Nominal (unlimited time): 2200 RPM, 1.15 ata
Combat power (up to 30 minutes): 2300 RPM, 1.23 ata
Emergency power (up to 5 minutes): 2400 RPM, 1.3 ata
Boosted power (up to 1 minute): 2400 RPM, 1.4 ata
Water rated temperature in engine output: 94 °C
Water maximum temperature in engine output: 100 °C
Oil rated temperature in engine intake: 30..75 °C
Oil maximum temperature in engine intake: 80 °C
Oil rated temperature in engine output: 95 °C
Oil maximum temperature in engine output: 105 °C
Supercharger gear shift altitude: fluid coupling
Empty weight: 2049 kg
Minimum weight (no ammo, 10% fuel): 2340 kg
Standard weight: 2614 kg
Maximum takeoff weight: 2893 kg
Fuel load: 304 kg / 400 l
Useful load: 844 kg
Forward-firing armament:
2 x 20mm gun "MG FF", 60 rounds, 540 rounds per minute, wing-mounted
2 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, synchronized
Bombs:
Up to 4 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bomb "SC 250"
Length: 8.8 m
Wingspan: 9.9 m
Wing surface: 16.4 m²
Combat debut: August 1940
Operation features:
- The aircraft has a wide automatization of the engine systems, in fact, to control speed it is only necessary to use the throttle lever. There is no need to manually set engine revolutions and mixture or supercharger gear in normal flight.
- To reduce swinging during taxiing due to prop-wash the prop pitch control should be switched to manual mode and pitch should be reduced to minimum.
- Water and oil radiator shutters are controlled manually.
- The aircraft has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by ground personnel.
- The aircraft has a manually controlled horizontal stabilizer. It should be set to +1° before takeoff and to -4°...-5° before landing. Also, it may be used to trim the flight stick during the flight. In a deep dive the stabilizer should be set so that the pilot must push the flight stick forward to maintain the dive angle.
- The aircraft has automatic wing slats. They deploy when the high angle of attack increases which makes pre-stall softer.
- The aircraft has a manual mechanical system for retracting the landing flaps, for this reason it is necessary to extend landing flaps well before final approach. Markers on the left-wing flap indicate how far the flaps are extended. The flaps can be extended to any angle up to 42°.
- The aircraft has a manual tailwheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- The aircraft has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- The aircraft has a fuel gauge which shows total fuel remaining. Also, it has an emergency fuel warning light (80 liters).
- The design of the cockpit canopy does not allow it to be opened during flight. The canopy should be closed before takeoff to prevent damage. The canopy has an emergency release system for bailouts.
- The control system for the bomb rack only allows to drop bombs one by one.
- The gunsight has a sliding sun-filter.
Basic data and recommended positions of the aircraft controls:
-
Starting the engine:
- recommended position of the mixture control lever: auto mixture control
- recommended position of the oil radiator control handle: open
- recommended position of the water radiator control handle: close
- recommended position of the prop pitch control handle: auto prop pitch control
- recommended position of the throttle lever: 10%
- before taxiing, you must unlock the tailwheel
-
Recommended mixture control lever positions for various flight modes: auto mixture control
3.1 Recommended positions of the oil radiator control handle for various flight modes:
- cruise flight: open 50%
- combat: open 50%
- takeoff: open
3.2 Recommended positions of the water radiator control handle for various flight modes:
- cruise flight: open 50%
- combat: open 50%
- takeoff: open 50%
- Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 5.2 l/min
- Combat engine mode: 6.6 l/min
Removed Headrest
Removed pilot armoured headrest for improved field of view
Removed mass: 8 kg
Estimated speed gain: 0 km/h
1 x SC 250 bomb
249 kg General Purpose Bomb SC 250
Additional mass: 279 kg
Ammunition mass: 249 kg
Racks mass: 30 kg
Estimated speed loss before drop: 34 km/h
Estimated speed loss after drop: 11 km/h
Armoured Wind Screen
Additional pilot protection: armoured triplex wind screen
Additional mass: 20 kg
Estimated speed loss: 1 km/h
Additional armour plates
Additional protection: bottom armour plates
Additional mass: 89 kg
Estimated speed loss: 4 km/h
4 x SC 50 bombs
4 x 55 kg General Purpose Bombs SC 50
Additional mass: 260 kg
Ammunition mass: 220 kg
Racks mass: 40 kg
Estimated speed loss before drop: 53 km/h
Estimated speed loss after drop: 13 km/h