il2
He 111 H-16
Description
Indicated stall speed in flight configuration: 150..194 km/h
Indicated stall speed in takeoff/landing configuration: 123..156 km/h
Dive speed limit: 560 km/h
Maximum load factor: 4.5 G
Stall angle of attack in flight configuration: 20 °
Stall angle of attack in landing configuration: 17 °
Maximum true air speed at sea level, engine mode - Climb: 370 km/h
Maximum true air speed at 2000 m, engine mode - Climb: 399 km/h
Maximum true air speed at 5000 m, engine mode - Climb: 410 km/h
Service ceiling: 6850 m
Climb rate at sea level: 5.3 m/s
Climb rate at 3000 m: 4.1 m/s
Climb rate at 6000 m: 2.3 m/s
Maximum performance turn at sea level: 30.8 s, at 250 km/h IAS.
Maximum performance turn at 3000 m: 45.2 s, at 250 km/h IAS.
Flight endurance at 3000 m: 6.7 h, at 300 km/h IAS.
Takeoff speed: 170..210 km/h
Glideslope speed: 180..200 km/h
Landing speed: 125..150 km/h
Landing angle: 9 °
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 Climb power, turn times are given for Take-off power.
Engine:
Model: Jumo-211F
Maximum power in Take-off mode at sea level: 1340 HP
Maximum power in Climb mode at sea level: 1120 HP
Maximum power in Climb mode at 1900 m: 1210 HP
Maximum power in Climb mode at 5300 m: 1060 HP
Engine modes:
Nominal (unlimited time): 2250 RPM, 1.15 ata
Climb power (up to 30 minutes): 2400 RPM, 1.25 ata
Take-off power (up to 1 minute): 2600 RPM, 1.40 ata
Water rated temperature in engine output: 80 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine output: 90 °C
Oil maximum temperature in engine output: 105 °C
Supercharger gear shift altitude: automatic
Empty weight: 8698 kg
Minimum weight (no ammo, 10% fuel): 9831 kg
Standard weight: 13017 kg
Maximum takeoff weight: 15689 kg
Fuel load: 2553 kg / 3450 l
Useful load: 6991 kg
Defensive armament:
Nose: 20mm gun “MG FF”, 240 rounds, 540 rounds per minute
Top: 13mm machine gun “MG 131”, 1000 rounds, 900 rounds per minute
Belly-backward: 2 x 7.92mm machine guns “MG 81”, 850 rounds, 1600 rounds per minute
Left: 7.92mm machine gun “MG 81”, 500 rounds, 1600 rounds per minute
Right: 7.92mm machine gun “MG 81”, 500 rounds, 1600 rounds per minute
Bombs:
Up to 16 x 55 kg general purpose bombs “SC 50”
Up to 4 x 249 kg general purpose bombs “SC 250”
Up to 2 x 500 kg general purpose bombs “SC 500”
Up to 2 x 1090 kg general purpose bombs “SC 1000”
Up to 2 x 1780 kg general purpose bombs “SC 1800”
2400 kg general purpose bomb “SC 2500”
Length: 16.38 m
Wingspan: 22.5 m
Wing surface: 79.5 m²
Combat debut: winter 1943
Operation features:
- Each engine has a two-stage mechanical supercharger with an automatic switch system that switches gears depending altitude and engine revolutions. It can also be manually switched to first gear.
- Engine mixture control is automatic.
- Engine RPM has an automatic governor and it is maintained at the required RPM corresponding to the governor control lever position. The governor automatically controls the propeller pitch to maintain the required RPM.
- Propellers have a feathering system which should be activated in case of engine damage to reduce drag of the propeller in auto-rotation.
- Water and oil radiator shutter controls are manual. The oil radiator control has five fixed positions.
- The aircraft has trimmers for all flight-controls: pitch, roll and yaw.
- Landing flaps have a hydraulic actuator and they can be extended to any angle up to 60°.
- The aircraft tailwheel rotates freely and does not have a lock. For this reason, it is necessary to confidently and accurately operate the rudder pedals during the 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 dedicated fuel gauges for left and right fuel tank groups and there is a switch between the internal and external fuel tank group indicator. In game the fuel indicator switch changes by pressing (RShift+I). Also, the airplane has low fuel warning lights (200 liters) for left and right fuel tank groups.
- The aircraft is equipped with an automatic bomb salvo controller, it allows you to switch between the bomb racks to be released (internal or external) and to switch between different salvo quantities. There is also a controller for a drop delay between each bomb in the salvo.
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: close
- recommended position of the water radiator control handle: close
- recommended position of the prop pitch control handle: light
- recommended position of the throttle lever: 0%
- 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:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 25% (in winter conditions - close if necessary)
- combat: open 50%
3.2 Recommended positions of the water radiator control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 20% (in winter conditions - close if necessary)
- combat: open 50%
- Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 10.4 l/min
- Combat engine mode: 13.6 l/min
Modifications
2 x SC 1000 heavy bombs
2 x 1090 kg General Purpose Bomb SC 1000
Additional mass: 2180 kg
Ammunition mass: 2180 kg
Estimated speed loss before drop: 23 km/h
Estimated speed loss after drop: 0 km/h
SC 2500 heavy bomb
2400 kg General Purpose Bomb SC 2500
Additional mass: 2400 kg
Ammunition mass: 2400 kg
Estimated speed loss before drop: 17 km/h
Estimated speed loss after drop: 0 km/h
2 x SC 1800 heavy bombs
2 x 1780 kg General Purpose Bomb SC 1800
Additional mass: 3560 kg
Ammunition mass: 3560 kg
Estimated speed loss before drop: 32 km/h
Estimated speed loss after drop: 0 km/h