Li-2 / IL-2 Sturmovik: Great Battles
Close
menu
Transport
Li-2
History
Specifications

The story of this airplane began in 1935 when Douglas Aircraft created the best passenger and transport airplane of its time — the DC-3. The aircraft became popular and was sold and produced under license all over the world. On April 11, 1936, a decision was made to purchase a license from the U.S. for production in the USSR, and in 1937, development of the licensed DC-3 began at Plant No. 84 in Khimki near Moscow.

Many complex problems had to be solved that could not be solved in Holland or in Japan (Mitsubishi), which also bought licenses but was forced to assemble the DC-3 from parts supplied by the USA. First of all, the dimensions had to be converted from the imperial to the metric system, while at the same time, the structural elements had to be recalculated according to domestic strength standards. The introduction of the pattern method was also no easy task. Plant No. 84 was able to safely overcome the difficulties that arose from time to time and finally organize the mass production of the aircraft under the designation PS-84. At the same time, the Soviet planes were very different from the overseas prototypes: they were built almost entirely from domestic materials, and the internal layout of the compartments was changed. The front door opened inwards, not outwards. M-62IR engines were installed. In general, they cannot be called a complete copy of the DC-3. On September 17, 1942, the aircraft received the designation Li-2, after the name of engineer B.P. Lisunov, who supervised the introduction of the aircraft into mass production (at the same time, until the end of the war, the new designation was applied only to military versions of the aircraft).

The aircraft was produced in many modifications, the most important being the following:
  • Li-2. Almost all Li-2s for military use were equipped with weapons and bomb racks. A bomb sight was installed. At the beginning of production, an MV-3 upper turret with a 7.62 caliber ShKAS machine gun was installed, later (from about autumn 1942) it was replaced by a UTK-1 turret with a 12.7 mm UBT machine gun. The aircraft could carry 1000 kg of bombs externally. The crew consisted of 6 airmen: two pilots, a navigator, a flight mechanic, a radio operator, and a gunner. From the fall of 1942, the Li-2 was produced as a multi-purpose military aircraft: in the cargo compartment, enlarged by the front cargo racks, the floor was reinforced and a large cargo hatch was installed on the left side. It could carry 18 stretchers in three tiers, and three folding seats made it possible to carry two slightly wounded people and a medic. Folding plywood benches along the sides of the fuselage made it possible to carry paratroopers.
  • Li-2NB - Night Bomber. Armament: 3 ShKAS machine guns (1 in the nose) and a 12.7 mm UBT turret. Four externally mounted bombs, each weighing 250 kg. The crew accommodation was modified. The cockpit door on the starboard side became convex, and behind it was placed an NKPB-7 (night) bomb sight, facing into the lower part of the door, whose glazing could be folded down to improve visibility. Instead of the RPK-2 radio semi-compass, the American Bendix MN-26C was installed, and the RSB-bis radio station was replaced by the RSR-1.
  • Li-2D - airborne, for dropping paratroopers (1942) with a turret-mounted 12.7 mm machine gun (sometimes coaxial 7.62 mm).
  • Li-2 (2M-88) - a series produced beginning in 1943, differing only in the type of engines with a power of 1100 hp. and weapons (a turret machine gun). It could carry 25 soldiers and reach speeds up to 350 km/h.
  • Li-2VP - an experimental night bomber with bombs placed in the cabin and dropped through tunnels in the floor. Armament - UTK-1 turret in the upper fuselage and two 7.62 mm ShKAS in the side hatches. Load from 1.5 to 2.5 tons of bombs.
  • Li-2T - post-war transport modification.

A total of 5,207 Li-2s were produced between 1939 and May 1953.

With the beginning of the Great Patriotic War, the aircraft performed a wide variety of tasks: the Li-2 dropped cargo to partisans, surrounded troops, landed troops, evacuated the wounded (including from besieged Sevastopol), transported military leaders, delivered orders, and was also used as a night bomber. By the summer of 1943, the Air Force had three air corps, including the 7th Air Corps of the ADD, almost entirely armed with Li-2s in both transport and bomber versions. By the end of the war, there were a total of 19 regiments that were equipped with these aircraft. The Li-2 was operated by the military transport aviation of the USSR Air Force until the 70s and was also supplied to other countries.

Sources:

1. Perov V., Rastrenin O. “Li-2 - “Air Horse” Airplanes of the World No. 1,2. 2000

2. V.B. Shavrov “History of aircraft designs in the USSR 1938-1950” 1988

3. Filimonov M. “The same “Dakota” Wings of the Motherland No. 12. 1993

4. Website https://aviarmor.net

Indicated stall speed in flight configuration: 115...135 km/h
Indicated stall speed in takeoff/landing configuration: 105...120 km/h
Dive speed limit: 410 km/h
Maximum load factor: 5.0 G
Stall angle of attack in flight configuration: 13 °
Stall angle of attack in landing configuration: 12.5 °
 
Maximum true air speed at sea level, engine mode - take-off: 322 km/h
Maximum true air speed at 900 m, engine mode - take-off: 333 km/h
 
Maximum true air speed at sea level, engine mode - economical maximum: 303 km/h
Maximum true air speed at 1700 m, engine mode - economical maximum: 320 km/h
 
Service ceiling: 5500 m
Climb rate at sea level: 4,0 m/s
Climb rate at 3000 m: 2,5 m/s
 
Maximum performance turn at sea level: 25.5 s, at 220 km/h IAS.
 
Flight endurance at 4000 m: 9h, at 2000 rpm / 640 mm Hg MAP
 
Takeoff speed: 120..130 km/h
Glideslope speed: 150..165 km/h
Landing speed: 105..115 km/h
Landing angle: 11.5 °
 
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 maximum continuous power, turn times are given for nominal power.
 
Engine:
Model: M-62IR
Maximum power in take-off mode at sea level: 1000 HP
Maximum power in maximum continuous (nominal) mode at sea level: 820 HP
 
Maximum power in maximum continuous (nominal) mode at 1700 m: 840 HP
 
Engine modes:
Take-off (up to 5 minutes): 2200 RPM, 1050 mm Hg
Nominal: 2100 RPM, 900 mm Hg
 
Oil rated temperature in engine output: 115 °C
Oil maximum temperature in engine output: 125 °C
Cylinder head rated temperature: 205 °C
Cylinder head maximum temperature: 235 °C
 
Empty weight: 7526 kg
Maximum takeoff weight: 11600 kg
Fuel load: 2240 kg / 3110 l
Useful load: 4074 kg 
 
Forward-firing armament:
7.62 mm "ShKAS" machine gun, 450 rounds, 1800 rounds per minute, nose-mounted
 
Defensive armament:
Top: 12.7 mm machine gun "UBT" in UTK-1 turret, 230 rounds, 1000 rounds per minute
Left: 7.62 mm "ShKAS" machine gun, 500 rounds, 1800 rounds per minute
Right: 7.62 mm "ShKAS" machine gun, 500 rounds, 1800 rounds per minute
 
Bombs:
Up to 4 x 254 kg general purpose bombs "FAB-250sv"
Up to 2 x 512 kg general purpose bombs "FAB-500M"
 
Length: 19.65 m
Wingspan: 28,81 m 
Wing surface: 91,7 m²
 
Combat debut: Autumn 1942
 
Operation features:
- IMPORTANT: take up to 50% fuel in cargo loadout to not exceed the maximum takeoff weight.
- The engine has no manifold pressure automatic governor. For this reason, manifold pressure not only depends on throttle position, but also from RPM and altitude. This requires additional checking of manifold pressure to not cause engine damage.
- Engine mixture control is automatic when the mixture lever is set to maximum. It is possible to manually lean the mixture by moving the mixture control to less than maximum. This also reduces fuel consumption during flight.
- 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.
- Oil radiators and engine cowl outlet shutters are manually operated.
- 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 50°.
- 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 is equipped with a parking brake system.
- The aircraft is equipped with landing and navigation lights.
- The engine has a one-stage mechanical supercharger.
- The aircraft has a fuel gauge which shows remaining fuel in fuel tanks depending on switch position. In the game the fuel indicator switch changes by pressing (RShift+I).
- The aircraft has a manual control for the tailwheel lock. The unlocked tailwheel has no turn limit. The tailwheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- The aircraft is equipped with three-channel autopilot system (main switch RAlt + A). Pilot has the ability to trim course (RAlt + Left/Right), pitch (RAlt + Up/Down) and roll (RShift + Left/Right) stabilizing angles.
- Cargo unload doors can be opened on the ground only.
- The side door must be opened for dropping paratroopers or cargo containers stored inside. Open it using the bomb bay doors toggle command ("N" by default) and then use the bomb drop button ("B" by default) to drop them.
 
Basic data and recommended positions of the aircraft controls:
1. Starting the engine:
- recommended position of the mixture control lever: forward
- recommended position of the cowl flap control handle: close
- recommended position of the radiator control handle: open 50%
- recommended position of the prop pitch control handle: heavy
- recommended position of the throttle lever: 15%
- before taxiing, you must unlock the tailwheel
- before taxiing, the parking brake must be released
 
2. Recommended mixture control lever positions for various flight modes:
- When running the engine at low throttle near the ground, the mixture control lever should be in the position of about 60%
- When the engine is running at full throttle near the ground, the mixture control lever should be in the 40-50% position.
- As you gain altitude, the altitude corrector closes.
 
3.1 Recommended positions of the radiator/cowl flap control handle for various flight modes: / no control of radiators/cowl flaps
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 50% (in winter conditions - close if necessary)
- combat: open 50%
 
3.2 Recommended positions of the radiator/cowl flap control handle for various flight modes: / no control of radiators/cowl flaps
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 40% (in winter conditions - close if necessary)
- combat: open 50%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 7.7 l/min
- Combat engine mode: 9.8 l/min
Up