C-47A / IL-2 Sturmovik: Great Battles
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Transport
C-47A
History
Specifications

In 1935, Douglas Aircraft created the most advanced passenger and transport aircraft of its time — the DC-3. The plane became popular and was sold and produced under license throughout the world, including the USSR in a significantly modified form under the name Li-2.

The first military version, the C-47A (based on the DC-3A), entered service in August 1939, while the C-47s specially adapted for military transport, called Skytrain, went into production in November 1941.

The C-47 was an all-metal low-wing aircraft with no external struts, a single wing, and retractable main landing gear struts. The wing was equipped with hydraulically operated landing flaps and light alloy ailerons with canvas surfaces. The leading edges of the wings and the tail were equipped with pneumatic rubber deicers. The power plant consisted of two R-1830-92 "Twin Wasp" engines with 1050 HP each at an altitude of 2285 meters. The crew consisted of 3 persons: two pilots and a radio operator.

In the cargo version, the C-47 could carry a payload of 2,722 kg. Other variants provided for the transport of 28 fully armed paratroopers (on folding bucket seats along the cockpit sides) or 18 wounded on stretchers and a three-person medical staff. Under the fuselage could be installed attachments and a mechanism for dropping parachute containers.

Major production modifications:
  • C-47 (R4D-1, designated "Dakota" I in the United Kingdom), a 28-seat transport with R-1830-92 engines, cargo doors, reinforced floor, extended wing, and astrodome, based on the DC-3A-360;
  • C-47A (R4D-5, "Dakota" III), with reinforced landing gear and improved electrical equipment;
  • C-47B (R4D-6, "Dakota" IV), with R-1830-90/90B/9C engines with two-stage superchargers for better altitude;
  • C-47D, a conversion of the C-47B engines to one supercharger speed;

The C-47 was used extensively by the Allies during the war and was used in all theaters. In the fall of 1942, Dakotas landed Anglo-American paratroopers in North Africa. In July 1943, the Dakotas landed Allied paratroopers in Sicily, in June 1944 in Normandy, and in August in southern France. The Dakotas also participated in the Arnhem operation and the crossing of the Rhine. C-47s were used for transportation in the Far Eastern theater. Thus, from 1943 to 1945, C-47s were used to transport cargo in the Far Eastern theater of operations. C-47s were used to transport supplies across the Himalayas to China and provided offensive support in the jungles of Burma where there was simply no other method of supply. The last major airborne landing was made by the British near Rangoon, Myanmar.

Approximately 600 aircraft were used by the U.S. Navy under the designation R4D.

Soviet C-47s delivered urgent cargoes during the Battle of Kursk, participated in the landing on the Bukrinsky bridgehead behind the Dnieper in 1944, provided "air bridges" to Slovakia and Yugoslavia, and supported actions on all fronts and fleets in the final stages of the war. Northern Fleet aviation used the C-47 to search for German U-boats in the Arctic. It did not carry bombs, but thanks to a large fuel reserve it could patrol for long periods in remote areas where other types of aircraft could not reach.

The transports also performed well during the short campaign in the Far East: the pace of the Soviet offensive was so fast that the forward tank units could only be supplied with fuel by air (the C-47 usually carried 12 barrels, and ammunition was also delivered by air). Groups of two to ten planes landed amphibious assaults in Harbin, Mukden, Girin, Port Arthur, and other places.

In the post-war period, the C-47 was used by many countries around the world as a bomber and transport aircraft in colonial and local wars. During the Vietnam War, the Americans upgraded several to AC-47 heavy attack aircraft, which strafed guerrilla areas. The last time C-47 bombers were used was in the "soccer" war between El Salvador and Honduras in July 1969 — Salvadoran crews used them to attack military installations in border areas.

Sources:

1. Kotelnikov V. "Douglas C-47 transport airplane" Aviakollektsiya №10. 2008

2. Website https://daveswarbirds.com

3. Filimonov M. "All the same "Dakota"" Wings of the Homeland No. 12. 1993

4. Rene J. Francillon "McDonnell Douglas Aircraft Since 1920, Vol 1". 1988

5. Website https://aviarmor.net

Indicated stall speed in flight configuration: 73...88 mph (118...142 km/h)
Indicated stall speed in takeoff/landing configuration: 67...77 mph (107...124 km/h)
Dive speed limit: 255 mph (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: 365 km/h (227 mph)
Maximum true air speed at 2000 m (6562 feet), engine mode - take-off: 394 km/h (245 mph)
 
Maximum true air speed at sea level, engine mode - economical maximum: 288 km/h (179 mph)
Maximum true air speed at 5000 m (16404 feet), engine mode - economical maximum: 348 km/h (216 mph)
 
Service ceiling: 8000 m (26247 feet)
Climb rate at sea level: 6,7 m/s (1319 fpm)
Climb rate at 3000 m: 6,2 m/s (1220 fpm)
Climb rate at 6000 m: 2,9 m/s (571 fpm)
 
Maximum performance turn at sea level: 22.0 s, at 175 mph (282 km/h) IAS.
Maximum performance turn at 3000 m (9843 feet): 31.0 s, at 165 mph (262 km/h) IAS.
 
Flight endurance at 3000 m (9843 feet): 3.5, at 300 km/h (187 mph) IAS.
 
Takeoff speed: 75...85 mph (121..137 km/h)
Glideslope speed: 95..105 mph (153..169 km/h)
Landing speed: 70..80 mph (112..128 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 Take-off power.
 
Engine:
Model: R-1830-92
Maximum power in take-off mode at sea level: 1170 HP
Maximum power in maximum continuous mode at sea level: 1030 HP
Maximum power in economical maximum mode at sea level: 590 HP
 
Maximum power in take-off mode at 4800 feet (1463 m): 1200 HP
Maximum power in maximum continuous mode at 7000 feet (2134 m): 1050 HP
Maximum power in economical maximum mode at 15000 feet (4572 m): 700 HP
 
Engine modes:
Take-off (up to 5 minutes): 2700 RPM, 46.0 inch Hg, "Auto-rich"
Maximum continuous (unlimited time): 2550 RPM, 41 inch Hg, "Auto-lean"
Economical maximum (unlimited time): 2325 RPM, 28.0 inch Hg, "Auto-lean"
 
Oil rated temperature in engine output: 60..75 °C
Oil maximum temperature in engine output: 100 °C
Cylinder head rated temperature: 150..232 °C
Cylinder head maximum temperature: 260 °C
 
Empty weight: 8029 kg (17700 lb)
Minimum weight (no ammo, 10% fuel): 8828 kg (19462 lb)
Standard weight: 6503 kg (14337 lb)
Maximum takeoff weight: 13337 kg (29403 lb)
Fuel load: 2188 kg (4824 lb) / 3043 l (804 gal)
Useful load: 5308 kg (11702 lb)
 
Length: 64.8 feet (19.75 m)
Wingspan: 28,96 m (95 feet)
Wing surface: 91,7 m² (987 feet²)
 
Combat debut: spring 1942
 
Operation features:
- 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.
- The engine is equipped with an automatic fuel mixture control which maintains optimal mixture if mixture lever is set to Auto Rich (66%) position. To use automatic mixture leaning to reduce fuel consumption during flight it is necessary to set mixture lever to Auto Lean (33%) position. In the case of malfunction of the automatic mixture control the mixture lever should be set to Emergency (100%) position. To stop the engine mixture lever should be set to the Idle Cut Off (0%25) position.
- 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 formation, navigation and landing 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 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 left passenger door must be removed before flight for dropping paratroopers or cargo containers. 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: Emergency
- recommended position of the cowl flaps control handle: open
- recommended position of the radiator control handle: open
- recommended position of the prop pitch control handle: 0%
- recommended position of the throttle lever: 20%
- 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: Auto Rich (auto mixture control) (Auto Lean if necessary to save fuel)
 
3.1 Recommended positions of cowl flaps for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 40% (in winter conditions - close if necessary)
- combat: open 50%
 
3.2 Recommended positions of the oil 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%
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 15.0 l/min
- Combat engine mode: 22.0 l/min
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