I.A.R. 80-A / IL-2 Sturmovik: Great Battles
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Fighter
I.A.R. 80-A
History
Specifications

In 1925, when an aircraft factory was built in Brasov with the help of French companies, Romania became a member of the countries producing aircraft. The history of this machine began with the purchase in Poland of a license for the PZL P.11f all-metal monoplane fighter. It was a gull-wing monoplane with non-retractable landing gear and an open cockpit. It was developed into the PZL P.24E fighter, which was built under license in Romania in 1937. The Romanian Air Force needed a more modern fighter, and in 1937 Romanian designers began developing such an aircraft to replace the Polish models. A prototype was built and flown in 1939, after which it went into serial production.

The IAR 80 was a single-seat high-speed monoplane with a low wing and retractable landing gear. The wing was an all-metal construction. The ailerons and flaps (hydraulically operated) had a canvas-covered tubular frame. The fuselage was of mixed construction. The forward section up to the cockpit was a trussed tubular frame, while the aft section was a classic semi-monocoque with structural members and stringers. The horizontal stabilizer had struts on the underside. The aircraft was equipped with a version of the French Gnome-Rhone "Mistral-Major" 900 hp engine produced under license in Romania and armed with four 7.92 mm Belgian FN Browning machine guns in the wing. The main disadvantage was the poor forward visibility due to the elongated fuselage forward section, especially dangerous during takeoff and landing. This was due to the placement of the fuel and oil tanks directly behind the engine, in front of the cockpit.

The IAR 80 design was modified during series production in response to operational experience and increased combat effectiveness. For example, the number of machine guns was increased from 4 to 6, and later a more powerful engine was installed — as a result, the fuselage of the first 95-series aircraft had to be reinforced with a Dural "belt" located just behind the cockpit (later the fuselage was modified).

The IAR 80 series 106-130 aircraft of 1941 were powered by the IAR-K14-1001A engine with a takeoff power of 1025 hp and a variable pitch propeller. The structure of the rear fuselage was reinforced with overlapping bands. As in the previous series, armored glass in the front part of the canopy, armor on the back of the pilot's seat, and a new sight were installed. As a result, the aircraft weight increased and maximum speed decreased. The armament consisted of six 7.92 mm machine guns and a bomb rack for 50 kg bombs was installed under the wing behind each landing gear strut. 25 aircraft of series 106-130 were delivered to the Air Force during the war against the Soviet Union. From 1943 all aircraft armed with six 7.92 mm machine guns were designated IAR 80A.

Romanian pilots trained together with German pilots for Operation Barbarossa. On the eve of the attack, the 8th Air Group (the equivalent of a Soviet air regiment, only with three squadrons) was moved to the border airfields and began combat missions on June 22, 1941. The 8th Air Group was then joined by the 7th Air Group, and as part of the 4th Air Fleet of the Air Force, the Romanian pilots ensured the advance of the 3rd and 4th Romanian Armies, first on the territory of Bessarabia and then in the Ukraine. Covering the Romanian units, the fighters participated in the Battle of Stalingrad, but from January 1943 all the planes were concentrated on the air defense of Bucharest and the area of Ploesti, protecting the oil fields from raids.

IAR 80As of various series were in service until 1944 when they were universally replaced by more modern models.

1. Radu Brinzan "Iar.80 and Iar.81: Airframe, Systems and Equipment" 2011

2. A. Haustov. "Made in Romania Fighter IAR 80". Journal "Aviation and Time" № 6, 2002.

3. Materials of the site airwar.ru

Indicated stall speed in flight configuration: 154..162 km/h
Indicated stall speed in takeoff/landing configuration: 143..151 km/h
Dive speed limit: 750 km/h
Maximum load factor: 12 G
Stall angle of attack in flight configuration: 16,0°
Stall angle of attack in landing configuration: 13,8°
 
Maximum true air speed at sea level, engine mode - nominal: 433 km/h
Maximum true air speed at sea level, engine mode - emergency: 450 km/h
Maximum true air speed at 4700, engine mode - nominal m: 511 km/h
Maximum true air speed at 3800 m, engine mode - emergency: 514 km/h
 
Service ceiling: 10500 m
Climb rate at sea level: 14,1 m/s
Climb rate at 3000 m: 13,6 m/s
Climb rate at 6000 m: 9,7 m/s
 
Maximum performance turn at sea level: 17,8 s, at 300 km/h IAS.
 
Flight endurance at 3000 m: 1.9 h, at 350 km/h IAS.
 
Takeoff speed: 150...180 km/h
Glideslope speed: 200...220 km/h
Landing speed: 170...180 km/h
Landing angle: 14.2 °
 
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 mominal power, turn times are given for emergency power.
 
Engine:
Model: I.A.R. 14 K. IV. C-32
Maximum power in Emergency mode at sea level: 1050 HP
Maximum power in Emergency mode at 2700 m: 1100 HP
Maximum power in Nominal mode at sea level: 930 HP
Maximum power in Nominal mode at 3200 m: 1000 HP
 
Engine modes:
Nominal (unlimited time): 2300 RPM, 850 mm Hg
Emergency (up to 3 minutes): 2300 RPM, 935 mm Hg
 
Oil rated temperature in engine output: 40..110 °C
Oil maximum temperature in engine output: 120 °C
 
Empty weight: 1980 kg
Minimum weight (no ammo, 10% fuel): 2293 kg
Standard weight: 2650 kg
Maximum takeoff weight: 3030 kg
Fuel load: 324 kg / 450 l
Useful load: 1050 kg
 
Forward-firing armament:
6 x 7.92mm machine gun "FN Browning 7.92 mod 1938", 2400 rounds, 1500 rounds per minute, wing-mounted
 
or (modification):
4 x 7.92mm machine gun "FN Browning 7.92 mod 1938", 1600 rounds, 1500 rounds per minute, wing-mounted
2 x 13.2mm machine gun "FN Browning 13.2", 300 rounds, 1080 rounds per minute, wing-mounted
or (modification):
 
2 x 7.92mm machine gun "FN Browning 7.92 mod 1938", 1400 rounds, 1500 rounds per minute, wing-mounted
2 x 20mm gun "MG 151/20", 350 rounds, 700 rounds per minute, wing-mounted
 
Bombs (modification):
Up to 2 x 55 kg fragmentation bombs "SC 50"
249 kg general purpose bomb "SC 250"
 
Length: 8.9 m
Wingspan: 10.5 m
Wing surface: 16.1 m²
 
Combat debut: Summer-Autumn 1941
 
Operation features:
- The aircraft has no constant propeller governor. The propeller speed is controlled by manually changing the propeller pitch using a switch on the instrument board (default propeller pitch commands in the sim are [RShift + +/-]).
- Due to the absence of a constant propeller speed governor, it is necessary to carefully monitor the propeller RPM, especially in a dive - due to the spinning up of the propeller during acceleration, it is possible to exceed the maximum RPM and cause an engine failure.
- The aircraft has no cylinder head temperature gauge - only an oil temperature gauge.
- The oil radiator of the I.A.R. 80-A has no regulation (there is a second adjustable oil radiator on I.A.R. 80-M modification).
- The aircraft is equipped with elevator trimmer.
- Mixture control is automated, the automatic regulator maintains the set mixture composition and automatically enriches the mixture at low and full throttle. The optimum mixture is set by the centre position of the control lever.
- The flaps are hydraulic and can be set to any angle up to 60°. In the dive bomber version, the fully released flaps are used as air brake. There is no flap position indicator.
- The aircraft has differential pneumatic wheel brakes with shared control lever. This means that if the brake lever is held and the rudder pedal the opposite wheel brake is gradually released causing the plane to swing to one side or the other.
- The aircraft has a hydrostatic fuel gauge which shows total fuel remaining only when manual sucker lever is pushed in. In the sim, hold [RShift+I by default].
- To drop bombs, you must switch on the bomb releasel system first [N key]. After dropping bombs, the system should be manually deactivated.
- When the bomb release system is switched on, the flaps are automatically fully released as an air brake and retract automatically either when the bomb release button is pressed or when the system is switched off.
- The bomb release system can either drop only the central bomb or all three bombs at once.
- The gunsight is adjustable: both the target distance and target base can be set.
- In the dive bomber version, the tilt of the gunsight is adjustable [RAlt + F by default].
- The gunsight has a sliding sun-filter [LAlt + F by default].
- The canopy cannot be opened at speeds above 250 km/h, as it is clamped by the flow of incoming air. On version I.A.R. 80-M is equipped with an emergency pneumatic canopy opening system, which allows the canopy to open at higher speeds.
 
Basic data and recommended positions of the aircraft controls:
1. Starting the engine:
- recommended position of the mixture control lever: 50% auto mixture control
- recommended position of the cowl flap control handle: close
- recommended position of the prop pitch control handle: heavy
- recommended position of the throttle lever: 0%
 
2. Recommended mixture control lever positions for various flight modes: 50% (auto mixture control)
 
3. Recommended positions of the cowl flap control handle for various flight modes:
- takeoff: open 100%
- 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: 6.9 l/min
- Combat engine mode: 7.7 l/min
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