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Aviation
IAR-93B
VI
Rank
AB
9.0
RB
9.0
SB
9.0
AB
RB
9.3
SB
9.3
AB
9.3
RB
9.3
SB
Battle rating
Italy
Research country
Strike aircraft
Main role
Romania
Operator
General information

In the late 1960s, Romania and Yugoslavia considered jointly developing a subsonic, multipurpose attack aircraft capable of intercepting low-flying targets. The aircraft's requirements were strict: it had to be simple and made from local components. It also had to be capable of landing on unprepared airfields, reliable, and easy to maintain. On May 20, 1971, the two countries signed a joint development agreement. Both the Romanian and Yugoslav prototypes made their first flight on October 31, 1974. Series production of the IAR-93 began in 1976 at the Avioane Craiova plant in Romania. A two-seater prototype took to the skies on January 23, 1977, but it was lost on November 24. Three aircraft were unveiled to the public on August 23, 1979.

The first production modification was the IAR-93A, which consisted of 15 pre-production and 18 production aircraft. This was followed by the IAR 93B, which featured a new wing, additional attachment points, enlarged fuel tanks, and improved aerodynamics. A total of 27 single-seat and seven two-seat aircraft were built. The aircraft remained in service until 1998, when the conflict in Yugoslavia made maintenance impossible.

The Romanian IAR-93B was introduced as a reward for the 2024 "Flight of the Vulture" event as part of the Revenue Share program in the Italian air research tree. This excellent attack aircraft is equipped with a ballistic computer, RWR, and air-to-air missiles for self-defense in close combat. Its good maneuverability is also nice to have. However, it lacks countermeasures and is usually slower than other jets.


Where to purchase

Flight performance
Max speed
at 0 m 1,1091,0871,1221,095 km/h
Rate of Climb 6546.479.651.6 m/s
Turn time 2729.525.928.2 s
Max altitude 13,000 m
Takeoff Run 900 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 1 person
Engine
Length 13.2 m
Wingspan 9.4 m
Wing Loading 322 kg/m²

Weight:
Base weight 5.896.085.736.05 t
Fuel in main tanks 2.5 t (40m)
Fuel in drop tanks 0.43 t (7m)

Limits:
Max Speed Limit (IAS) 1,155 km/h
Mach Number Limit 1.09 M
G limit ≈ -5/9 G
Flap Speed Limit (IAS) 400 km/h
Gear Speed Limit (IAS) 475 km/h
Offensive armament
2 × 23 mm GSh-23L cannon
Ammunition 400 rounds
Fire rate 3,396 shots/min
One-second Burst Mass 9.9 kg

BeltBelt fillingArmor penetration (mm) at a distance:
10 m100 m500 m1000 m1500 m2000 m
HEFI-T/AP-I/HEF-I31292115107
HEF-I/AP-I/AP-I/AP-I31292115107
HEFI-T/HEF-I/HEFI-T/HEF-I/AP-I31292115107
AP-I/HEF-I/HEF-I31292115107
Suspended armament
Max weight 7,711 kg
Wing loading left / right
Maximum 3,855 kg
Max. difference 1,900 kg

NameWeightSlot
75.3 kg
16 × 110.2 kg
32 × 225.5 kg
235 kg
2 × 131.4 kg
3 × 225 kg
3 × 402 kg
250 kg
508.3 kg
Drop tank (540 liters.)145 kg
Economy
Repair cost Basic → Reference
AB 2,730 → 4,114 SL
RB 7,908 → 11,917 SL
SB 9,131 → 13,760 SL
Crew training 150,000 SL
Experts 520,000 SL
Aces 2,400 GE
Research Aces 950,000 RP
Reward multiplier AB / RB / SB
120 / 330 / 600 % SL
220 % RP
Total cost of modifications 167,600 RP
261,000 SL
Talisman cost 2,600 GE

Flight performance
Survivability
Weaponry
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