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configurations
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- HÜRKUS-A: Basic version which is to be certified with EASA according to CS-23 requirements.
- HÜRKUS-B: Advanced version with integrated avionics (including HUD, MFDs, and Mission Computer).
- HÜRKUS-C: Light Attack/ Armed Reconnaissance
- HÜRKUS-D: naval / coast guard maritime patrol variant, proposed
- Hurkus-C UAS : unmanned version being developed for the Turkish Armed Forces
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| Design Features |
- Superior aerodynamic performance, TAI designed wing airfoil
- 1,600 shp PT6A-68T Pratt & Whitney Canada turboprop engine
- Five bladed aluminum Hartzell HC-B5MA-3 propeller
- Martin-Baker Mk T-16 N 0/0 ejection seats
- Inverted Flight
- Good visibility from both cockpits, 50 down-view angle from rear cockpit
- Comfortable accommodation of wide range of pilot sizes
- Pressurized cockpit (nominal 4.16 psid)
- On-Board Oxygen Generating System (OBOGS)
- Anti-g System
- Environmental Control System (Vapor Cycle Cooling)
- Strengthened canopy for bird strike resistance
- High shock absorbing landing gears for training missions
- Hands On Throttle and Stick (HOTAS)
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| Length | 11.17 m (36 ft 8 in)
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| Wingspan | 9.96 m (32 ft 8 in)
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| Height | 3.70 m (12 ft 2 in)
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| Powerplant | 1 × Pratt & Whitney Canada PT6A-68T turboprop aircraft engine
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| Propellers | 5-bladed Hartzell Propeller HC-B5MA-3
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| Engine Power | 1,200 kW (1,600 shp)
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| Maximum Speed | 310 KCAS (574 km/h)
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| Cruise Speed | 250 kts
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| Stall Speed (landing configuration) | 77 KCAS (143 km/h)
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| G Limits | +7g / -3.5 g
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| Climb | 15000 ft in 5 min
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| Maximum rate of Climb (@ sea level) | 4370 ft/min (22 m/s)
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| Service Ceiling | 34700 ft (10577 m)
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| Maximum Endurance (@15,000 ft) | 4 h 15 min
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| Maximum Range (@15,000 ft) | 798 n mile (1478 km)
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| Total Take-Off Distance (@ sea level) | 1605 ft (489 m)
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| Total Landing Distance (@ sea level) | 1945 ft (593 m)
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| g limits | +7 / -3,5g
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| Armament |
Guns: 12.7mm and 20mm pods
Rockets: Roketsan Cirit, 2.75 inch rockets
Missiles: Roketsan UMTAS
Bombs: Mk-81, Mk-82, Tübitak SAGE HGK-3 (82), Tübitak SAGE KGK-82, BDU33 and MK106 training ordinance
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| Avionics |
Air data computer
Attitude and heading reference system
Emergency locator transmitter
GPS
Mode S transponder
Radar altimeter
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| Crew | one
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| Capacity | one passenger
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| Seating configuration | Stepped tandem
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| Pressurization | nominal 4.16 psid
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| Air | On-Board Oxygen Generating Systems (OBOGS)
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| Anti-G system | Yes
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| 0/0 Ejection seat | Martin-Baker Mk T-16 N 0/0 ejection seats
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