Tactical aircraft with
comprehensive training capability
With over 30 years of service, this aircraft combines efficiency, low operating costs, and cutting-edge technology: digital avionics, radar simulation, virtual scenarios, data link, and a modern, fuel-efficient engine. Its versatility and reliability position it as a highly competitive solution in the military training segment.
TECHNICAL SPECIFICATIONS
With more than 30 years of proven service, it combines efficient aerodynamics, state-of-the-art digital avionics, and a low-consumption turbofan engine. This configuration allows it to fulfill basic-advanced training missions and light attack tactical operations, both day and night, with high productivity.
It maintains a proven design with a robust structure, reliable systems, and power-assisted flight controls, ensuring ease of maintenance and a competitive operating cost. Its tandem pressurized cockpit incorporates a Full Glass Cockpit compatible with NVG (Night Vision Goggles) and 0/0 ejection seats. The system is complemented by integrated logistical support (ILS/CLS) and ground-based training (ITS) solutions, including simulators and procedures trainers, providing a flexible, effective, and sustainable platform throughout a life cycle exceeding 40 years.
It features modern integrated avionics, virtual training systems with radar simulation, tactical scenarios, and data link. Its open and modular architecture allows for flexible and scalable configurations according to training or combat needs, offering an efficient and versatile solution comparable to modern fighter jets.
Piloting
Contact / Aerobatics.
Instrument Flight / Formation.
Day / Night.
Tactical
Basic, Advanced, and BVR (Beyond Visual Range) Air-to-Air combat.
Air-to-Ground missions (Tactical navigation, CAS, etc.).
Virtual / Live Weapon Delivery.
Light Attack
Air-to-Air / Air-to-Ground missions.
Interception of low-performance aircraft.
Counter-narcotics operations.
Five hardpoints (1760 STD NATO Pylons) *Optional.
Characteristics
| Honeywell, TFE 731-40-2N | Turbofan Engine |
| Empuje Max (ISA, SL) | 1,820 kg - 4,000 lb |
| Empuje Max (Uso) | Sin lim. / Put and Forget |
| TSFC | (0,46 Lb./ Lb./ h) |
| TOW (Entrenador) | 3,890 kg - 8,570 lb |
| MTOW (Máximo de despegue) | 5,000 kg - 11,040 lb |
| WF (Combustible máximo interno) | 1,380 lit |
| Cargas externas (Máximo) | 1,200 kg - 2,650 lb |
| V máxima Nivelado (SL/ 28.000 ft) | 430/ 470 KTAS |
| V máxima Operativa KEAS/ M | 480/ 0.8 |
| V perdida- Flaps- Configuración Aterrizaje | 85 KEAS |
| V ascenso (ISA- SL) | 6,050 ft/min |
| Alcance (Comb Max. Int, 30' reserv) | 1,270 nm |
| Autonomía (Comb Max Int, 30' reserv) | 5 Hr |
| Techo de servicio | 42,300 ft |
| Máximo G viraje sostenido (SL) | 5 g |
