- Yes
- No
ENAER A-36 Toquí
History:
The operational life of the A-36 (C-101 Aviojet) begins in 1982 when the training version called T-36BB Halcón is used. Subsequently, in 1984, a co-production agreement was signed between the companies CASA (Spanish) and Enaer (Chilean) which allowed Enaer to obtain the license for the development and assembly of said aircraft. In Chile, the C-101BB Halcón version was assembled, which had a more powerful engine with 3,700 pounds of thrust. Subsequently, the Chilean Air Force asked the company for an improved version of the aircraft, which resulted in the A-36CC Halcón with a new 4,300-pound-thrust Garrett TFE731-5-1J powerplant. This version can perform ground attack missions, reconnaissance, escort, armed training, etc, they were also provided with British Aerospace Sea Eagle anti-ship missiles, being successfully tested, but since the Navy integrated helicopters with Exocet missiles, it was decided to maintain the helicopters armament to avoid duplication of services.
Sea Eagle anti-ship missiles
The birth of the Chilean Toquí
In the mid-90s in Chile, the new modernization of the A-36 Halcón began, which consisted of 4 important improvements, being the implementation of HOTAS for the pilot, integration of a navigation system and a SAGEM brand attack system, for planning of flight missions and weapons handling, and the adoption of the Ferranti brand HUD for the presentation of data on the Head-Up Display, together with these new capabilities at the avionics level, integrated within its possibilities the Israeli Shafrir II air-to-air missile firing. All these works resulted in the A-36 Toqui (Halcón II), a unique model in the world, being officially presented at the ENAER premises on November 26, 1997. They were finally decommissioned in 2022 with 40 years of service, being a icon in the Chilean Aviation since it was one of the few models that were produced and totally improved in Chile.
Specifications:
- Crew:
- 2
- Armament:
- Primary: 1x DEFA 553 30 mm cannon and 130 shots in a gondola located in the ventral part of the aircraft
- Secondary: Warload - 2250 kg in 6 hardpoints:
- Bombs: 500-kg bombs, 375-kg bombs, 250-kg bombs, CB-500-K cluster bombs, napalm bombs BLU-27
- Rockets: LAU-10 with 4 Zuni rockets, LAU-3/A with 19 FFAAR mighty mouse rockets, Matra 155 18x68-mm
- Missiles: AIM-9 Sidewinder, ASM-65A Maverick, Shafrir II, Matra Magic 2, Anti-ship missile Sea Eagle.
- Additional systems: HOTAS, Navigation system and another attack system brand SAGEM, HUD of the Ferranti brand, Small rangefinder radar.
- Dimensions:
- Length: 12.50 m
- Wingspan: 10.6 m
- Height: 4.25 m
- Wings area: 20.00 m²
- Weight empty: 3500 kg
- Weight normal take-off: 5000 kg
- Weight maximum take-off: 6300 kg
- Weight Internal fuel: 1822 kg
- Performance:
- Powerplant: 1 TJE Garrett TFE731-5-1J, 4,300-pound-thrust
- Maximum speed: in altitude 834 km/h, on sea level 769 km/h
- Cruising speed: 656 km/h
- Range: 3706 km
- Combat radius: 370-964 km
- Rate of climb: 1859 m/min
- Service ceiling: 12800 m
- Maximum overload: 7.5
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