Flat Wing Aspect Ratio
5.6
Entry Into service
1980-03-17
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All data (28 fields)
- Name
- CASA C-101 Aviojet
- Manufacturer
- Construcciones Aeronauticas
- Description
- The CASA C-101 Aviojet is a low-wing single engine jet-powered advanced trainer and light attack aircraft designed and manufactured by Spanish aircraft company Construcciones Aeronáuticas SA (CASA).
- ICAO Code
- C101
- First Flight
- 1977-06-27
- Entry Into service
- 1980-03-17
- Service End
- 2025-01-01
- Designer
- Construcciones Aeronauticas
- Type
- Advanced jet trainer and light attack aircraft
- Length (m)
- 12.5
- Height (m)
- 4.25
- Cockpit Crew
- 2
- Max Speed (km/h)
- 769
- Cruise Speed (km/h)
- 656
- Min Speed (km/h)
- 183
- Max Ceiling (m)
- 12800
- Rate of Climb (m/s)
- 24.9
- Armament
- :* 1 × 30 mm DEFA cannon :or :* 2 × 12.7 mm M3 machine guns in detachable pods underneath the forward fuselage; :* Up to 2220 kg disposable stores on 6 underwing pylons; :* 2 – Rafael Shafrir (A-36 "Toqui") air-to-air missiles
- Endurance (h)
- 30
- Number Built
- 166
- Powerplant Description
- 1 × Honeywell TFE731-5-1J turbofan engine, 19.13 kN thrust each
- Primary Users
- Spanish Air and Space Force, Chilean Air Force , Honduran Air Force , Royal Jordanian Air Force
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/CASA_C-101_Aviojet
- Flat Wing Span (m)
- 10.6
- Flat Wing Area (m²)
- 20
- Flat Wing Aspect Ratio
- 5.6
- Wake Category
- L
- Number of Engines
- 1