- All-Composite,
modern, two-seat trainer aircraft designed by NAL and type-certified
by the Director General of Civil Aviation of India
- Neat
cockpit with every good visibility
- Dual
controls with excellent control harmony
- Turbo-charged
engine with constant speed propeller
- Rugged,
operationally cost-effective and easy to maintain
- Extensively
tested for certification compliance, including lighting
protection
- Ideally
suited for pilot training, sports,and hobby flying. The
aircraft could also be developed for surveillance, aerial
photography, coast guard and environment monitoring roles
- Day-night
flying capability
- Fully
certified by DGCA under FAR-23 via JAR-VLA for day/night
operations
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SPECIFICATIONS
Power
Plant
Rotax
914 F3 turbo-charged engine with 100BHP at 5500 RPM Max. continuous
and 115 BHP at 5800 RPM.
Propeller
Variable pitch 170 cm (67") Hoffmann propeller
Performance
(ISA sea level)
Max.
Cruise speed - 93 kias
Max.
Rate of climb - 650 ft/min
Endurance - 4h
Stall speed with flaps 20° - 43 kias
Take-off (over 15m height) - 450m
Landing (over 15m height) - 600m
Geometry
Wing span - 10.47 m
Wing area - 12.47 m²
Length - 7.658 m
Height - 2.614 m
Cabin width - 107 cm
Weight
Empty weight (night operations with lightning protection)
- 545 kg
All-up weight - 750 kg
Useful load - 205 kg
Fuel capacity - 85 ltr
Instruments
/ Avionics
Day Operations Airspeed Indicator, Altimeter,
Vertical Speed Indicator, Outside Air Temperature, Magnetic
Compass, Slip/Skid Indicator, NAV/COMM, Intercom, Emergency
Locator Transmitter (ELT), Voltameter and Indicators for RPM,
Manifold Pressure, Oil Pressure, Oil Temperature and Cylinder
Head Temperature.
Night
Operations Additionally :
Artificial Horizon, Directional Gyro, Turn
Co-ordinator, Navigation Lights, Landing Lights, Anti-Collision
Lights, Panel Lights and Map Lights.
Optional GPS
Electrical system 14 VDC
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