| Powerplant / Airframe |
|
| Lycoming 0-235-L2A engine, 118 hp at 2800 rpm
|
|
| Sensenich propeller, fixed pitch, 1m83 |
| Dry battery 12V / 24 A/h with external pozer plug |
| Semi-monocoque aluminium alloy structure, anti-corrosion
treated |
| Forward sliding bubble-canopy |
| Quickly removable engine cowlings |
| Long-stroke, oleo-pneumatic damped landing gear |
| Hydraulic Cleveland disk brakes |
| Steerable nose wheel, auto centering in flight |
| 120 liters / 31.7 US Gal fuel bank, with dipstick |
| Wing mounted taxi / landing lights |
| Two-color paint scheme, on white overall polyurethane
paint |
| |
| Cockpit accommodation |
|
| Bucket-seats, adjustable fore-and-aft in 6 different
positions, with 4-strap safety harness |
|
| Vinyl and fabric upholstrery |
|
| Dual stick flight controls |
|
| Dual left-hand throttle controls |
|
| Pilot's and co-pilot's toe-brakes |
|
| Electrical flaps control, with 3 pre-selected
positions |
|
| |
| Basic equipment |
|
| Airspeed indicator (dual scale km/h - kt)
|
|
| Altimeter (sensitive, ft - mb) |
|
| Rate of climb indicator (ft - mb) |
|
| Magnetic compass |
|
| Tachometer |
|
| Oil pressure & temperatures gauges |
|
| Fuel pressure gauge |
|
| Fuel quantity gauge |
|
| Flight-time recorder |
|
| Annunciator panel, 8 warming lights |
|
| Horizon & Directional gyro, on vacuum pump |
|
| Turn coordinator, electrical |
|
| Navigation lights |
|
| Taxi & landing lights |
|
| Anti-collision strobe light (on fuselage top) |
|
| Instrument panel lighting, with dimmer |
|
| Four individual mike-and-headset jack sockets |
|
| Push-to-talk button on each stick |
|
| |
| Avionics (to customer's
requests), Typical equipment : |
|
| COM / NAV King KX 155, VOR / LOC KI 208 indicator
|
|
| Garmin 150 XL GPS, King KT 76C Tansponder |
|
| ACK 30 Alticoder, SPA 400 intercom system |
|
| |
| Options |
|
| Exhaust gas temperature indicator |
|
| Carburetor air temperature indicator |
|
| Cylinder head temperature indicator |
|
| Outside air temperature indicator |
|
| Pilot heating |
|
| |
|
| |
| |
|
