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$ 100,184
DynAero MCR-01 Sportster, certified in the VLA (Very Light Aircraft) Category
Details
- Year 2002
- TTAF 350
- Max Take Off Weight 490 kg
- Cabin Width 1.12 m
- Exterior Length 5.48 m
- Reg. Number French
- Condition Used
Description
Privately owned. Based in Bad-Ragaz Switzerland
Manufactured by the current owner with the manufacturer Dyn Aero in France between 1998 and 2002.
Final certification performed with Dyn Aero
VAT Payd in Switzerland
Motor, Rotax 912S
Power 100 hp
Max Engine RPM:
Take Off 5800 RPM
Maximum Continuous 5500 RPM
Constant Speed Propeller
Two Axis Autopilot
Garmin GPS 195 switched on autopilot
EFIS Elektronic Flight Instrument System, attitude indicator, altitude, speed, checklists, etc.
Filser Electronics COM
Filser Mode S Transponder
Hydraulic Brakes
Carburator Heat
Engine Adjustable Temperature Cowl Flaps
Fuel consumption: 240 km/h, 15-16 lt/hr
Wing Span 6.63 m
Wing Surface 5.2 m2
flaps -25 Degrees
Fuel Tank Capacity: 88 liters
Vne 173 kts
Vno 143 kts
Va 127 kts
Vfe 92 kts
Empty Weight: 259 kg
Max Engine RPM:
Take Off 5800 RPM
Maximum Continuous 5500 RPM
PERFORMANCES MOTEUR ROTAX 912S Puissance (hp) : 100 Croisière 75%, FL 0 (km/h) : 295 Croisière 75%, FL 80 (km/h) : 318 Consommation à 75% (litres/h) : 21.3 Rayon d’action, rés. std 75% (km) : 1 194 Croisière 65% FL110 (km/h) : 312 Consommation à 65% (litres/h) : 18.5 Rayon d’action, rés.std, 65% (km) : 1 375 Dist.de décollage, hélice à PV (m) : 152 Taux de montée, FL 0, PV (ft/min) : 1 750
Note: It is possible to install a Balistic Recovery System (Parachute)
Additonal cost, around Euro 12'00-16'000. Additonal weight: 10-12 kg
NOT INCLUDED IN THE SALE.
Specifications subject to verification
Listed price
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