Aero-AT3-R100

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Price: Negotiable
Delivery Date: Within 3 days after your order is confirmed.
Place Of Origin France
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  • Description
  • Powered by
    Engine .............................................................................................................................................................................................. Rotax 912 S
    Power ............................................................................................................................................................................................... 100 hp
    Propeller ...................................................................................................................................................................................... 3 blade ELPROP ground adjustable carbon
    ...........................................................................................................................................................................................................................composite aero-elastic propeller
    TBO ....................................................................................................................................................................................................... 2000h
     
    Weights
    Mallowable weight- .................................................................................................................................................. 582 kg / 1282 lb
    MTOW
    Emty weight............................................................................................................................................................................. 360 kg / 794 lb
    Useful load ............................................................................................................................................................................... 222 kg / 485lb
     
    Fuel capacity .......................................................................................................................................................................... 65L / 18.5 gal
     
    Dimensions
    Wing area .................................................................................................................................................................................. 9,3 m2 / 100,6 ft2
    Wing span .................................................................................................................................................................................. 7,552m / 24.77 ft
    Length ................................................................................................................................................................................................. 5,880m / 19.29 ft
    Height ................................................................................................................................................................................................. 2,230m / 7,31 ft
     
    Performance
    Cruising speed ..................................................................................................................................................................... 200km/h / 108 kts IAS
    Max cruising speed ...................................................................................................................................................... 220km/h / 119 kts IAS
    VNE never exceed speed .................................................................................................................................... 236km/h / 127 kts IAS
    VA maneuvering speed .......................................................................................................................................... 208km/h / 112 kts IAS
    VS stall speed ........................................................................................................................................................................ 82km/h / 44 kts CAS
     
    Take-off/ landing distance.................................................................................................................................. 145/200m / 476/656 feet
    Take-off/ landing distance (over 50'/15m)............................................................................... 275/450m / 902/1476 feet
    Rate of climb ......................................................................................................................................................................... .4.6m/s / 906 fpm
    Range .................................................................................................................................................................................................717km / 387nm
    Celling ............................................................................................................................................................................................... .4000m / 13123 ft
    Designed load factor ................................................................................................................................................. +3,8/-1,5 g
    Power loading ....................................................................................................................................................................... 5.82kg/hp / 12.82 lb/hp
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