Aircraft Specifications
ROTAX 912 A  (or 912 UL)
  • Airframe                      All-metal construction
  • Wingspan                   28'6"
  • Fuselage length         18'0"
  • Wing area                  92.5 sq.ft
  • Gross weight              1168 lbs
  • Empty weight              727 lbs
  • Wing loading              12.6 lbs/sq.ft
  • Power loading            14.6 lbs/hp
  • Engine                        80 hp
  • Fuel tank capacity      13.1 US gallons,
                                  
DATA
PERFORMANCE
  • VNE                                                                134 kts IAS
  • Maximum level speed ISA Sea Level               104 kts TAS
  • Cruising speed, 75%                                       95 kts TAS
  • Stall speed clean max. weight                          45 kts CAS
  • Roll rate 60 kts with 40º Flaps                          30º/sec
  • Rate of climb, max. weight                                650ft/min
  • TO Dist to 50ft ISA sea level, max. weight        <1614 ft
  • Ground roll                                                       <892 ft
  • Load factor flaps up                                       +3.8g -1.5g
  • Useful load                                                        441 lbs
  • Estimated fuel consumption                              4.5 US gallons/h