GT 400

Specifications:

 POWERPLANT
Model ROTAX 503 w/Gear drive
No. Cylinders 2
Displacement 496.7 cc
Horsepower 50 hp
Recommended TBO 300 hrs
Propeller 68" x 32"
Fuel Capacity 5 gal
 AIRFRAME                                        R503
Length 19ft 9in
Height. 6' 6"
Wingspan 30ft
Wing area 146 sq ft
Wing loading 3.9 lb/sq ft
Power loading 11.4 lb/hp
Seats 1
Minimum flight crew 1
 WEIGHTS
Max takeoff weight 570 lbs
Empty weight 316 lbs
Useful load 254 lbs
Payload w/full fuel 224 lbs
 PERFORMANCE
Takeoff distance, ground roll 65 ft
Takeoff distance, 50 ft obstacle 169 ft
Rate of climb 1450 ft/min
Max level speed, sea level 78 mph
Landing distance, 50 ft obstacle 350 ft
Landing distance, ground roll 100 ft
Glide Ratio 7.5:1
Minimum sink rate 450 ft/min
 
 CRUISE PERFORMANCE CHART:
At 55% power (rpm/mph) 5300/64
At 65% power (rpm/mph) 5600/68
At 75% power (rpm/mph) 5900/72
At 100% power (rpm/mph 6500/78
 FUEL FLOW
At 55% power (gph/mi) 3.67/87
At 65% power (gph/mi) 4.33/79
At 75% power (gph/mi) 5.00/72
At 100% power (gph/mi) 6.67/58
 AIRSPEEDS
Vx (Best angle of climb) 32 mph
Vy (Best rate of climb) 41 mph
Va (Design maneuvering) 61 mph
Vne (Never exceed) 74 mph
Vs1 (Stall, flaps up, power off) 29 mph
Vs0 (Stall, flaps down, power off ) 27 mph
Landing approach speed 40 mph






Features

  • Limited Warranty (see your dealer for details)
  • Spring loaded landing gear, steerable Nose Wheel 4
  • position flaps
  • State-of-the-art landing gear suspension
  • Virtually vibration-free engine mount
  • Lowest cockpit noise level of all ultralights tested
  • 65 mph cruise
  • Tapered wing
  • Short take-off & landing
 


  • Airspeed indicator
  • 30 minute set-up and breakdown
  • Adjustable pilot seat
  • Removable 5 gallon fuel tank
  • Extraordinary visibility
  • Delivered in easy-to-assemble kit (dealer assembly service
  • available at participating dealers)
  • Easy maintenance and repair
  • Wide range of option

NOTE: All specifications are based on manufacturer's calculations.
All performance figures are based on standard day, standard atmosphere, at sea level and 175 lb.
pilot weight, unless otherwise noted. Flight training required. Specifications subject to change without notice. The
empty weight is shown with allowance made for pilot/vehicle recovery system deducted. The empty weight for all
models is approximate due to a 4% MIL SPEC tolerance on materials.
SPECIFICATIONS SUBJECT TO CHANGE WITHOUT NOTICE.
This information is for reference only, please consult Quicksilver or one of it’s dealers for exact and up to date
specifications.


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