GT400

Quicksilver Aircraft.

GWS IS YOUR BEST RESOURCE FOR QUICKSILVER IN TAIWAN

The GT 400 Spring loaded steerable nose wheel * four position flaps * state-of-the-art landing gear suspension * virtually vibration-free engine mount * lowest cockpit noise level of all ultralights tested * 58 mph cruise * tapered wing * short take-off and landing * airspeed indicator * quick set-up and breakdown * adjustable pilot seat * extraordinary visibility * delivered in easy-to-assemble-kit * optional 50 hp 503 Rotax engine.

NOTE : DYE LOTS MAY VARY

FEATURES

Limited Warranty (see your dealer for details)
Spring loaded, 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
72 mph cruise
Tapered wing
Short take-off & landing
Airspeed indicator
15 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 maiintenance and repair
Wide range of options

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:

Powerplant.....ROTAX 447 w/Gear drive
No. Cylinders...........................................2
Displacement..............................436.6 cc
Horsepower......................................40 hp
Recommended TBO.....................250 hrs
Propeller......................................60" x 32"
Fuel Capacity.....................................5 gal

Kit Cost: ...............Contact dealer for price

SPECIFICATIONS:

Powerplant.....ROTAX 503 w/Gear drive
No. Cylinders............................................2
Displacement...............................496.7 cc
Horsepower........................................50 hp
Recommended TBO......................250 hrs
Propeller........................................68" x 32"
Fuel Capacity.......................................5 gal

Kit Cost: ...............Contact dealer for price

STANDARD CONFIGURATION-STRUT BRACED WING

AIRFRAME
Length........................................................
Height........................................................
Wingspan..................................................
Wing area.................................................
Wing loading............................................
Power loading..........................................
Seats.........................................................
Minimum flight crew.................................

WEIGHTS:
Max takeoff weight..................................
Empty weight...........................................
Useful load...............................................
Payload w/full fuel....................................

PERFORMANCE:
Takeoff distance, ground roll..................
Takeoff distance, 50 ft obstacle.............
Rate of climb............................................
Max level speed, sea level......................
Landing distance, 50 ft obstacle............
Landing distance, ground roll.................
Glide Ratio...............................................
Minimum sink rate....................................

CRUISE PERFORMANCE CHART:
At 55% power (rpm/mph)........................
At 65% power (rpm/mph)........................
At 75% power (rpm/mph)........................
At 100% power (rpm/mph)......................

FUEL FLOW:
At 55% power (gpm/mi)..........................
At 65% power (gpm/mi)..........................
At 75% power (gpm/mi)..........................
At 100% power (gpm/mi)........................

AIRSPEEDS:
V_x (Best angle of climb)..........................
V_y (Best rate of climb).............................
V_a (Design maneuvering).......................
V_ne (Never exceed).................................
V_s1 (Stall, power off)................................
V_s0 (Stall, flaps down, power off)...........
Landing approach speed ......................

R447
237 in.
78 in.
30 ft
146 sq ft
3.9 lb/sq ft
14.25 lb/hp
1
1

570 lbs
276 lbs
294 lbs
264 lbs

75 ft
215 ft
1000 fpm
61 mph
350 ft
100 ft
7:1
450 fpm

5300/51
5600/55
5900/58
6500/61

3.0/85
3.5/78
4.0/72
4.5/67

_{-32 mph}
_{-41 mph}
_{-61 mph}
_{-74 mph}
_{-29 mph}
_{-27 mph}
_{-40 mph}

OPTIONAL CONFIGURATION-STRUT BRACED WING

WEIGHTS:
Max takeoff weight...................................
Empty weight............................................
Useful load................................................
Payload w/full fuel.....................................

PERFORMANCE:
Takeoff distance, ground roll..................
Takeoff distance, 50 ft obstacle.............
Rate of climb............................................
Max level speed, sea level......................
Landing distance, 50 ft obstacle............
Landing distance, ground roll..................
Glide Ratio...............................................
Minimum sink rate....................................

CRUISE PERFORMANCE CHART:
At 55% power (rpm/mph).........................
At 65% power (rpm/mph).........................
At 75% power (rpm/mph).........................
At 100% power (rpm/mph).......................

FUEL FLOW:
At 55% power (gph/mi)..........................
At 65% power (gph/mi)..........................
At 75% power (gph/mi)..........................
At 100% power (gph/mi)........................

AIRSPEEDS:
V_x (Best angle of climb)...........................
V_y (Best rate of climb)..............................
V_a (Design maneuvering).........................
V_ne (Never exceed)...................................
V_s1 (Stall, power off).................................
V_s0 (Stall, flaps down, power off)............
Landing approach speed.........................

R503
238 in
78 in
30 ft
146 sq ft
3.9 lb/sq ft
11.4 lb/hp
1
1

570 lbs
306 lbs
264 lbs
234 lbs

65 ft
169 ft
1450 fpm
78 mph
350 ft
100 ft
7.5:1
450 fpm

5300/64
5600/68
5900/72
6500/78

3.67/87
4.33/79
5.00/72
6.67/58

_{-32 mph}
_{-41 mph}
_{-61 mph}
_{-74 mph}
_{-29 mph}
_{-27 mph}
_{40 mph}

The GT 400 Special

The GT 400 Special Edition Spring loaded steerable nose wheel * four position flaps * state-of-the-art landing gear suspension * virtually vibration-free engine mount * GT 400 R447B kit * Small Nose Fairing and Windshield * tapered wing * short take-off and landing * airspeed indicator * quick set-up and breakdown * adjustable pilot seat * extraordinary visibility * delivered in easy-to-assemble-kit

Description
Gt 400 R447B kit
Small Nose Fairing & Windshield

Limited Edition Special Price

Contact dealer for price

The GT 400 is quite possibly the finest ultrlight type aircraft ever designed.
Ask anyone whose flown one. GT 400 owners luv'em. It was the first and only
certified ultralight type one seat aircraft in the USA. Its true assembly style kit,
outstanding flying characteristics and exceptional quality have put the GT 400
in a class by itself. Try it and you will know why.

Custom colors, stripes and wheel pants optional

GT400 LE

FEATURES

Limited Warranty (see your dealer for details)
Spring loaded, 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
58 mph cruise
Tapered wing
Short take-off & landing
Airspeed indicator
15 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 maiintenance and repair
Wide range of options

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.

STANDARD CONFIGURATION-STRUT BRACED WING

R447
237 in.
78 in.
30 ft
146 sq ft
3.9 lb/sq ft
14.25 lb/hp
1
1

570 lbs
276 lbs
294 lbs
264 lbs

75 ft
215 ft
1000 fpm
61 mph
350 ft
100 ft
7:1
450 fpm

5300/51
5600/55
5900/58
6500/61

3.0/85
3.5/78
4.0/72
4.5/67

_{-32 mph}
_{-41 mph}
_{-61 mph}
_{-74 mph}
_{-29 mph}
_{-27 mph}
_{-40 mph}

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