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| Quicksilver GT 400 |
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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. |
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
For pricing information contact sales@fpna.com |
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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 |
Rotax 447 w/Gear Drive |
Rotax 503 w/Gear Drive |
| Powerplant |
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| Model |
52hp Rotax-503 |
52hp Rotax-503 |
| No. Cylinders |
2 |
2 |
| Displacement |
436.6 cc |
496.7 cc |
| Horsepower |
40 hp |
50 hp |
| Recommended TBO |
250 hrs |
250 hrs |
| Propeller |
68" x 32" |
68" x 32" |
| Fuel capacity |
5 gals |
5 gals |
| Configuration with Strut Braced Wing |
| Airframe |
R447 |
R503 |
| Length |
237 in. |
238 in |
| Height |
78 in |
78 in |
| Wingspan |
30 ft |
30 ft |
| Wing area |
146 sq ft |
146 sq ft |
| Wing loading |
3.9 lb/sq ft |
3.9 lb/sq ft |
| Power loading |
14.25 lb/hp |
11.4 lb/hp |
| Seats |
1 |
1 |
| Minimum flight crew |
1 |
1 |
| Weights |
| Empty Weight |
276 lbs |
306 lbs |
| Useful load |
294 lbs |
264 lbs |
| Payload w/full fuel |
264 lbs |
234 lbs |
| Max takeoff weight |
570 lbs |
570 lbs |
| Performance |
| Takeoff distance, ground roll |
75 ft |
65 ft |
| Takeoff distance, 50 ft obstacle |
215 ft |
169 ft |
| Rate of climb |
1000 fpm |
1450 fpm |
| Max level speed, sea level |
61 mph |
78 mph |
| Landing distance, 50 ft obstacle |
350 ft |
350 ft |
| Landing distance, ground roll |
100 ft |
100 ft |
| Glide Ratio |
7:1 |
7.5:1 |
| Minimum sink rate |
450 fpm |
450 fpm |
| Cruise Performance |
| At 55% power (rpm/mph) |
5300/51 |
5300/64 |
| At 65% power (rpm/mph) |
5600/55 |
5600/68 |
| At 75% power (rpm/mph) |
5900/58 |
5900/72 |
| At 100% power (rpm/mph) |
6500/61 |
6500/78 |
| Fuel Flow |
| At 55% power (gph/mi) |
3.0/85 |
3.67/87 |
| At 65% power (gph/mi) |
3.5/78 |
4.33/79 |
| At 75% power (gph/mi) |
4.0/72 |
5.00/72 |
| At 100% power (gph/mi) |
4.5/67 |
6.67/58 |
| Air Speeds |
| Vx (Best angle of climb) |
32 mph |
32 mph |
| Vy (Best rate of climb) |
41 mph |
41 mph |
| Va (Design maneuvering) |
61 mph |
61 mph |
| Vne (Never exceed) |
74 mph |
74 mph |
| Vs1 (Stall, power off) |
29 mph |
29 mph |
| Vs0 (Stall, flaps down, power off) |
27 mph |
27 mph |
| Landing approach speed |
40 mph |
40 mph |
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For information contact sales@fpna.com
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