Pioneer 300 Hawk (Retract)
The Pioneer 300 Hawk is a wonderful aircraft built for the more discerning pilot, featuring retractable undercarriage, with performances that will surprise you!
Details of Pioneer 300 Hawk
Available as kitsets that are built to two different stages depending on the builders experience.
Standard Equipment:
Rotax ULS2 100 Hp engine with airbox
P300 Coverred "S" wing
40 lt wing fuel tanks
Andair fuel selector
Fiber panel and consolle
Cabin fresh air intake
Key canopy lock
Aileron electric trim
Elevator electric trim
Electric flaps
Electronic flaps controller
Electric retractable gear
Gas nose landing gear
Gas main landing gear
Landing gear doors
UK cloche
UK pedals
Luxury upholstery
Plus cabin heating
3 points safety belt
Oil inspection door
Landing lights inserted in cowling
Strobe and nav lights
Radio prewiring
Auxiliary electric socket
White paint with sticker livery
Pioneer canopy cover
Flight and maintenance manual - check list
Tools
Standard Instruments:
Speedmeter
Altimeter
CSI
Bank indicator
Compass
Fuel press indicator
2 fuel level indicators
2 x EGT
Oil temp indicator
Oil press indicator
Airbox temp indicator + O.A.T.
Voltmeter
Ampermeter
Fuel computer
Specifications:
| Engine power | 100Hp (variable pitch propeller) |
| DIMENSIONS | |
| Wing span | 7.55 m ala S/S wing (* 8.10 m ala N/N wing) |
| Wing area | 10.5 mq (11mq) |
| Length | 6.25 m |
| Cabin width | 1.05 m |
| WEIGHTS | |
| Empty weight (without parachute) | 285 kg |
| Max take off weight (ULM) | 450 kg |
| Max weight (VLA) | 560 kg |
| LOADS | |
| In flight load factor | +3.8/-1.9 g @ 560 kg |
| Tank capacity | 80 l |
| Installable auxiliary tank capacity | 32 l |
| Overall payload limit (VLA) | 275 kg |
| Baggage volume | 226 l |
| Max baggage load | 20 kg |
| PERFORMANCE | |
| Maximum level speed | 280 km/h (270 km/h) |
| Cruise speed (@75% power) | 250 km/h (240 km/h) |
| Stall speed | 65 km/h |
| Best climb rate speed | 120 km/h |
| Best climb angle speed | 100 km/h |
| Best rate of clime | 455 m/min (1500 ft/min) |
| Roll rate | 90°/sec |
| Aerodynamic efficiency | 13:1 |
| Range (@75% power) | 1000 km |
| Range with auxiliary tank (@75% power) | 1400 km |
| Fuel consumption (@75% power) | 18.5 l/h |
| Service Ceiling | 6000 m |
| Take off distance | 120 m |
| Landing distance | 120 m |
