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THE HAWK CLASS, THE FOCUS POINT
Derived from the Pioneer 300 standard, it’s a natural Pioneer’s aircraft evolution. The aircraft, maintaining all the good P300 flight qualities, is equipped with very good quality & luxury interiors.

The wing skin is fully made of plywood and is now working with respect to the flight loads, the retractable landing gear is equipped with a gas-oil damper system giving a surprising taxing, take-off and landing comfort.
The aircraft is equipped with the new higher and aerodynamic canopy, updated to offer a good cockpit comfort also to the tall pilot. The instrument panel, that is now made of composite materials, has a three dimensional shape to improve the instrument visual and the interiors look.
 
Descriptions
 
  • Low wing.
  • Tricycle retractable landing gear with oil-air shock absorbers.
  • Electrical landing gear retraction with manual emergency actuation.
  • Stearable nose landing gear.
  • Landing gear vane fairings.
  • 2 place, side by side arrangements with double control stick.
  • Tractive propeller.
  • Mixed composite material and wood structure.
  • Detachable fully plywood covered wings.
  • Three axis trim system.
  • Well finished and comfortable interiors, car quality standards.
  • Ergonomic seats.
  • Composite material instrument panel
  • Very good visibility.
 
Specifications
 
DIMENSIONS
WING SPAN 7.55 m
WING REFERENCE SURFACE 10 mq
FUSELAGE LENGTH 6.25 m
CABIN WIDTH 1.05 m
CABIN HEIGHT 1.05 m
WEIGTHS
EMPTY OPERATIVE WEIGHT 290 Kg
MAXIMUM TAKE OFF WEIGHT (ULM) 450 Kg
MAXIMUM TAKE OFF WEIGHT ((JAR-VLA) 530 Kg
LOADS
IN FLIGHT LOAD FACTORS +4 / -2 g
TANK CAPACITY 80 l
INSTALLABLE AUXILIARY TANK CAPACITY 32 l
OVERALL PAY LOAD LIMIT (ULM) 160 Kg
OVERALL PAY LOAD LIMIT (JAR-VLA) 240 Kg
VBAGGAGE VOLUME 226 l
MAXIMUM BAGGAGE AMOUNT 20 Kg
 
 
Performances
 
PERFORMANCES (ROTAX 912S, VARIABLE PITCH PROPELLER, SEA LEVEL)
MAXIMUM LEVELLED SPEED 285 km/h
CRUISE SPEED (@ 75% POWER) 255 km/h
STALL SPEED 65 km/h
RAPID CIMB SPEED 120 km/h
STEEP CLIMB SPEED 100 km/h
BEST RATE OF CLIMB 460 m/min (1500 ft/min)
ROLL SPEED 120°/sec
AERODYNAMIC EFFICIENCY 12.5:1
RANGE @ 75% POWER 1000 km
RANGE @ 75% POWER WITH AUXILIARY TANK 1450 km
FUEL CONSUMPTION @ 75% POWER 18.5 l/h
OPERATIVE CEILING ALTITUDE 6000 m
TAKE OFF & LANDING GROUND RUNNING 120 m
 
Standard equipment
 
Generals

 

  • Rotax engine 912 UL 80 hp.
  • CSuper Wing - Covered.
  • Gas Suspension Landing Gear (Main + Front).
  • Electric Landing Gear.
  • 2 Fuel Tanks 40 lt each.
  • UK Pedals.
  • UK Stick.
  • Black seat belts.
  • Flap Electronic Controller.
  • Electric Elevator trim.
  • Fiber Instrument Panel and Consolle.
  • Andair Fuel Valve.
  • Landing Gear Doors.
  • Morenica Seats (couple).
  • Morenica Upholstery.
  • Rudder Trim.
  • Cabin Heat.
  • Wing Strobe Light SL6N - PLUS and Landing Light.
  • Cockpit Air Vents.
  • Pioneer Protective Cover.
  • White Body with Two Stripes.
Intruments

  • Speedmeter.
  • Altimeter.
  • Vario.
  • Electric Turn Coordinator.
  • Compass.
  • 2 Fuel Level Indicators.
  • Fuel Pressure Indicator.
  • MED 80 BW Multi engine data include:
    Cooling fluid temperature indicator
    Oil temperature indicator
    Oil pressure temperature indicator
    2 EGT indicators.
  • Auxliliary Electric Socket.
  • Radio Predisposition.
  • Tools.
  • Flight Manual - Check list.
  • Maintenance Manual.