AIRCRAFT DIRECT TO PILOT / BUYER, Many Countries - Except Turkey.
DIRECT FROM MANUFACTURER - NO DEALERS - £ 349,000 excl VAT "15%"
We have reduced the sale price to £ 349,000 - £ 19,000 less than suggested sales price.
Valid on orders placed on or before - 30th June 2009.
VIEW OUR NEW WEBSITE & VIEW THE 9 Minute VIDEO, SHOWING THE AIRCRAFT IN ACTION - INTERIOR & EXTERIOR VIEWS.
View Our Website: premiaireaviation.com (launch date - 4th February)
CONTACT US ABOUT YOUR COUNTRY
4 Seater Aircraft, 6 Seater Available where the large capacity luggage compartment would be sacrificed, with an extra 2 doors.
Description of structure:
Monocoque construction entirely made of carbon composite with honeycomb filler. The wing is outfitted with flaps and ailerons and has folded tips to facilitate hangaring. Fuel tanks are built into the wing. The airfoil, which is constant along the entire span, is NACA 747A315. Dihedral equals 1.75 deg.
The fuselage has a large door opened upwards in the front section and a cargo hatch in the central section. The passenger cabin has four independent seats; those at the front are slidable and have an adjustable back-rest. The seats are outfitted with three-point inertia reel safety belts.
The vertical tail unit is integrated with the fuselage. Tail plane in T system. Both control surfaces have electric trimmers. Rigid type control systems, rudder controlled by cables. The aircraft is propelled by two counter-rotating LYCOMING IO320 / LIO320 engines with 160HP at 2,700 rpm. The three-blade, constant speed, hydraulically controllable-pitch propellers are manufactured by the MT 3 company.
The landing gear is hydraulically retracted into the fuselage space. It is equipped with a gas shock absorber and hydraulic damping.
Electrical system: voltage: 28V, two Kelly Aerospace alternators, 1 GILL battery with ground power socket.
Fuel system: Tanks with a total capacity of 440 l, two main fuel pumps and two auxiliary fuel pumps are installed in the wings. The tanks are equipped with fuel level gauges and a low fuel level sensor.
Hydraulic system: used for retracting/lowering landing gear, built with Parker Hannifin components.
Brake system: hydraulic Parker Hannifin, Goodridge
Telecommunication: Garmin GMA-340
Navigation: Garmin GNS-430, GNS-530
Flight instruments: United Instruments, UMA Instruments, R.C. ALLEN
Vacuum system: for supplying Rapco Inc. flight instruments
Engine instruments: J.P. Instruments EDM900
Engine fire alarm system.
Wing gross area: 16.50 m2
Maximum take-off flight: 1820kg
Cargo: max. 550kg
Cargo in cabin: max. 450 kg
Fuel: max. 240 kg
Range: max. 1500km
Cruising speed 80%: 278 km/h
Cruising speed 60%: 268 km/h
Maximum speed: 350 km/h
Landing speed: 148 km/h
Stalling speed: 113 km/h
Rate of climb: 1300 ft/min
Ceiling: 5500 m
Take-off run: 352 m
Landing run: 319 m
QUITER THAN ANY FRONT FACING PROPELLER TWIN AIRCRAFT