The Magnum is a quantum leap in light aircraft design and performance with the pedigree of full CAA Type Certification behind it which ensures the quality, back up and long life which such an aircraft demands.
FIRST - Fully CAA Type Approved.
FIRST - All composite hydraulic fully retracting tricycle undercarriage
FIRST - 30% Fowler flaps with low drag cruise setting
FIRST - 160 kts continuous cruise on 100 HP 1000 nautical miles range
FIRST - 200 kg crew, 50 kg baggage, room for skiis 21:1 L/D ratio, max 21 deg alpha
All epoxy composite monocoque, post cured in heated moulds to 80 deg C. - Extensive use of carbon fibre - Extensive use of PVC sandwich panels
Moulded monococque; Glass outer skin, latest high temp PVC sandwich core....... Structure protected against specified levels of BVID.
Moulded glass/carbon sandwich skins; carbon capped I beam main spar and rear flap spar. Conventional glider type spar extensions and spherical wing shear pins.
Laminar flow computer CFD generated section. Wind tunnel tested. - Conventional ailerons on cranked tip. - One man folding facility. - Cantilevered low wing with outboard crank dihedral. - 30% Fowler flap with 10% negative cruise flap with electrical operation by encoded disc position.
Conventional tractor, tricycle. - UC in composite trailing link, "Hyperlast" damper, hy draulic retracting - 12v electric pump with free fall facility. - TOST wheels and hydraulic disc brakes - All moving horizontal stabilizer with trim tab - Side by side seating, semi reclining, dual control. - Carbon framed twin forward hinging plexiglas canopies, gas strut servo. All round and rearward view. - All systems designed for long life and low maintenance.
Rudder, by cable through independently adjustable pedals. - Elevator - push rod with trim anti servo tab. - Ailerons - push rod - Flaps - torsion drive through control gearbox and rack and pinion drive. - Undercarriage - hydraulic operation, vent for emergency deploy.
Currently planned to use the well proven Rotax 914 Turbo charged engine giving 115 hp for 5 mins and 100 hp continuous with optional VP propellor, now approved to full FAR 23.
Flaps 30% Fowler, 10% Cruise
Engine - Rotax 914F turbocharged fully certificated
Propeller - MT Constant speed, 1.7 m