Beiträge von troed

    TECHNICAL SPECIFICATIONS:

    WEIGHT
    Empty weight (914) 272 Kg (600 lb.)
    Maximum take-off gross wt - USA 550 Kg (1212 lb.) (Note: European "ultralight" limitations are 450 Kg)
    Useful Load - USA 277 Kg (612 lb.)

    PERFORMANCE
    Maximum speed 115 mph
    Cruising speed 90 mph
    Absolute ceiling 4000 m (13,000 ft)
    Service ceiling 3500 m (11,400 ft)
    Take-off roll 70 m (230 ft)
    Landing roll from 0 to 30 m (0 to 100 ft)
    Rate of climb 5 m/s (950 ft/min)
    Fuel tank capacity 72 lt (19 gal)
    Endurance 3.4 h
    Range (no reserve) 300 miles

    DIMENSIONS

    Rotor diameter 8535 mm (28 ft)
    Propeller diameter 1700 mm (67 inch)
    Overall width 1800 mm (71 inch)
    Overall length 4655 mm (184 inch)
    Overall height 2600 mm (103 inch)

    DESCRIPTION

    Airframe: Chrome-alloy aeronautical 4130 steel, tig welded. Fiberglass fuselage canopy. Fiberglass wheel pants. Fiberglass instrument panel.
    Seat: With integral fuel-tank manufactured in epoxy resin reinforced with fiberglass.
    Baggage Capacity: 150 Liters
    Instruments: Rotor Tach, Altimeter, Airspeed Indicator, Flydat or EIS engine monitor
    Engine: 914 Rotax Turbo, 4 cylinders, 4-stroke, water-cooled, 115 hp with electric starter and mechanical prerotator.
    Propeller: Arplast 67 inch three-blade carbon fiber with ground adjustable pitch.
    Rotor: two-blade, composite materials.
    Controls: Single - Front Seat.
    Trim Electric

    STANDARD EQUIPMENT Electric Starter
    Airpeed Indicator
    Altimeter
    Flydat or EIS Instrument Monitor
    Cockpit partial enclosure
    Prerotator
    Rotor Brake
    Carburetor Heat and Temperature Gauge - 912 (non-turbo) only
    Wheel Brakes and Wheel Pants
    Landing Light
    Electric Trim - Front
    19 gallon Fuel Tank
    Arplast Propeller
    Magni Rotor

    OPTIONS: Electric trim control - rear seat
    Removable Rear Seat Windscreen

    Dateien

    • Magni_M22.jpg

      (29,22 kB, 465 Mal heruntergeladen, zuletzt: )

    TECHNICAL SPECIFICATIONS:

    WEIGHT
    Empty weight (914) 270 Kg (595 lb.)
    Empty weight (912 ULS) 265 Kg (585 lb.)
    Maximum take-off gross wt - USA 550 Kg (1212 lb.) (Note: European "ultralight" limitations are 450 Kg)
    Useful Load - USA 280 Kg (617 lb.)

    PERFORMANCE
    Maximum speed 115 mph
    Cruising speed 90 mph
    Absolute ceiling 4000 m (13,000 ft)
    Service ceiling 3500 m (11,400 ft)
    Take-off roll 70 m (230 ft)
    Landing roll from 0 to 30 m (0 to 100 ft)
    Rate of climb 5 m/s (950 ft/min)
    Fuel tank capacity 72 lt (19 gal)
    Endurance 3.4 h
    Range (no reserve) 300 miles

    DIMENSIONS

    Rotor diameter 8535 mm (28 ft)
    Propeller diameter 1700 mm (67 inch)
    Overall width 1800 mm (71 inch)
    Overall lenght 4655 mm (184 inch)
    Overall height 2600 mm (103 inch)

    DESCRIPTION

    Airframe: Chrome-alloy aeronautical 4130 steel, tig welded. Fiberglass fuselage canopy. Fiberglass wheel pants. Fiberglass instrument panel.
    Seat: With integral fuel-tank manufactured in epoxy resin reinforced with fiberglass.
    Instruments: Rotor Tach, Altimeter, Airspeed Indicator, Flydat or EIS engine monitor
    Engine: 914 Rotax Turbo, 4 cylinders, 4-stroke, water-cooled, 115 hp with electric starter and mechanical prerotator. Available also with Rotax 912 ULS (100 HP).
    Propeller: Arplast 67 inch three-blade carbon fiber with ground adjustable pitch.
    Rotor: two-blade, composite materials.
    Controls: Dual.
    Trim Electric

    STANDARD EQUIPMENT Electric Starter
    Airpeed Indicator
    Altimeter
    Flydat or EIS Instrument Monitor
    Cockpit partial enclosure
    Prerotator
    Rotor Brake
    Carburetor Heat and Temperature Gauge - 912 (non-turbo) only
    Wheel Brakes and Wheel Pants
    Landing Light
    Electric Trim - Front
    19 gallon Fuel Tank
    Arplast Propeller
    Magni Rotor

    OPTIONS: Electric trim control - rear seat
    Removable Rear Seat Windscreen

    Dateien

    WEIGHT
    Empty weight (914) 248 Kg (547 lb.)
    Empty weight (912) 244 Kg (538 lb.)
    Maximum take-off gross wt - USA 550 Kg (1212 lb.) (Note: European "ultralight" limitations are 450 Kg)
    Useful Load - USA 302/306 Kg (648 lb.)

    PERFORMANCE
    Maximum speed 115 mph
    Cruising speed 90 mph
    Absolute ceiling 4000 m (13,000 ft)
    Service ceiling 3500 m (11,500 ft)
    Take-off roll 70 m (230 ft)
    Landing roll from 0 to 30 m (0 to 100 ft)
    Rate of climb 5 m/s (950 ft/min)
    Fuel tank capacity 45 It (12 gal)
    Endurance 2.1 h
    Range (no reserve) 190 miles

    DIMENSIONS
    Rotor diameter 8230 mm (27 ft)
    Propeller diameter 1700 mm (67 inch)
    Overall width 1800 mm (71 inch)
    Overall length 3950 mm (156 inch)
    Overall height 2500 mm (98.4 inch)

    DESCRIPTION

    Airframe: Chrome-alloy aeronautical 4130 steel, tig welded. Fiberglass fuselage canopy. Fiberglass wheel pants. Fiberglass instrument panel
    Seat: With integral fuel-tank manufactured in epoxy resin reinforced with fiberglass.
    Instruments: Engine Tach, Rotor Tach, Airspeed Indicator, Altimeter, Flydat or EIS engine monitor
    Engine: 914 Rotax Turbo, 4 cylinders, 4-stroke, water-cooled, 115 hp with electric starter and mechanical prerotator. Available also with Rotax 912 ULS (100 HP).
    Propeller: Arplast 67 inch three-blade carbon fiber with ground adjustable pitch.
    Rotor: Two-blade, of composite materials.
    Controls: Single
    Trim Electric

    STANDARD EQUIPMENT: Electric Starter
    Airpeed Indicator
    Altimeter
    Flydat or EIS Instrument Monitor
    Cockpit partial enclosure
    Prerotator
    Rotor Brake
    Carburator Heat and Temperature Guage- 912 (non-turbo) only
    Wheel Brakes and Wheel Pants
    Landing Light
    Electric Trim
    13 gallon Fuel Tank
    Arplast Propeller
    Magni Rotor

    OPTIONS: Supplemental Tank (+9 gallons)

    Dateien

    • Magni_M14.jpg

      (26,9 kB, 1.095 Mal heruntergeladen, zuletzt: )

    Name: Angelo
    Ausbildung: 2004 bei Thomas Kiggen, Michael Ullrich, Björn Krischker
    2004 - 2007: MT03
    2007-2008: Magni M16, Magni M22
    2009 - : Magni M24 Orion
    Ratings: MT03, MT0sport, ELA 07s, XENON RST, Magni M16, Magni M22, Magni M24 Orion
    Flug-locations: AT, HU, DE, IT, CZ, SL, RO, PO, FR, SW, NZ


    Ich freue mich nun auch in diesem Forum diskutieren zu dürfen und rege an, einen link mit Uploadmöglichkeit zu schaffen. Viele Dinge in der Gyrofliegerei lassen sich am besten anhand von Fotos, Graphiken und Tabellen erklären bzw. darstellen :D