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Maximum speed got during the tests amounts to 210 km/h without any
vibration or stability decrease. After introducing the mass balance of the control
surfaces, the plane is expected to fly safely at the speed of over 250 km/h .
Permissible wind components for take-off and landing:
- Head-wind: 15 m/s
- Cross-wind: 5 m/s
Lift ratio (soaring):
- With the engine off: 13-14
- With
the idle run engine: 9-10
Serial equipment:
Safety:
- Parachute
rescue system by Galaxy.
- Tetra
pointed, regulated safety belts.
- White,
stroboscopic, anti collision lamp on the fin.
- Half-transparent
tanks enabling optical control of fuel level.
- Fuel sedimentation tank.
- Metal
fuel conduit in the fuselage.
- Locked fuel filler.
- Fire
partition is covered with fireproof shell.
- Cockpit is externally
locked.
- Breaking power divisor.
- Shock absorber legs.
Comfort:
- Dim
cockpit glazing (free of charge option).
- Cockpit
raised by to gas springs.
- Bucket
seats, re-set on the surface, with taken off upholstery.
- Upholstered
arm-rest between the seats.
- Two luggage boots.
- Regulated
hot and cold air ventilators.
- Locked bonnet.
Avionics / Equipment of the cockpit:
- Speedometer.
- Variometer.
- Altimeter.
- Compass.
- Bank
indicator cross level with a ball.
- Fuel
indicator with two reserve lamps.
- Main
valve cutting off the fuel supply.
- Flap position indicator.
- Oil
pressure (four-stroke engines) and charging a battery lights.
- The
main switch of current.
- Two firing switches.
- Ignition
switch equipped with service position.
- Central
control stick with brake lever, equipped with gilded switches
controlling flaps, trimmer and broadcasting station.
- Aerial
and the cable feeding broadcasting station (12 V).
- Folding
throttle levels on both sides.
- Choke rod.
- Voltmeter.
- Revolution counter.
Engine
indicators:
Rotax 912 UL:
- Cooling fluid temperature.
- Oil temperature.
- Oil pressure.
- Fuel pressure.
Verner 133 M:
- Left head temperature.
- Right head temperature.
- Oil temperature.
- Oil pressure.
- Fuel pressure.
Rotax 582 UL:
- Cooling fluid temperature.
Additional equipment (extra charge
accessories):
- Broadcasting
station ICOM IC - A110 / A110 EURO.
- Intercom.
- Head-phones.
- Number signs.
Technical
data / Plane performance:
Span: 10,0 m
Length: 5,95 m
Height: 2,30 m
Lifting surface: 9,72 m2
Surface load: 49,4 kg/m2
Maximum take-off mass: 480
kg
Minimum speed at maximum take-off mass and
respectable flap settings:
- 6° ( flight ): 68
km/h !
+ 15° ( take off ): 64
km/h !!
+ 28° ( landing ): 56 km/h
!!!
Maximum speed Vne: 210
km/h
Landing run: 100 m
... with Rotax 912 UL:
Complete kerb weight: 280
kg
Maximum speed in horizontal flight: 210 km/h
Cruising speed ( 75% power ): 180 km/h
Maximum ascending velocity: 8 m/s
Take-off run: 80 m
15 m take-off: 150 m
Range: 700 km
... with Verner 133 M:
Complete kerb weight: 290
kg
Maximum speed in horizontal flight: 190 km/h
Cruising speed ( 75% power ): 165 km/h
Maximum ascending velocity: 5 m/s
Take-off run: 120 m
15 m take-off: 220 m
Range: 500 km
...with Rotax 582 UL:
Complete kerb weight: 265
kg
Maximum speed in horizontal flight: 180 km/h
Cruising speed ( 75% power ): 155 km/h
Maximum ascending velocity: 4 m/s
Take-off run: 120 m
15 m take-off: 220 m
Range: 450 km
Technical data of the engines:
Rotax 912 UL:
Tetra-cylindered, four-stroke engine in boxer system. Air-cooled block,
liquid-cooled heads.
Engine equipment in Beetle:
- Toothed
revolution reducer with vibration damper.
- Double firing.
- Two Bing carburettors.
- Oil cooler.
Capacity: 1211 cm3
Piston diameter: 79,5 mm
Piston stroke: 61 mm
Compression ratio: 1 : 9,0
Maximum power: 81 HP at 5800 Rpm
Continuous power: 79 HP at 5500 Rpm
Maximum turning moment: 103 Nm at 4800 Rpm
Alternator: 12 V / 250 W
Revolution reducer ratio: 1:2,27
TBO: 1200 h
Fuel: 100 LL Avgas or car petrol min. 91 Okt.
Verner 133 M.:
Two-cylindered, four-stroke engine in boxer system. Air-cooled block
and heads.
Engine equipment in Beetle:
- Toothed
revolution reducer with vibration damper.
- Double firing.
- Two Dilortto carburettors.
- Oil cooler.
Capacity: 1329 cm3
Piston diameter: 97 mm
Piston stroke: 90 mm
Compression ratio: 1 : 9,8
Maximum power: 78 HP at 5000 Rpm
Continuous power: 68 HP at 4000 Rpm
Maximum turning moment: 129 Nm 3500 Rpm
Alternator: 12 V / 150 W
Revolution reducer ratio: 1:2,0
TBO: 800 h
Fuel: 100 LL Avgas or car petrol min. 95 Okt.
Rotax 582 UL:
Two-cylindered, two-stroke engine. Liquid-cooled block and heads.
Engine equipment in Beetle:
- Toothed
revolution reducer with vibration damper.
- Double firing.
- Two Bing carburettors.
Capacity: 580 cm3
Piston diameter: 76 mm
Piston stroke: 64 mm
Maximum power: 65 HP 6800 Rpm
Maximum turning moment: 75 Nm 6000 Rpm
Alternator: 12 V / 150 W
Revolution reducer ratio: 1:3,0
TBO: 300 h
Fuel: Car petrol min 90 Okt with the addition of two-stroke engine oil -
proportion 1:50
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