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PS-28 Cruiser - SKYcastle

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letak CSA 4.indd 1 12.4.2012 11:48:04<br />

BRS system as an option www.czechsportaircraft.com<br />

EASA E A S Certi�ed A C e r t if ie d<br />

<strong>PS</strong>-<strong>28</strong> <strong>Cruiser</strong><br />

info@czechsportaircraft.com, +420 576 514 032<br />

www.<strong>SKYcastle</strong>.nl<br />

info@skycastle.nl +31 653 941 985<br />

New Era<br />

of General Aviation Training<br />

Started<br />

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PROPELLER<br />

Manufacturer:<br />

Model<br />

numbe<br />

Diameter:<br />

Type:<br />

ENGINE<br />

Manufacturer:<br />

B RP-<br />

Powertrain<br />

GmbH&Co.<br />

KG<br />

Model<br />

number:<br />

Rotax<br />

912ULS2<br />

Type: 4-stroke, 4-cylinder horizontally opposed, spark ignition<br />

engine<br />

with<br />

one<br />

central<br />

camshaft-push-rod-OHV<br />

Maximum power rating: 74 kW, 100 HP at 5 800 RPM<br />

e<br />

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AVIONICS<br />

Airspeed indicator<br />

Altitude indicator<br />

Vertical speed indicator<br />

cial horizon<br />

Turn and bank indicator<br />

Directional gyro<br />

Magnetic compass<br />

Engine RPM<br />

Oil temperature gauge<br />

Oil pressure gauge<br />

CHT gauge<br />

Fuel pressure gauge<br />

Fuel quantity gauge<br />

Voltmeter<br />

VHF:<br />

XPNDR:<br />

Intercom<br />

G<strong>PS</strong>:<br />

ELT:<br />

<strong>PS</strong>-<strong>28</strong> <strong>Cruiser</strong> Classic<br />

r:


<strong>PS</strong>-<strong>28</strong> <strong>Cruiser</strong> is a double seater aircraft of full-metal construction. The aircraft is<br />

arranged as a low wing mono-plane with cantilevered wings and a conventional<br />

empennage. <strong>PS</strong>-<strong>28</strong> <strong>Cruiser</strong> is EASA certifi ed aircraft, primary designed for basic<br />

fl ight training, as well as for advanced fl ight training, practice of group fl ying and,<br />

of course, for tourist fl ying.<br />

<strong>PS</strong>-<strong>28</strong> <strong>Cruiser</strong><br />

Wingspan: 8,6 m<br />

Lenght: 6,62 m<br />

Height: 2 315 m<br />

Wing Area: 12,3 m2 Wingspan: 8,6 m<br />

Height: 2 315 m<br />

MTOW: 600 kg<br />

Empty weight: 374 kg<br />

Cockpit width: 1 170 mm<br />

Range: 1 100 km<br />

Endurance: 6 hours 10 min<br />

Fuel capacity: 2x57 l<br />

Average fuel consumption: 17,5 l/FH<br />

Approved fuel:<br />

Max. Max. baggage weight<br />

Mogas, Avgas<br />

in rear fuselage:<br />

Max. baggage weight<br />

18 kg<br />

in each wing locker: 10 kg<br />

Cruise speed at 3000 ft, 75% power:<br />

93 KIAS (172 km/h) km/h)<br />

Max. horizon speed: 119 KIAS (220 km/h)<br />

V : NE<br />

Stall speed V : SO<br />

Climb rate: 138 KIAS (255 km/h)<br />

31 KIAS (57 km/h)<br />

825 ft/min (4,5 m/s)<br />

Take-off distance to 15 m: concrete 387 m<br />

grass 457 m<br />

Landing distance from 15 m: concrete 362 m<br />

grass 338 m<br />

<strong>PS</strong>-<strong>28</strong> <strong>Cruiser</strong><br />

Glass Cockpit<br />

ENGINE<br />

Manufacturer: BRP- Powertrain GmbH&Co.KG<br />

Model number: Rotax 912ULS2<br />

Type: 4-stroke, 4-cylinder horizontally opposed, spark ignition<br />

engine with one central camshaft-push-rod-OHV<br />

Maximum power rating: 74 kW, 100 HP at 5 800 RPM<br />

PROPELLER<br />

Manufacturer: Woodcomp s.r.o.<br />

Model number: Klassic 170/3/R<br />

Diameter: 1 712 mm<br />

Type: three composite blades, ground adjustable<br />

AVIONICS<br />

Primary Flight Data Display: Dynon D100<br />

Engine monitoring system: Dynon D120<br />

VHF/NAV: Garmin SL-30 VHF/NAV+HS34<br />

Intercom<br />

Transponder: GTX-3<strong>28</strong>, S mode, Class 2<br />

G<strong>PS</strong>: Garmin 695<br />

ELT: 121.5 MHz, 243.0 MHz, 406 MHz<br />

Backup Airspeed indicator<br />

Backup Altitude indicator<br />

BRS system as an option<br />

letak CSA 4.indd 2 12.4.2012 11:48:11

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