1Briefing Czechsportaircraft PS-28 Cruiser

Introductie Czechsportaircraft PS-28 Cruiser

2Briefing Czechsportaircraft PS-28 Cruiser

Uw presentatoren:

André van den Worm“Het vliegtuig”

Mark Kipping“De elektronica”

Programma:19.30 – 20.00 Het vliegtuig, daarna kort filmpje.20.05 – 20.15 Korte pauze20.15 - ?? Systemen.

3Briefing Czechsportaircraft PS-28 Cruiser

Deze presentatie kan / mag niet operationeel gebruikt gebruikt worden!

Daar zijn het POH, Rotax Manual en de checklist voor.

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Het vliegtuig | stijl

- Hedendaags ontwerp, opvallende ontwerplijnen met zeer goede vliegeigenschappen.- Standaard leren interieur benadrukt het chique voorkomen.- De PS28 Cruiser is wereldwijd uitgeroepen tot het best verkopende lichte GA toestel in 2012!

Piloot | ruimte - Schouderbreedte van 1,18 meter.- Vliegers tot 1,98 meter genieten een uitstekende 'zit‘.- De pedalen zijn over een groot bereik te stellen.

Sensatie | snelheid - Modern naca vleugelprofiel geeft een respectabele en efficiente kruissnelheid.- De vloeistof gekoelde Rotax boxermotor brengt het toestel gemakkelijk boven de 100 knots.- De grote servo aangedreven fowler flaps verlagen de stall snelheid tijdens de landing tot ongeveer 30 knots.

Kosten | technologie - Rotax vliegtuigmotor (TBO 2000 uur), zowel Mogas als Avgas gecertificeerd.- Het verbruik ligt bij een economische kruissnelheid op 16 L/uur.- Aluminium airframe.- Het vlieg-instrumenten paneel met drie beeldschermen.

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Weights:

Max. takeoff and landing weight 600 kgMax. weight of fuel 82 kgMax. baggage weight in rear fuselage 18 kgMax. baggage weight in each wing locker 10 kgEmpty weight (minimum equipment) 389,5 kg +2%Useful load 210,5 kg

NOTEActual empty weight is shown in Section 9, Supplement No. 02

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Loading:

Do not exceed maximum takeoff weight 600 kg.

Number of seats: 2

Minimum crew (only on the left seat): 1 pilotMinimum crew weight: 55 kgMaximum crew weight on each seat: 115 kg

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Speeds:Maximum at sea level 119 KIASCruise, 75% power at 3,000 ft 93 KIAS

Rate of climb:At sea level 825 fpmBest angle of climb speed (vx) 55 KIASBest rate of climb speed (vy) 62 KIAS

Stall speeds:VS0 – flaps down, power – idle 31 KIASVS – flaps up, power – idle 37 KIAS

T/O:- at 30 - 34 KIAS pull slightly to lift the nosewheel

Airplane unstick at 40 - 44 KIASClimb after reaching airspeed 62 KIAS

Descend:Optimum glide speed 60 KIASApproach speed 60 KIAS

Before landing:Airspeed 60 KIAS

Balked landing:Airspeed min60 KIASClimb after reaching 62 KIAS

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Het circuit:

DOWNWIND: 80kts/ No Flaps

BASELEG: 70pkts/ Flaps T/O

FINAL: 60kts/ Flaps full CLIMB: 65kts

Flaps T/O

200’ a.t.o checks

POINT OF DESCENT: (einde downwind)

1.Bocht inzetten,gas terughalen (RPM � ____)

2.Snelheid terug laten lopen naar 70kts

3.Flaps T/O

TURN TO FINAL:

1.Bocht inzetten,

2.Flaps t/o snelheid 70kts

3.Flaps full, snelheid 60kts (gele driehoek), gas regelen.

©WM/090805

Aanvang downwind checks

Aanvang downwindchecks

PS-28 PH-VTACIRCUIT-PROCEDURE, SNELHEDEN EN POWERSETTINGS (NORMALE CIRCUITS).vs.1.20139

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“Turning baseleg….. Oeppssss…

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Airspeeds for Emergency procedures:

- Engine failure after takeoff- Gliding speed (flaps retracted (0°)- Precautionary landing with engine (flaps in landing position (30°)

- Emergency landing without engine power

60KIAS

- Emergency descent 138 KIAS (flaps retracted 0°)

NOTEAltitude loss during 180° turn is approximately 400 ft

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Emergency landing without engine power:

1. Airspeed - maintain 60 KIAS.

2. Emergency landing area - chose suitable area without obstacles.

- the engine cannot be re-started-

3. COMM - giving location and intentions - if possible4. Ignition Switch - OFF5. FUEL selector - OFF6. MASTER GEN - OFF7. Approach - without steep turns8. Safety harness - fasten9. Flaps - as necessary10. MASTER BAT - OFF - before landing

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Gewoon, even er tussendoor…..

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Demonstrated wind performance

Max. demonstrated headwind velocity for take-off and landing: ..... 24 knots

Max. demonstrated crosswind velocity for take-off and landing: ..... 12 knots

Flight in rain:

When flying in the rain, no additional steps are required.Aircraft qualities and performance are not substantially changed.However VMC must be maintained

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Fuel systemIf left tank is full, start engine with the fuel selector set to LEFT.If you would start the engine with the fuel selector set to RIGHT and the left tank is full, than fuel bleed from the left tank vent may occur because a fuel return hose is led only into the lefttank and returning fuel will overfill the left tank.

Recommended fuel type:NOTE: Refer to the ROTAX Operator’s Manual, section 2.4 Fuel, and Rotax ServiceInstruction SI-912-016

1/ MOGASEuropean standard - min. RON 95, EN 228 Super, EN 228 Super plus.

CAUTION:Fuels that contain more than 5% ethanol blend have not been tested and are notpermitted for use.

2/ AVGASUS standard - AVGAS 100 LL (ASTM D910)AVGAS 100 LL places greater stress on the valve seats due to its high leadcontent and forms increased deposits in the combustion chamber and leadsediments in the oil system.Thus it should only be used in case of problems with vapor lock or when other types of gasoline are unavailable.

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Range and endurance:

Range: 512 NM (948 km)Endurance: 5:26 h:mm

Conditions:Usable fuel 113 L(Fuel Capacity 2 x 57 ltr)

75% power of engine 5,000 RPMAltitude 3,000 ftReserve 30 minutes

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Take off distance to 50 ft (15 m):Concrete: 387 m 1270 ftGrass: 457 m 1499 ft Landing distance:Concrete: 362 m 1188 ftGrass: 338 m 1109 ft

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Flight test PILOT januari 2011:

http://www.czechsportaircraft.it/wp-content/uploads/2010/12/Pilot-Magazine-Jan-2011-CSA-PS-Second-Look.pdf

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VRAGEN ?

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Bedankt voor de aandacht en “see you in the ………..”!

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Film over de PS28 SportCruiser en de Czech Sport Aircraft fabriek