PH-VTA introductie

Report
Introductie Czechsportaircraft PS-28 Cruiser
Briefing Czechsportaircraft PS-28 Cruiser
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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 pauze
20.15 - ?? Systemen.
Briefing Czechsportaircraft PS-28 Cruiser
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Deze presentatie kan / mag niet operationeel gebruikt
gebruikt worden!
Daar zijn het POH, Rotax Manual en de checklist voor.
Briefing Czechsportaircraft PS-28 Cruiser
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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
Max. weight of fuel
Max. baggage weight in rear fuselage
Max. baggage weight in each wing locker
Empty weight (minimum equipment)
Useful load
600 kg
82 kg
18 kg
10 kg
389,5 kg +2%
210,5 kg
NOTE
Actual 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 pilot
Minimum crew weight:
55 kg
Maximum crew weight on each seat: 115 kg
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Speeds:
Maximum at sea level
Cruise, 75% power at 3,000 ft
119 KIAS
93 KIAS
Rate of climb:
At sea level
Best angle of climb speed (vx)
Best rate of climb speed (vy)
825 fpm
55 KIAS
62 KIAS
VS0 – flaps down, power – idle
VS – flaps up, power – idle
31 KIAS
37 KIAS
Stall speeds:
T/O:
-
at 30 - 34 KIAS pull slightly to lift the nosewheel
at 40 - 44 KIAS
after reaching airspeed 62 KIAS
Airplane unstick
Climb
Descend:
Optimum glide speed
Approach speed
Before landing:
Airspeed
Balked landing:
Airspeed
Climb
60 KIAS
60 KIAS
60 KIAS
min60 KIAS
after reaching 62 KIAS
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Het circuit:
Aanvang downwind checks
CIRCUIT-PROCEDURE, SNELHEDEN EN
POWERSETTINGS (NORMALE CIRCUITS).vs.1.20139
PS-28 PH-VTA
DOWNWIND: 80kts/ No Flaps
Aanvang downwindchecks
POINT OF DESCENT: (einde
downwind)
1.Bocht inzetten,gas terughalen (RPM ____)
2.Snelheid terug laten lopen naar 70kts
3.Flaps T/O
BASELEG: 70pkts/ Flaps T/O
TURN TO FINAL:
1.Bocht inzetten,
2.Flaps t/o snelheid 70kts
3.Flaps full, snelheid 60kts (gele driehoek), gas regelen.
FINAL: 60kts/ Flaps full
CLIMB:
65kts
Flaps T/O
200’ a.t.o checks
©WM/090805
Briefing Czechsportaircraft PS-28 Cruiser
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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°)
NOTE
Altitude 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-started3. COMM - giving location and intentions - if possible
4. Ignition Switch - OFF
5. FUEL selector - OFF
6. MASTER GEN - OFF
7. Approach - without steep turns
8. Safety harness - fasten
9. Flaps - as necessary
10. 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 system
If 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 left
tank 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 Service
Instruction SI-912-016
1/ MOGAS
European 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 not
permitted for use.
2/ AVGAS
US standard - AVGAS 100 LL (ASTM D910)
AVGAS 100 LL places greater stress on the valve seats due to its high lead
content and forms increased deposits in the combustion chamber and lead
sediments 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:
Endurance:
512 NM (948 km)
5:26 h:mm
Conditions:
Usable fuel
113 L
(Fuel Capacity 2 x 57 ltr)
75% power of engine
Altitude
Reserve
5,000 RPM
3,000 ft
30 minutes
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Take off distance to 50 ft (15 m):
Concrete:
387 m 1270 ft
Grass:
457 m 1499 ft
Landing distance:
Concrete:
362 m
Grass:
338 m
1188 ft
1109 ft
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Flight test PILOT januari 2011:
http://www.czechsportaircraft.it/wp-content/uploads/2010/12/Pilot-MagazineJan-2011-CSA-PS-Second-Look.pdf
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VRAGEN ?
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Bedankt voor de aandacht en
“see you in the ………..”!
Briefing Czechsportaircraft PS-28 Cruiser
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Film over de PS28 SportCruiser en
de Czech Sport Aircraft fabriek
Briefing Czechsportaircraft PS-28 Cruiser
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