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SINUS UL MOTORGLIDER 2003 TECNICAL DATA
Note: In the air adjustable pitch propeller (VARIO) is included in the basic price
model | SINUS 503 | SINUS 912 |
ENGINE ROTAX | 503 UL DCDI 2V | ROTAX 912 UL2 |
max power(with 2 carb.) | 50 hp at 6600 rpm | 80 hp at 5500 rpm |
PROPELLER | Pipistrel VARIO | Pipistrel VARIO |
SIZES | ||
wing span | 14,97 m | 14,97 m |
length | 6,6 m | 6,6 m |
height | 1,70 m | 1,70 m |
wing area | 12,26 m2 | 12,26 m2 |
rudder area | 1,1 m2 | 1,1 m2 |
tail area | 1,63 m2 | 1,63 m2 |
aspect ratio | 18,3 | 18,3 |
positive flaps | 9 deg, 18 deg | 9 deg, 18 deg |
negative flaps | 5 deg | 5 deg |
center of gravity | 20% - 39% | 20% - 39% |
WEIGHTS | ||
empty weight | 265 kg | 284 kg |
max take off weight (MTOW) | 450 kg / 472,5 kg FR | 450 kg / 472,5 kg FR |
fuel tanks capacity | 2 x 30 l | 2 x 30 l |
useful fuel | 2 x 27 l | 2 x 27 l |
PERFORMANCES | ||
stall with flaps | 63 km/h | 63 km/h |
stall without flaps | 66 km/h | 66 km/h |
cruising speed (75% power) | 170 km/h | 200 km/h |
max. horizontal speed | 186 km/h | 220 km/h |
VNE | 225 km/h | 225 km/h |
max speed with airbrakes out | 160 km/h | 160 km/h |
max speed with flaps down | 130 km/h | 130 km/h |
manoeuvring speed | 135 km/h | 135 km/h |
best climb speed | 115 km/h | 120 km/h |
max climb rate ( 450 kg) | 3,2 m/sec | 6,5 m/sec |
climb rate at 140 km/h | 2,8 m/sec | 6,3 m/sec |
min.sink speed | 90 km/h | 90 km/h |
min.sink (prop. 90 deg.) | 0,96 m/sec | 1,03 m/sec |
max. sink with airbrakes | 5,5 m/sec | 5,5 m/sec |
best glide ratio speed | 95 km/h | 95 km/h |
best glide (prop. 90 deg.) | 1:28 | 1:27 |
glide at 150 km/h (prop 90 deg) | 1:18 | 1:18 |
take off run ( 450 kg) | 118 m | 88 m |
take off over 15 m obstacle (450 kg) | 210 m | 148 m |
service ceiling ( 450 kg) | 6100 m | 8800 m |
45° - 45° roll time | 4,2 sec | 4,2 sec |
fuel consum. at cruis. speed | 10,2 l/hour | 9,2 l/hour |
endurance | 5,3 hours | 5,8 hours |
range distance | 900 km | 1200 km |
max load factor permitted ( x 1,8) | +4 g - 2 g | +4 g - 2 g |
max load factor tested | + 7,2 g - 7,2 g | + 7,2 g - 7,2 g |
Note: All data are subject to change without
notice!
*The aircraft are designed to comply with Slovenian Ultralight/Microlight
certification rules, adopted by JAR VLA and JAR 22 rules. Ultralight/Microlight
certification basis varies from country to country, therefore the actual data
may be different from stated above. Please check the homologations link.
IN BASIC PRICE ARE INCLUDED:
OUT SURFACES WHITE COLOURED, CABINE INDOOR SURFACES GREY OR BLUE COLOURED
COLOURING, FINISHING AND POLISHING OF JOINTS ON ALL PLASTIC PARTS
POSITIVE AND NEGATIVE FLAPERONS
AUTOMATIC COMMAND ANNEXATION AT WING CONNECTION
WING AIR BRAKES
ANCHORING POINTS IN THE WINGS
MECANICAL TRIMMER
INTEGRATED TANKS IN THE WINGS WITH FILLING CAPS ON TOP
NEW SHAPE VISUAL CONTROL OF THE FUEL LEVEL
WARNING LIGHTS FOR MINIMUM FUEL LEVEL
NOISE REDUCING FIREWALL
3 POINT "SCHROTH" SEAT BELTS
BAGGAGE SAC BEHIND THE SEATS
LIGHT CABINE CARPETS IN GREY OR BLUE COLOUR
CONFORTABLE SEATS WITH ADJUSTABLE HEAD RESTS
ENGINE HOT AIR CABINE HEATING SYSTEME FOR THE COCKPIT
BOTH SIDES FORWARD ADJUSTABLE PEDDALS
THREE POINT DOOR FIXATION
CABIN AIR VENT HOLE ON THE LEFT DOOR
CABIN WINDOW ON THE RIGHT DOOR
RIVETTED AND GLUED UVR PROTECTED SCRATCH FREE LEXAN ON THE CABINE AND ON THE
DOORS
FAST SCREWS ON THE ENGINE COVERS
HYDRAULIC DISK BRAKES ON THE MAIN WHEELS WITH WHEEL BRAKES LEVERS ON BOTH SIDES
MAIN WHEELS FAIRINGS
CONTROLLED TAIL WHEEL
ALL NEEDED ENGINE MODIFICATIONS AND ALL NEEDED PLANTS
ALL THROTTLE CONTROL BOWDENS IN TEFLON
ELECTRIC STARTER
ACCUMULATOR
REGULATOR-RECTIFIER
ELECTRIC RECYCLING PUMP
FUEL AND AIR CLEANER
IGNITION MASTER KEY SWITCH, BATTERY MASTER SWITCH, AUX.SWITCHES WITH FUSES AND
CONTROL LAMPS
CIGARETTE LIGHTER CONNECTOR
INSTRUMENT PANNEL WITH
BRAUNIGER ALPHAMFD multifunction engine & flight instrument with all flight and
engine instruments functions,
fuel consumption control, memory, alarm, hour counter, clock, flight data
recorder, etc.
LIBELLE (SLIP INDICATOR)
MAGNETIC COMPASS WITH MOUNT
2 BLADE CARBON FIBRE IN THE AIR ADJUSTABLE PROPELLER WITH 90 DEGREES GLIDING
POSITION
SPINNER
The prices and data may change without note.
The price is orientative, f.co Pipistrel, without Slovenian WAT, export and
transport costs. The price in different countries may be different cause costs
of local import and transport costs, cost of local homologations and different
tecnical recquests. For any information from the countries where we have
distributors, please contact distributors first.
model
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503
|
912
|
|
STANDARD VERSION (ALL
SPECIFIED OPTIONS)
|
price EUR
|
49.200
|
60.700
|
ADVANCED KIT
|
|
46.200
|
56.500
|
KIT 49%
|
42.000
|
51.900
|
PIPISTREL
d. o. o. AJDOVŠČINA
GORIŠKA CESTA 50 A
5270 AJDOVŠČINA, SLOVENIJA (SI)
E-mail: pipistrel@siol.net
Tel.: + 386 5 36 63 873
Fax: +386 5 36 61 263