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Taurus is made in highest technology composites (epoxy resin, glass fibre, carbon fibre, kevlar fibre and honeycomb structures). The airfoil used on wings is ORL 170, (F. Orlando).
| model |
TAURUS 503 |
| ENGINE ROTAX |
503 UL DCDI 2V |
| max power(with 2 carb.) |
53 hp at 6600 rpm |
| PROPELLER |
2 blade Pipistrel 1600 mm diam |
| SIZES |
| wing span |
14.97 m |
| length |
7.17 m |
| height |
1.41 m |
| wing area |
12.33 m2 |
| rudder area |
0.9 m2 |
| horizontal tail area |
1.36 m2 |
| aspect ratio |
18.6 |
| positive flaps |
5 deg, 9 deg, 18 deg |
| negative flaps |
-5 deg |
| center of gravity |
22% - 41% |
| WEIGHTS |
| empty weight |
285 kg |
| minimum pilot weight |
60 kg |
| maximum total pilots weight |
220 kg |
| max take off weight (MTOW) |
450 kg / 472.5 kg |
| fuel tank capacity in the wing |
30 l |
| useful fuel |
27 l |
| PERFORMANCES |
| stall with flaps |
62.5 km/h |
| stall without flaps |
67 km/h |
| manoeuvring speed |
141 km/h |
| max speed with flaps extended |
130 km/h |
| max speed with airbrakes extended |
225 km/h |
| max. permitted speed |
205 km/h |
| VNE |
225 km/h |
| min.sink |
0.74 m/sec |
| min.sink speed |
85km/h |
| max. sink with airbrakes |
5.5 m/sec @ 100 km/h |
| best glide |
1: 41 |
| best glide ratio speed |
115 km/h |
| best glide at 140 km/h |
1: 36 |
| best glide at 180 km/h |
1: 25 |
| max towing speed |
150 km/h |
| 45°-45° roll time |
3.9 sec |
| take off run MTOW |
155 m |
| take off over 15 m MTOW |
300 m |
| cruising speed with 75% power |
145 km/h |
| best climb speed |
100 km/h |
| max climb rate (MTOW) |
3.5 m/sec |
| service ceiling MTOW |
4,200 m |
| max load factor permitted (x1,8) |
+5.3g -2.65g |
| max load factor tested |
+ 7.2g - 7.2g |
| fuel consum. at full power |
18 lph |
Note: all data are calculated and are subjected to change without notice
BASIC PRICE INCLUDES:
- out surfaces white coloured, cabine indoor surfaces blue coloured
- colouring, finishing and polishing of joints on all plastic parts
- positive and negative flaperons
- automatic command annexation at wing connection
- controlled tail wheel
- wing air brakes
- mecanical elevator trim
- integrated 30 liter fuel tank in the wing with filling cap on top
- noise reducing firewall
- "3 point ""schroth"" seat belts"
- light cabine carpets in blue colour
- white transparent cockpit plexy
- confortable seats with adjustable head rests
- on ground forward adjustable peddals
- five point door fixation
- cabin window with air vent hole on both sides
- separated venting for each pilot
- rectractable mecanical main landing gear
- hydraulic disk brakes on the main wheels
- cigarette lighter connector
- instrument pannel with
- all flight and engine instruments
- libelle (slip indicator)
- magnetic compass with mount
- 2 blade fix pitch wooden propeller
- engine rotax 503 53 hp with 2 carburators
- and automatic electric system to retract the engine
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| (c) Pipistrel UK & Ireland, 2007 |
Website by Galway Media |
