model |
SINUS 912 |
ENGINE ROTAX |
ROTAX 912 UL2 |
max power(with 2 carb.) |
80 hp at 5800 rpm |
PROPELLER |
Pipistrel VARIO |
SIZES |
|
wing span |
14,97 m |
length |
6,6 m |
height |
1,70 m |
wing area |
12,26 m2 |
rudder area |
1,1 m2 |
tail area |
1,63 m2 |
aspect ratio |
18,3 |
positive flaps |
9 deg, 18 deg |
negative flaps |
5 deg |
center of gravity |
20% - 39% |
WEIGHTS |
|
empty weight |
285 kg |
empty weight light version |
275 kg |
max take off weight (MTOW) |
450 kg / 472.5 kg / 544kg |
fuel tanks capacity |
2 x 30 l / 2 x 50 l |
useful fuel |
2 x 27 l / 2 x 45 l |
PERFORMANCES |
DATA PUBLISHED FOR TOM of 472.5 kg |
stall with flaps |
63 km/h |
stall without flaps |
66 km/h |
cruising speed (75% power) |
200 km/h |
max. horizontal speed |
220 km/h |
VNE |
225 km/h |
max speed with airbrakes out |
160 km/h |
max speed with flaps down |
130 km/h |
manoeuvring speed |
141 km/h |
best climb speed |
120 km/h |
max climb rate ( 450 kg) |
6,5 m/sec |
climb rate at 140 km/h |
6,3 m/sec |
min.sink speed |
90 km/h |
min.sink (prop. 90 deg.) |
1,03 m/sec |
max. sink with airbrakes |
5,5 m/sec |
best glide ratio speed |
95 km/h |
best glide (prop. 90 deg.) |
1:27 |
glide at 150 km/h (prop 90 deg) |
1:18 |
take off run ( 450 kg) |
88 m |
take off over 15 m obstacle (450 kg) |
148 m |
service ceiling ( 450 kg) |
8800 m |
45° - 45° roll time |
4,2 sec |
fuel consum. at cruis. speed |
9,2 l/hour |
endurance (std tanks) |
5,8 hours |
range distance |
1200 km |
max load factor permitted ( x 1,8) |
+4 g - 2 g |
max load factor tested |
+ 7,2 g - 7,2 g |
|
