|
XT912-SST |
| PERFORMANCE |
Australian |
European |
USA |
|
Never Exceed Speed VNE indicated |
85 |
kts |
157 |
km/hr |
98 |
mph |
|
Cruise Speed @ MTOW |
70
|
kts |
130
|
km/hr |
80
|
mph |
|
Stall Speed @ MTOW |
35 |
kts |
65 |
km/hr |
40 |
mph |
|
Best Climb Rate(49 knots) @ MTOW |
825 |
ft/min |
4.2 |
m/sec |
825 |
ft/min |
| Best Climb Speed |
49 |
kts |
91 |
km/hr |
57 |
mph |
|
Take off Distance to 15 mts or 50 feet- Note 1 |
247 |
m |
247 |
m |
810 |
ft |
|
Landing Distance @ MTOW from 15 mts- Note 1 |
325 |
m |
325 |
m |
1066 |
ft |
|
Descent Rate 54knots @ MTOW - Note 3 |
770 |
ft/min |
3.9 |
m/sec |
770 |
ft/min |
|
Fuel Tank Capacity - Note 3 |
70 |
lt |
70 |
lt |
18.5 |
gal |
|
Typical Fuel Burn @ Cruise (MTOW) |
11
|
lt/hr |
11
|
lt/hr |
2.9
|
gal/hr |
| Range @� Cruise |
730
|
km |
730
|
km |
453
|
miles |
| |
| NOTE 1: Take off
and landing distances were measured from a short grass
runway. |
|
The data includes the reserve factor of 1.3 as stated
in the manual. |
|
NOTE 2: Fuel consumption figures are included as
a guide only. The consumption figures should not be
used for planning purposes. |
| NOTE 3: Maximum usable fuel 67 Liters
or 17.7 US Gal |
| DESIGN LOADS |
Australian |
European |
USA |
|
Max take off weight (MTOW) |
450 |
kg |
450 |
kg |
992 |
lbs |
|
Ultimate load @ MTOW |
+6g / -3g |
|
Flight limits @ MTOW |
+4g / -0g |
|
Total maximum crew weight |
200 |
kg |
200 |
kg |
440 |
lbs |
| Permitted range of pilot weights (Front seat) |
55-100 |
kg |
55-100 |
kg |
121-220 |
lbs |
| Permitted range of pilot weights (Rear seat) |
0-100 |
kg |
0-100 |
kg |
0-220 |
lbs |
|
Maximum empty weight (see note 3) |
260 |
kg |
260 |
kg |
573 |
lbs |
| |
|
NOTE 3: Includes 3 liters (2kg) unusable fuel. Empty
weight is defined in section 6.2 of the manual. |
| |
| DIMENSIONS |
Australian |
European |
USA |
| Wing Span |
9.97 |
m |
9.97 |
m |
32.7 |
ft |
| Wing Area |
13.5 |
sq mts |
13.5 |
sq mts |
146 |
sq ft |
| Aspect Ratio |
6.6 |
| Wing Weight |
58
|
kg |
58
|
kg |
128
|
lbs |
| Overall Height (Control Bar Fwd) |
3.07
|
m |
3.07
|
m |
10.1
|
ft |
|
Trike Width (to outside of wheel spats) |
1.91 |
m |
1.91 |
m |
6.27 |
ft |
|
Trike Length |
2.745
|
m |
2.745
|
m |
9.01 |
ft |
| Wheel
Track |
1.7 |
m |
1.7 |
m |
5.58 |
ft |
| Wheel
Base |
1.89 |
m |
1.89 |
m |
6.2 |
ft |
| Trike Height |
2.53 |
m |
2.53 |
m |
8.3 |
ft |
| Cockpit Width |
0.7 |
m |
0.7 |
m |
2.3 |
ft |
|
Wing� (Packed) Length |
5.6 |
m |
5.6 |
m |
18.37 |
ft |
| Wing Length (Short Packed) |
4.2 |
m |
4.2 |
m |
13.78 |
ft |
| |
| POWER
PLANT |
PROPELLOR |
| Make |
Rotax Bombardier |
Propellor |
Bolly |
| Model |
912
UL 2 |
Type |
Bos3 68X58_SL ground adjustable |
| Power |
80 |
Hp |
Diameter |
68" |
| Type |
4 Stroke-1198cc |
Pitch |
20 +/- 0.5 deg @ radius of 24" |
| Ignition System |
Dual Electronic |
|
|
| No Cylinders |
4 |
|
|
| Electric Start |
Standard |
|
|
| Reduction Ratio |
2.43:1 |
|
|
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