Edge
XT 912 / Streak III
|
PERFORMANCE |
Australian |
European |
USA |
Never Exceed Speed VNE indicated
|
85
|
kts |
157
|
km/hr |
98
|
mph |
Cruise Speed @ MTOW
|
65 |
kts |
120 |
km/hr |
75 |
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)
|
12 |
lt/hr |
12 |
lt/hr |
3.17
|
gal/hr |
Range @� Cruise |
702 |
km |
702 |
km |
436 |
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 |
50
|
kg |
50
|
kg |
110.23
|
lbs |
Overall Height (Control Bar Fwd) |
3.65 |
m |
3.65 |
m |
11.98 |
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 |
6.20 |
ft |
Trike Height |
2.53 |
m |
2.53 |
m |
8.30 |
ft |
Cockpit Width |
0.7 |
m |
0.7 |
m |
2.30 |
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 |
|
|