|
Edge
XT 912 / Cruze
|
| PERFORMANCE |
Australian |
European |
USA |
|
Never Exceed Speed VNE indicated
|
73
|
kts |
135
|
km/hr |
84
|
mph |
|
Cruise Speed @ MTOW
|
50
|
kts |
92
|
km/hr |
57
|
mph |
|
Stall Speed @ MTOW
|
33
|
kts |
61
|
km/hr |
38
|
mph |
|
Best Climb Rate(49 knots) @ MTOW
|
976
|
ft/min |
5.0
|
m/sec |
976
|
ft/min |
| Best Climb Speed |
45
|
kts |
83
|
km/hr |
52
|
mph |
|
Take off Distance to 15 mts or 50 feet- Note 1
|
210
|
m |
210
|
m |
689
|
ft |
|
Landing Distance @ MTOW from 15 mts- Note 1
|
306
|
m |
306
|
m |
1004
|
ft |
|
Descent Rate 54knots @ MTOW - Note 3
|
597
|
ft/min |
3.0
|
m/sec |
597
|
ft/min |
|
Fuel Tank Capacity - Note 3
|
70 |
lt |
70 |
lt |
18.5 |
gal |
|
Typical Fuel Burn @ Cruise (MTOW)
|
9.5
|
lt/hr |
9.5
|
lt/hr |
2.5
|
gal/hr |
| Range @� Cruise |
650
|
km |
650
|
km |
403
|
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 |
14.4
|
sq mts |
14.4
|
sq mts |
155
|
sq ft |
| Aspect Ratio |
6.6 |
| Wing Weight |
51
|
kg |
51
|
kg |
112
|
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 |
|
|
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