|
U.S.
Sport Pilot |
| Engine |
Lyc O-235 |
Rotax 912 |
Rotax 912-S |
| Horsepower |
116 |
80 |
100 |
| Power Loading (lb./hp) |
11.4 |
16.5 |
13.2 |
| Gross Weight (lb.) |
1320 |
1320 |
1320 |
| Empty Weight (lb.) |
880
|
725 |
730
|
| Useful Load (lb.) |
440 |
595
|
590
|
| Wing Area (sq. ft) |
150 |
150 |
150 |
| Wing Loading (lb./sq. ft) |
9 |
9 |
9 |
| Rate of Climb @ Gross (ft/min) |
700 |
550 |
670 |
| Climb Speed (mph) |
65 |
60 |
60 |
| Take Off Run (ft) |
400 |
350 |
300 |
| Landing Roll (ft) |
400 |
350 |
350 |
| 50' Obstacle Clearance (ft) |
780 |
850 |
750 |
| Stall (No Flap) Power Off (mph) |
45 |
40 |
40 |
| Stall (FULL FLAP) Power Off (mph) |
42 |
35 |
36 |
| Cruise (65% POWER) (mph) |
105 |
95
|
100 |
| Vne (mph) |
151 |
143 |
143 |
| Top Speed (mph) |
115 |
105 |
110 |
| Fuel Burn (gal/hr) |
6 |
3.5 |
5 |
| Fuel Capacity (US gal) |
32 |
32 |
32 |
Range (hrs) (no reserve)
|
5
|
8 |
6
|
Range (statute miles) (no res.)
|
525 |
760 |
600 |
| G Limit (Ultimate) |
+5.7 -3.8 |
+5.7 -3.8 |
+5.7 -3.8 |
PLEASE NOTE: The stated
performance figures are estimates only, based on textbook
analysis and design criteria. In a continuing effort to
improve standards of development, Murphy Aircraft Mfg. Ltd.
reserves the right to make changes to design and performance
specifications at any time without notice.
|
