|
BACK
|
P92-JS
|
| DIMENSIONS |
| Wing
Span |
30
ft 6 in (9,30 m)
|
| Lenght
over-all |
20
ft 8 in. (6,30 m)
|
| Height
over-all |
8
ft (2,45 m)
|
| Width
cabin |
3
ft 7.5 in. (1.10 m)
|
| Wing
area |
142
sq ft (13,2 mq)
|
| Aspect
ratio |
6,55
|
| Dihedral
angle |
1,5°
|
| Tailplane
span |
9
ft 6 in. (2,90 m)
|
| Wheel
track |
6
ft (1,80 m)
|
| Wheel
tyres |
5,00-5
|
| ENGINE
& PROPELLER |
| Power
max |
ROTAX
912A 59,6 Kw (80 hp) @ 5800 rpm
ROTAX 912S 73,5 Kw (100 hp) @ 5800 rpm
|
| Propeller |
GT
wooden two-blade
|
| Fuel |
EURO
SUPER
|
| Tanks |
80
hp (70 Lt. - 18,5 US gallons)
|
| WEIGHT |
| Max
T.O. |
1212
lb (550 Kg)
|
| Useful
Load |
530
lb (240 Kg)
|
| Wing
loading |
8,83
lb/sq ft (41,7 Kg/mq)
|
| Basic
empty weight (standard) |
683
lb (310 Kg)
|
| Load
ultimate factor |
+3.8
-1.5
|
| PERFORMANCE |
80
hp
|
100
hp
|
| Max
speed s/l |
110
kts (200 km/h)
|
119
kts (220 km/h)
|
| Cruising
speed 75% |
100
kts (185 km/h)
|
100
kts (185 km/h)
|
| Rate
of climb |
860
ft/min (5 m/s)
|
1000
ft/min (5 m/s)
|
| Stalling
speed (flap down) |
36
kts (67 km/h)
|
36
kts (67 km/h)
|
| Service
ceiling |
13500
ft (4100 m)
|
14000
ft (4300 m)
|
| Max
range (without reserve) 65% |
400
nm (740 km)
|
450
nm (740 km)
|
| Take
off to 15m (50 ft) |
1100
ft (330 m)
|
950
ft (290 m)
|
| Take
off run |
540
ft (165 m)
|
470
ft (145 m)
|
| Landing
run |
315
ft (100 m)
|
315
ft (100 m)
|
| Landing
distance |
870
ft (265 m)
|
870
ft (265 m)
|
NOISE EMISSION BELOW 65 dB
|