| Engine: |
2 Lycoming 1O-360
200 H.P fuel injected |
| Propeller: |
|
| Electrical Supply |
12 Volts : Battery situated in FWD Baggage Compartment |
| Normal cruise: |
145 mph 2200 rpm 2200" m/p |
| Maximum Weight: |
4200 lbs (1909 Kg) |
| Basic Empty Weight: |
2935lbs (1334 kg) |
| Useful Load |
1265 lbs (575 Kg) |
| Fuel capacity: |
Full: 97 US galls
Usable: 96 US galls |
| Fuel flow rate (75%): |
21 imp galls/hour
100 ltr/hour |
| Fuel flow rate (65%): |
18 imp galls/hour
85 ltr/hour |
| Oil Capacity: |
Minimum 6 US Quarts, Maximum 8 US Quarts per engine |
Airspeed Limitations
|
| Never exceed speed (Vne): |
217 mph |
| Maximum structual crusing speed (Vno): |
190 mph |
| Maximum Flap extension speed (Vfe): |
10 deg 160 mph
25 deg 140 mph
40 deg 125 mph |
| Maximum Gear Extension speed (Vle): |
150 mph |
| Maximum Gear up speed (Vlo): |
125 mph |
| Manoeuvring speed (Va): |
at 4200 lbs 146 mph
at 2743 lbs 133 mph |
| Minimum Control Speed (Vmca): |
at 4200 lbs 146 mph
80 mph |
| Maximum crosswind: |
13 KT |
| Stall speeds (0 deg angle of bank): |
clean: 76 mph
40 deg flap: 69 mph |
Normal Operation
|
| Take-off Performance - Ground Roll: |
800 ft |
| Take-off Performance to 50 ft: |
1235 ft |
| Landing Performance - Ground Roll: |
705 ft |
| Landing Performance from 50 ft: |
1335 ft |
| Rate of climb at sea level: |
1360 ft/min |
| Rate of climb at sea level single engine: |
190 ft/min |
| Service Ceiling: |
17 900ft |
| Absolute Ceiling: |
19 400ft |
| Service Ceiling single engine: |
3 650ft |
| Absoulte Ceiling single engine: |
5 000ft |
| Take-off safety speed: |
85 mph |
| Best rate of climb speed (Vy): |
105 mph with 2400 rpm 2400" mp |
| Best angle of climb speed (Vx): |
105 mph with 2400 rpm 2400" mp |
| Best rate of climb single engine (Vyse): |
105 mph |
| Cruising Speed 75%: |
172 mph |
| Cruising Speed 75% 6000': |
186 mph |
| Optimum Speed 65% 9000': |
183 mph |
| Base approach speed: |
105 mph rpm A/S 2400" mp |