Feature Title
The P68C is the sensible alternative to many single engine and light twin aircraft in today’s General Aviation market, with fuel consumption comparable to many six-cylinder single engine piston aircraft, the P68C is in a class of its own. As a result the P68C is a serious option for satisfying your flying needs.
Specifications
Engine (two Lycoming):
Max Ramp Weight:
Max Take Off Weight:
Max Landing Weight:
Std. Empty Weigt:
Max Useful Load:
Fuel Capacity:
Number of Seats:
Luggage Capacity:
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IO 360 A1 B6 (200 HP)
2100 kg 4630 lb
2084 kg 4594 lb
1980 kg 4365 lb
1420 kg 3130 lb
680 kg 1500 lb
696 lt 184 USG
6
0,56 mc 20 cu.ft |
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Performance
Max Speed @ S.L:
Max Range Cruise Speed(@ 75% & 7500 ft) :
Rate of Climb :(2 Engines S.L. @ MTOW) :
Rate of Climb (1 Engine S.L. @ MTOW) :
Stall Speed (full flaps) : Service Ceiling (2 engines) :
Service Ceiling (2 engines) :
Service Ceiling (1 engine) :
Max Range (best economy @ 7000 ft) :
T.O. Distance Over 50 ft (ISA, S.L, MLW, no wind) :
T.O. Distance (ISA, S.L, MLW, no wind) :
Landing Distance Over 50 ft (ISA, S.L, MLW, no wind) :
Landing Distance (ISA, S.L, MLW, no wind) :
Load Factor:
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320 km/h 173 kts
301 km/h 160 kts
6 m/s 1100 fpm
1 m/s 200 fpm
115 km/h 62kt
6020 mt 19750 ft
1520 mt 5000 ft
2960 km 1510 nm
400 mt 1312 ft
240 mt 787 ft
600 mt 1969 ft
200 mt 656 ft
+ 3,74g - 1,50 g
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