Aircraft S/N : 17201510 / 1976
Engine
- Type Lycoming O-320-E2D
- Power 150 BHP @ 2700 RPM
- Static RPM 2300 - 2420 RPM
Fuel
- Type 100 (green) or 100LL (blue)
- Total usable 144 l. (38 USGal)
- FFcruise, 75%BHP 31l/u (8,2 USGal)
Oil
- Type W80
- Total Capacity 7,6 l (8.0 qt)
- min. Required 5,7 l (6.0 qt)
Speed max glide range : 65 kts. (Cl/CD)max = 9
Empty weight : 670,3kg.
Max usable load : 372,7 kg. (norm) / 236,9 kg. (util)
MTOW : 1043 kg. (norm) / 907,2 kg. (util)
Max. crosswind component : 15 kts.
ISA MSL T/O run required : 264 m (flaps 0)
ISA MSL T/O distance required over 50 ft : 465 m (flaps 0)
ISA MSL landing ground roll : 159 m (full flaps)
ISA MSL LDR : 381 m (full flaps) over 50 ft.
Significant speeds (kts):
Vs : 47 flaps up/ 41 flaps full Vx : 59 Vglide : 65 flaps up/ 60 flaps down Vy : 78 SL/ 74 @ 4000ft Vfe : 85 Va : 97 @ 1043kg./81 @ 740 kg. Vno : 128 Vne : 160