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Description
Metric
Imperial
GENERAL
Certification basis
ASTM F2245-16c
LTF UL-2019
SACAA-Part 24
ASTM F2245-16c
LTF UL-2019
Fuel capacity
105 (L)
27.7 (gal)
Cockpit width widest point
1,075 (m)
42.3 (in)
Total length - FRL Level
5,915 (m)
232.87 (in)
Wing Span
9,34 (m)
30.64 ft
Wing Area
12,19 (m2)
131.2 ft2
Wing MAC
1,305 (m)
14 ft2
Height FRL level (6.00 x 6)
2,625 (m)
89 (in)
Seats
2 side by side
2 side by side
Wheel track
1,73 (m)
68 (in)
Available as a nose wheel or tailwheel aircraft.
Weights and Loads
Empty Weight (kg) (options dependent)
340-365kg
750-805 (lbs)
Empty Weight (kg) (options dependent)
(excluding parachute)
340-365kg
750-805 (lbs)
MTOW
600 (kg)
1320 (lbs)
Baggage capacity (kg)
30
66 (lbs)
Baggage volume (m3)
0.1
0.1
Limit design load factors (g)
+4/-2
+4/-2
Ultimate design load factors
+6/-3
+6/-3
Powerplant **
Engine
Rotax 914
Rotax 912 uls
Hp
115
100
Propeller (FP-Propeller 3-blade electric variable pitch with warp drive blades)
Full Auto
Full Auto
Performance
(Based on a standard Rotax 912 uls engine)
Take-off roll
80 (m)
260 (ft)
Landing roll
90 (m)
295 (ft)
Rate of Climb
800 (ft/min)
800 (ft/min)
Stall, Clean config
42 (kt)
42 (kt)
Stall Landing config (8 degr)
37 (kt)
37 (kt)
Stall full flap (12-15 degr)
35 (kt)
35 (kt)
Cruise @ 5100rpm @ 7000ft (IAS)
85 (kt)
85 (kt)
VNE
121 (kt)
121 (kt)
VNO
100 (kt)
100 (kt)
VA
90 (kt)
90 (kt)
VH
105 (kt)
105 (kt)
Service ceiling (ft)
14000
14000
Fuel consumption (L/hr)
18 (L/hr)
4.8 (gal(US)/hr)
Demonstrated cross wind (kt)
20
20
Performance figures based on a sea-level standard day using the powerplant listed and employing average piloting techniques. (Take-off distance, climb rate and cruise figures will significantly improve with the fitment of the approved turbo charged engine versions.)
