1
Q
MTOW
A
650 kg
2
Q
MLW
A
650 kg
3
Q
Maximum Operating Altitude
A
13000 ft
4
Q
Maximum Load Factor (Flaps UP)
A
+3.8/-1.9 g
5
Q
Maximum Load Factor (Flaps LND)
A
+1.9/0 g
6
Q
Approved Fuel
A
MOGAS + AVGAS 100LL
7
Q
Max/Min Oil Level
A
3/2.5
8
Q
Maximum Number of Occupants
A
2
9
Q
Glide Ratio
A
12.8 (2 nm / 1000 ft)
10
Q
Maximum Baggage Compartment Capacity
A
20 Kg
11
Q
Maximum Demonstrated Crosswind Component
A
15 kn
12
Q
Engine Model
A
ROTAX 912 S2
13
Q
Maximum Engine Power
A
98.6 hp @ 2388 rpm
14
Q
Maximum Continuos Engine Power
A
92.5 hp @ 2265 rpm
15
Q
Maximum time above MCP
A
5 minutes
16
Q
Maximum Total Fuel Tank Capacity
A
124 l
17
Q
Maximum Total Usable Fuel
A
120 l
18
Q
Maximum and Minimum Temp. for Engine Start
A
+50/-25 °C
19
Q
Va
A
98 kias
20
Q
VFE (any setting)
A
70 kias
21
Q
VR
A
50 kias
22
Q
Vx
A
63 kias
23
Q
Vy
A
67 kias
24
Q
Best glide speed (Vg)
A
71 kias
25
Downwind speed
70 kias
26
Approach speed (Flaps LND)
60 kias
27
Approach speed (Flaps UP)
65 kias
28
Maximum reccomended Turbulent Air Penetration Speed
98 kias
29
Stall Speed (Flaps UP)
49 kias
30
Stall Speed (Flaps TO)
46 kias
31
Stall Speed (Flaps LND)
40 kias
32
Altimeters max difference (VFR)
± 75 ft
33
Magnetos drop max/diff
210/50 rpm
34
Carb Heat Expected drop
<100 rpm
35
RPM min/max (ground)
600/2100 rpm
PPL Exam
flashcards
Decks in class (2)
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