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F
L
I
G
H
T
F
L
I
G
H
T
5.3.2
Endurance
In the following table are stated fuel consumptions, endurances
and ranges for RPM settings of UFM – 13 ultralight aeroplane.
Engine speed
Airspeed
Fuel
consumption
Range
5.3.3
Demonstrated crosswind performance
Max. permitted cross wind velocity
for take-off and landing
Max. permitted head wind velocity
for take-off and landing
Date of Issue: 30. 1. 2008
M
A
N
U
A
L
F
O
R
M
A
N
U
A
L
F
O
R
U
F
U
F
Regime
[rpm]
IAS [km/h]
CAS [km/h]
[l/h]
[km]
U
L
T
R
A
L
I
G
H
T
U
L
T
R
A
L
I
G
H
T
M
–
1
3
M
–
1
3
Max. Continuous
Power
5500
160
165
20
825
5
12
A
E
R
O
P
L
A
N
E
A
E
R
O
P
L
A
N
E
Economy
Cruise
4500
130
132
9.5
1390
m/s
m/s
5-7
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