F
F
L
L
I
I
G
G
H
H
T
T
M
M
A
A
N
N
U
U
A
A
L
L
F
F
O
O
R
R
U
U
L
L
T
T
R
R
A
A
L
L
I
I
G
G
H
H
T
T
A
A
E
E
R
R
O
O
P
P
L
L
A
A
N
N
E
E
U
U
F
F
M
M
–
–
1
1
3
3
Date of Issue: 30. 1. 2008
1-4
1.4
Descriptive data
1.4.1
Aeroplane description
UFM - 13 ultralight aeroplane is intended for recreational and
cross-country flying. It is not approved for aerobatic operation.
UFM - 13 is
a single engine, all-
fibreglass aeroplane
with two side-by-
side
seats.
The
aeroplane
is
equipped with fixed
two
main
wheel
undercarriage with a
steer able tail wheel.
The fuselage is a
fibreglass shell with
fibreglass
seats
integrated.
Safety
belts are attached to
the seats and to a
shelf intended for
putting off lightweight objects (headphones, maps, etc.).
The wing is a monospar construction with a sandwich skin com-
posed of two layers of fibreglass and special foam. Control surfaces and
empennage is of the same construction.
The aeroplane is controlled by dual push-pull control system, only
rudder drive is controlled by cable. The ailerons and elevator are controlled
by the control stick located between the pilot's legs (co-pilot's). The rudder
is controlled by the rudder pedals, flaps are operated by a control lever
located between the pilots on the fuselage main spar.
Summary of Contents for UFM - 13 LAMBADA
Page 2: ......
