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
7-4
7.1
Introduction
This section provides description and operation of the aeroplane
and its system.
Refer to Section 9, Supplements, for details of optional systems
and equipment.
7.2
Airframe
UFM – 13 airframe is all-fibreglass monocoque construction.
7.2.1
Fuselage
All-fibreglass monocoque construction with integrated seats. There
are stiffening ribs inside the fuselage rear and the fin reinforced with foam.
7.2.2
Wing
The fibreglass wing has one main spar with carbon flanges, no
ribs; the stressed skin is of sandwich construction with a foam core.
7.2.3
Horizontal Tail Unit (HTU)
HTU is of the same construction as the wing, only the spar is
formed by a fibreglass profile.
7.2.4
Vertical tail unit (VTU)
VTU is of sandwich construction and without a spar.
Summary of Contents for UFM - 13 LAMBADA
Page 2: ......
