Page 7- 2
1
rd
Edition, Rev 0
Section 7 – Airframe and Systems description
Introduction
1.
Introduction
This section provides description and operation of the aircraft and its systems.
2.
Airframe
2.1.
W
ING
The wing is of a rectangular planform, with a small tapering of the leading edge
near the cabin, allowing an improved visibility, also in steep turn. Its structure
consists of a single spar metal torsion box. The aircraft is equipped with half-span
slot flaps, with the flap hinge positioned on the lower part of the wing. All struc-
tural parts are made of aluminum light alloy (2024-T3 and 6061-T6), except for tips
and fairings which are in fiberglass.
Fig. 7-1. R
IGHT
W
ING
E
XPLODED
V
IEW
2.2.
F
USELAGE
The P92 Echo MkII fuselage is mainly made by carbon fibers composite materi- als.
The fuselage is made by two main shells that are later assembled bonding the two
main bodies and the floor (in composite material too) and adding aluminum
stiffeners that allow the connection of the main landing gear, seats, wing and in-
strument panel. In this context the fuselage and vertical fin are a unique body. The
following picture shows the main components of the fuselage section.
Summary of Contents for P92 Echo MKII
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