Tecnam P92-JS - INTRODUCTION; AIRFRAME; WING

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
7-2
P92-JS
S E C T I O N 7
SYSTEMS
INTRODUCTION
This section provides description and operation of the aircraft and its systems.
AIRFRAME
WING
The wing is constructed of a central light alloy torque box; an aluminum
leading edge with integrated fuel tank is attached to the front spar while flap
and aileron are hinged to rear spar. Flaps are constructed of a center spar to
which front and rear ribs are joined; wrap-around aluminum skin panels cover
the flap structure. The aileron is constructed of an aluminum spar to which a
formed sheet metal leading edge and metal ribs are attached; a wrap-around.
thermosetting synthetic material covers aileron structure.
Fig. 7-1. RIGHT WING EXPLODED VIEW