Flaps Control; Elevator Control - Pro.Mecc Freccia Maintenance Manual

Ul-aircraft ltf-ul 2003
Table of Contents

Advertisement

Maintenance Manual V001
FRECCIA
Control-stick adjustment
If the control stick is in a neutral position and the ailerons are not lined up with the respecti-
ve tips, act as follows:
1 Remove the door on the seats's floor;
2 Unscrew the M6 nut to take off the connecting rod from the control-stick transfer;
3 Fix the aileron and the control stick in a neutral position;
4 The connecting rod goes up an adjustable head: unscrew the control for some turns and
rig the head until it can enter easily in the control-stick bolt;
5 Screw again the M6 nut and lock the checknut;
6 Close the door.
Seite 18

2.9. FLAPS CONTROL

Flaps control is electric-type, made of a linear actuator driven by electric switch. The control sys-
tem is positioned inside the fuselage, accessible removing the trunk.
Flaps control is an electric switch with up-down positions located on the instrument panel in the
cockpit, on the control panel; by means of it flaps can be adjusted in continuous movement from
0° to 35° positions.

2.10. ELEVATOR CONTROL

The stabilizer is slightly in nosedive position to facilitate the aircraft nose-up, especially on take-
off. The elevator travel, respect to the neutral position, is of 20° +-1° upward and 15° +-1° down-
ward.
The elevator control is consisting of handle, connecting rod and quickdraw. The duralumin tube is
connected to axis, by means of ball bearing. The flapping of the "pushed" or "pulled" handle is
limited by control stops on the two sides of the axis.
The axis is fastened to the fuselage frame's bottom tube through two bolts; around them the con-
trol stick is rotated lenghtwise.
The control-stick quickdraw is connected to the elevator one through a bar.
Maintenance Manual V001
FRECCIA
Seite 19

Advertisement

Table of Contents
loading

This manual is also suitable for:

Ul-aircraft ltf-ul 2003

Table of Contents