Zlin Aviation
Section 1
Maintenance Manual Aircraft Maintenance Manual
Issued: 01/02/2006
QAP-AMM-Rev02
Date of latest Revision: 23/01/2013
Page Number: 1-24
Landing gear
Level of
certification
Check tire condition and pressures. Check wheel fairing if installed
Owner
Check landing gear structures, attachments, bolts, for condition and correct torque.
Check oil fitting on the brake pumps for leakages. Check wheels for status and axle
bolt.
Owner
Check bungee cords conditions
Owner
Check telescope safety wires.
Owner
Check AOSS system assembly if present (follow AOSS manual)
Owner
Controls-Seats-Seat belts
Level of
certification
1
Check aileron wires, pulleys, and turnbuckles for integrity, security and
correct tension. Check the connection between the two ailerons cables, positioned
behind the second seating. Check the vertical arm welded on the torque tube, and the
bolt and castle nut (and pin) used to connect together the two mentioned ailerons
cables.
Check that all the wire cables are correctly working inside the pulley and that have
not slipped outside of it. Refer to chapter 2.3.2.1 STEEL WIRE CABLES AND
PULLEYS
Owner
2
Check aileron wires upper joins and pulleys. Check that all the wire cables are
correctly working inside the pulley and that have not slipped outside of it
Owner
3
Check aileron wires lower joins and pulleys. Check that all the wire cables are
correctly working inside the pulley and that have not slipped outside of it
Owner
4
Check flap cable and bungee. Pins and cotter pins. Check all the line of
control cable from the flap lever to the bungees. Test the normal operation of the flap
system using the flap lever.
Owner
5
Check the pedals. Rod connections (nr.04) between pedals, bolts, nuts and
pins. Check the spring below the main seating, connected to the rear pedals. Check
the turnbuckles of the rudder cables, pulleys and cables for condition.
Check the correct assembling of the brake pumps. Check for oil leaking.
Owner
6
Check the sticks, rod connections, bolts, castles nuts and pins. Check the
correct movements of the whole system. Control the universal hinge (two stainless
steel U profiles) connecting the horizontal aluminium push pull tube coming from the
torque tube, to the elevator aluminium push pull tube below the baggage
compartment. Control the bolts (nr. 03) that are connecting all the mentioned system
(universal joint). Check the connections (bolts, joints and nuts) of the whole push pull
tubes inside the fuselage up to the elevators.
Owner
7
Check throttle assembly, bolts, connecting rod, cables, and smooth operation.
Owner
8
Check for seats belts integrity and connecting bolts.
Owner
9
Check the seats (structure integrity, connections bolts, cleaning)
Owner
10
Check the trim lever for security. Check the correct operation of the trim
system
Owner
