TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 05 Inspection and Maintenance
Page 38 Issue: 04.APR 2016
Check park brake action. (brake lock must allow no slip of
aircraft at 100% max power)
Reinstall the main wheel fairings after the inspection of the
main landing gear is done.
Check tire pressure:
Main Landing Gear 2.2 bar
Visually check the condition of the wing skin and the
condition of the riveting. No deformations, cracks, or
loosened rivets are allowed.
Check the condition and attachment of the wing tip and
navigation lights.
Inspect wing internal for accumulation of water and/or
moisture.
Demount the inspection hatches and check the condition of
the control pull-push rods.
Check for torque of joints, jamming, excessive play and
excessive wear. Correct on condition.
Visually check the condition of the rivet joints and sealant of
the fuel tanks for tightness.
Check the connection, integrity, tightening and locking of the
fuel hoses. Visually check the area around the fuel meters and
the fuel hoses for tightness of the fuel system.
Check the connection of the fuel meters and the condition of
the electric cables.
Perform Major inspection according to
04-30-10.
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