TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 05 Inspection and Maintenance
Page 38
Issue: 04.APR 2016
Scheduled Inspection
(50 h)
100 h/
annual
as
specified
Finish
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
○
○
Wings
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.
2000h/
15years
