TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 05 Inspection and Maintenance
Issue: 04.APR 2016
Page 43
Scheduled Inspection
(50 h)
100 h/
annual
as
specified
Visually check the upholstering of the seats and of the cockpit
area.
○
○
Check the condition of the seats for cracks in the structure.
○
Visually check the condition and anchoring of the harness.
○
○
Front and aft fuselage cross spar
Visually check the condition of the wing box. Deformations,
cracks, loosened rivets and other damage are not allowed. Pay
specific attention to wing spar attachment areas.
○
Visually check the condition of the aft fuselage spars.
Deformations, cracks, loosened rivets and other damage are
not allowed. Pay specific attention to wing spar attachment
areas.
○
Control systems
Flap Actuation System
Check for condition and proper, smooth operation through
full travel. Check for free movement.
○
○
Lubricate bearings as required
○
Visually check the attachment, torque and locking of the
electric flap drive in fuselage.
○
Check condition of the flap control transmission in wing and
fuselage. Check push rods for condition and security. No gap
to the rod ends. Check rivets for security of attachment.
○
Check deflections. Nominal values:
15⁰ ± 2⁰
30⁰ ± 2⁰
40⁰ ± 2⁰
500h/
5 years
Visually check in fuselage the rivets connecting the torsion
tube with the fitting for the wing quick connect. (3 rivets each
left and right must be tight and no cracks in tube - use mirror
and operate flap)
500h/
5 years
