TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 05 Inspection and Maintenance
Page 40
Issue: 04.APR 2016
Scheduled Inspection
(50 h)
100 h/
annual
as
specified
Wing attachment
Demount the wing root fairings.
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○
Visually check the condition of the wing root fairings for
cracks and other damage. Repair or replace, if necessary.
○
○
Check the torque and locking of the main wing spar bolts and
of the rear spar bolt with a torque wrench.
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○
Visually inspect all the connections at wing attachments.
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○
Check the attachment of the wings for play by moving the
wing forward and back, up and down.
○
Lubricate according to the lubrication plan Section
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○
Reinstall the wing root fairings only after the completion of
the inspection.
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○
Fuselage
Visually check the skin and the riveting. No deformities,
cracks or loosened rivets are allowed.
○
○
Visually check the rivets near the main landing gear legs.
○
Check the condition and the attachment of the antennas,
beacons and other external installations
○
○
Perform Major inspection according to
04-30-10.
2000h/
15years
Canopy
Visually check the canopy for cracks, scratches and other
damage. In case of crack detection contact TOMARK Aero for
instructions.
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○
Check the condition of all attachments of the canopy.
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○
Check the condition and movement of the canopy windows.
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Check the functioning of the gas springs.
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Check the condition of the canopy sealing.
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