TOMARK Viper SD-4 RTC - Page 34

TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 05 Inspection and Maintenance
Page 34 Issue: 04.APR 2016
Scheduled Inspection
(50 h)
100 h/
annual
as
specified
Inspect battery isolation provisions.
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Cabin Heat System
Inspect hoses for attachment, leaks and wear.
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Inspect air scoop at radiator for cleanness
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Inspect save closure of cabin air nozzles and vents
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Inspect heat exchanger on exhaust for cracks
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Engine Mount
Inspect engine mount attaching bolts at the firewall. Check
torque on all attachment points, re-torque as required.
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Inspect shock mount rubber elements (vibration isolators) for
condition.
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Check engine to shock mount attaching bolts, castle nuts and
cotter pins.
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Inspect engine mount structure for cracks and damage.
Pay specific attention to weld connections. In case of doubt
consider dye penetrant inspection.
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Visually check the firewall for cracks and corrosion, in
particular in the places of all the engine mount attachment
points.
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Unscrew and visually check the condition of the bolts
attaching the engine to the engine mount.
1000h
Perform Major engine mount inspection per 04-30-20.
2000h
Propeller
Remove spinner.
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Inspect spinner for cracks and fractures.
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Inspect propeller mounting bolts. Re-torque mounting bolts.
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First 25 hours of operation for new or overhauled engine