Section 4
Normal Procedures
PILOT’S OPERATING HANDBOOK
4-6
2015-07-20
Doc. No. POH-20101308
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condition of rudder and elevator attachment
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freedom of rudder and elevator movement
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condition of trim tab, condition and security of elevator trim tab control
rods
8. Rear part of fuselage - check
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surface condition
9. Right wing flap- see 5
10. Right aileron- see 4, except trim tab
11. Right wing tip - see 3
12. Right wing - see 2 - except the landing light and Pitot tube
13. Right landing gear leg - see 1
14. Front part of the fuselage - right hand side - check
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tilting canopy attachment and condition
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condition and attachment of GPS antenna
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condition and cleanness of air intakes
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condition of the nose landing gear leg and nose wheel
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condition of the nose wheel control rods
15. Engine
Checks before the first flight of day - it is necessary to remove upper engine
cowling:
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condition of engine bed
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condition of engine attachment
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condition of exhaust system
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condition of engine cowlings
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visual check on fuel and electrical system condition
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check on cooling liquid volume in the expansion tank on the engine body
(replenish as required up to max. 2/3 of the expansion tank volume)
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check on cooling liquid level in the overflow bottle (volume should be
approx. 0.42 pints (0.2 liter))
Checks before every flight:
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cleanness of air intakes
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check on oil level (between marks - flattening on the dip stick; difference
between min. – max. marks is 0.5 l)
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proper closing of the upper engine cowling
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