Calidus
NORMAL PROCEDURES
AutoGyro_POH_Calidus Revision 4.0 – Issue Date 17.JAN.2019 4-3
Station 3 (keel tube and propeller)
ʘ Keel tube protection pad ...................................................... No excessive wear
Propeller condition and cleanliness .......................................................... Check
Propeller leading edge and tips........................................................No damage
Spinner (if installed) .................................................................. Tight, no cracks
Variable pitch propeller (if installed): brushes........................................... Check
Variable pitch propeller (if installed): edge strips ...................................... Check
Station 4 (engine, LH side)
ʘ Main frame rear side / welded joints.......................... No cracks, no deformation
Oil cooler and hoses LH......................................... Clean, no leaks, fittings tight
Exhaust system LH............................................................................ No cracks
Engine cowling LH .................................. Properly installed, all fasteners locked
Station 5 (main gear spring spar, LH)
LH Main wheel running surface................................................................ Check
Air pressure and slip mark ............................................................. Visual check
ʘ Brake, disc attachment (4 bolts) and wheel attachment............................ Check
Wheel spat and attachment ..................................................................... Check
ʘ Main gear spring spar attachment............................................................ Check
Main gear spring spar ........................................................................ No cracks
Vibration decoupling element attachment (2x).......................................... Check
Rotor flight control............................................... No excessive play and secure
ʘ Teeter bolt (bolt end)........................................................................ Free to turn
Teeter bolt (nut end) ................................................................Split pin installed
Station 6 (passenger station, LH side)
Aft canopy hinge .....................................................................................Secure
Station 7 (pilot station, LH side)
Forward canopy hinge ............................................................................ Secure
Canopy sliding window and frame........................................... Check, no cracks
Static port ................................................................................. Clean and open
Station 8 (forward fuselage and canopy)
General appearance .....................................................................................OK
Pitot cover (if installed)........................................................................ Removed
Pitot tube .................................................................................. Clean and open
Rotor lash bag (if sufficient brake pressure) ........................................ Removed
Canopy condition and cleanliness........................................... Check, no cracks
ʘ Nose wheel condition and air pressure..................................................... Check
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