DA20-C1 Flight Manual
Normal Operating Procedures
Doc # DA202-C1 April 16, 2009 Page 4 - 7
Revision 24 DOT Approved
CAUTION
VISUALLY INSPECT FOR THE FOLLOWING CONDITIONS:
DEFECTS, CONTAMINATION, CRACKS, DELAMINATIONS,
EXCESSIVE PLAY, INSECURE OR IMPROPER MOUNTING
AND GENERAL CONDITION.
ADDITIONALLY, CHECK THE CONTROL SURFACES FOR
FREEDOM OF MOVEMENT.
CAUTION
SET PARKING BRAKE PRIOR TO REMOVING WHEEL
CHOCKS.
1. Left Main Landing Gear
a) Landing Gear Strut visual inspection
b) Wheel Fairing visual inspection
c) Tire Pressure (33 psi / 2.3 bar) check
d) Tire, Wheel, Brake visual inspection
e) Wheel Chocks remove
2. Left Wing
a) Entire Wing visual inspection
b) Stall Warning check (suck on opening)
c) Pitot-Static Probe clean, holes open
d) Tie down remove
e) Taxi and Landing Lights visual inspection
f) Wing Tip, Position Lights and Strobe visual inspection
g) Aileron Balancing Weight visual inspection
h) Aileron including Inspection Panel visual inspection
i) Wing Flap including Inspection Panel visual inspection
3. Fuselage
a) Skin visual inspection
b) Fuel Tank Vent check
c) Fuel Drains drain water
d) Structural Temperature Indicator check that structural
(for aircraft with other than white temperature does
Undersides) not exceed) 55º C
(131º F)
e) Maintenance Fuel Drains no leaks
f) Fuel Quantity visual inspection (use fuel
pipette)
g) Antennas visual inspection
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