SECTION 4 CESSNA
NORMAL PROCEDURES MODEL T182T NAV III
GFC 700 AFCS
U.S.
PREFLIGHT INSPECTION (Continued)
1 CABIN (Continued)
17. AVIONICS Switch (BUS 1) - OFF
18. AVIONICS Switch (BUS 2) - ON
19. Aft Avionics Fan - CHECK (verify fan is heard)
20. AVIONICS Switch (BUS 2) - OFF
21. PITOT HEAT Switch - ON (carefully check that pitot tube is
warm to the touch within 30 seconds)
22. PITOT HEAT Switch - OFF
23. Stall Warning System - CHECK (gently move the stall vane
upward and verify that the stall warning horn is heard)
24. LOW VOLTS Annunciator - CHECK (verify annunciator is
shown)
25. MASTER Switch (ALT and BAT) - OFF
26. Elevator and Rudder Trim Controls - TAKEOFF position
27. FUEL SELECTOR Valve - BOTH
28. ALT STATIC AIR Valve - OFF (push full in)
29. Oxygen Supply Pressure - CHECK
30. Oxygen Masks - CHECK
31. Fire Extinguisher - CHECK (verify gage pointer in green arc)
2 EMPENNAGE
1. Baggage Compartment Door - CHECK (lock with key)
2. Rudder Gust Lock (if installed) - REMOVE
3. Tail Tiedown - DISCONNECT
4. Control Surfaces - CHECK (freedom of movement and security)
5. Trim Tabs - CHECK (security)
6. Antennas - CHECK (security of attachment and general
condition)
3 RIGHT WING Trailing Edge
1. Flap - CHECK (security and condition)
2. Aileron - CHECK (freedom of movement and security)
(Continued Next Page)
T182TPHBUS-00
4-6
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