—
SECTION 4
CESSNA
_
NORMAL PROCEDURES
MODEL 172S NAV III
PREFUGHT INSPECTION (Continued)
-
0 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.
LOW VOLTS Annunciator - CHECK (Verify annunciator is
shown)
24.
MASTER Switch (ALT and BAT)-OFF
—
25.
Elevator Trim Control - TAKEOFF position
26.
FUEL SELECTOR Valve - BOTH
|
27.
ALT STATIC AIR Valve-OFF (push full in)
—
28.
Fire Extinguisher - CHECK (Verify gage pointer in green
arc).
@ EMPENNAGE
—
1.
Baggage Door - CHECK (lock with key)
2.
Autopilot Static Source (if installed) - CHECK (Verify opening
is clear)
—
3.
Rudder Gust Lock (if installed) - REMOVE
4.
Tail Tiedown-DISCONNECT
n
5.
Control
Surfaces
-
CHECK
freedom
of
movement
and
security
6.
Elevator Trim Tab - CHECK security
—
7.
Antennas - CHECK for security of attachment and general
condition
@ RIGHT WING Trailing Edge
—
1.
Flap - CHECK for security and condition
2.
Aileron - CHECK freedom of movement and security
(Continued Next Page)
14-8
U.S.
172SPHAUS-04
—