Cessna SkyHawk SP 172S NAV III 2005 Pilot Operating Handbook page 217

CESSNA
MODEL 172S NAV III
SECTION 7
AIRPLANE AND SYSTEMS DESCRIPTION
INSTRUMENT PANEL
(Continued)
CENTER PANEL LAYOUT (Continued)
The standby instrument cluster is in the center instrument panel
below the GMA 1347 Audio Panel. A conventional (mechanical)
airspeed indicator and a sensitive aneroid altimeter are on each
side of the vacuum-powered attitude indicator. The pitot-static
instruments share the airplane pitot head and static ports with the
GDC 74A Air Data Computer. The attitude indicator features a low
vacuum IIflag" to provide immediate warning of vacuum system
failure.
The Bendix/King KAP 140 2 Axis Autopilot with Altitude Preselect is
found on the center panel below the standby instruments. A DC
electric powered turn coordinator, installed forward of the instrument
panel and not visible to the pilot, provides a roll rate signal to the
KAP 140. The KAP 140 receives NAV, HOG, and analog roll
steering inputs from the G1000 system. KAP 140 ROL, VS, and
ALT modes operate independently from the G1000. Refer to sectionl
9, Supplement 3 for operation of the BendiX/King KAP 140 2 Axis
Autopilot.
The engine controls are found on the lower center instrument panel
below the KAP 140 Autopilot (if installed). The controls arel
conventional push-pUll-type controls for throttle and mixture. See
\ ENGINE description in this section for operating information.
The Alternate Static Air valve is found adjacent to the throttle
control. Refer to the PITOT-STATIC SYSTEM AND INSTRUMENTS
description in this section for operating information.
The wing flap control and indicator is found at the lower right side of
the center panel. Refer to the WI NG FLAP SYSTEM description in
this section for operating information.
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172SPHAUS-03
U.S. 7-11