CESSNA SECTION 7
MODEL 182T NAV
Ill AIRPLANE AND SYSTEMS DESCRIPTION
INSTRUMENT PANEL
(Continued)
PILOT PANEL LAYOUT
(Continued)
The circuit breaker panel is found along the lower edge of the pilot's
instrument panel below the electrical equipment switch panel and
pilot control wheel column. Each circuit breaker is identified for the
equipment or function it controls and for the bus from which it
receives power. Lighting for this sub-panel is controlled using the
SWICB PANELS dimmer control. See the ELECTRICAL
EQI-IIPMENT descriptions in this section for further information.
CENTER PANEL LAYOUT
The Garmin GMA 1347 Audio Panel is found on the upper half of
the center instrument panel (immediately to the right of the PFD). A
pushbutton switch labeled
"
DISPLAY BACKUP" to manually select
display reversion mode is found on the lower face of the GMA 1347.
Refer to the GMA 1347 Pilot's Guide for operating information.
The GDU 1040 Multifunction Display (MFD) is found on the upper
center panel to the right of the GMA 1347. The MFD depicts Engine
Indication System information along the left
slde of the d~splay and
shows navigation, terrain, lightning and traffic data on the moving
map. Flight management or display configuration information can be
shown on the MFD in place of the moving map pages. Refer to the
Garmin
G1OOOTM GPSIMFD Pilot's Guide for operating information.
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 "flag" to provide immediate warning of vacuum system
failure.
(Continued Next Page)
U.S. 7-11
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