LEFT (PILOT SIDE) PANEL LAYOUT
The GDU 1040 Primary Flight Display (PFD), centered on the instrument
panel in front of the pilot, displays the primary ight instruments during normal
operation. During reversionary operation (MFD failure) or when the DISPLAY
BACKUP switch is selected, the Engine Indication Crew Alert System (EICAS)
is shown on the PFD. Refer to the Garmin G1000 Cockpit Reference Guide
(190-00645-XX) for specic operating information.
The standby instrument cluster is located on left portion of the pilot side
instrument panel. A conventional (mechanical type) airspeed indicator and a
sensitive aneroid altimeter are installed above and below the electric powered
attitude indicator. The standby pitot-static instruments share the left pitot-
static tube with the number 1 GDC 74A Air Data Computer. The standby
attitude indicator features a STBY PWR button, three LED lights, a PULL TO
CAGE knob, a gyro warning ag and a symbolic airplane adjustment knob.
The battery master switch is located on the lower left portion of the pilot
instrument panel. Located to the right of the master switch are switches for
the airplane electrical systems and equipment. Each switch is labeled for its
function and is ON when the switch handle is in the up position. Refer to the
Electrical Equipment descriptions in this section for further information.
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