CESSNA SECTION 7
MODEL T182T NAV III AIRPLANE AND SYSTEM DESCRIPTION
GFC 700 AFCS
U.S.
INSTRUMENT PANEL (Continued)
RIGHT PANEL LAYOUT
The Emergency Locator Transmitter (ELT) remote switch (ON/ARM/
TEST RESET) is positioned at the upper inboard corner of the right
panel adjacent to the MFD. Refer to Section 9, Supplements, for ELT
operating information.
The Hour (Hobbs) meter is found to the right of the ELT switch and
records engine operating time, when oil pressure is greater than 20
PSI, for maintenance purposes. Refer to the ENGINE INSTRUMENTS
description in this section for further information.
CENTER PEDESTAL LAYOUT
The center pedestal, located below the center panel, contains the
elevator and rudder trim control wheels, trim position indicators, cowl
flap control lever, 12V power outlet, aux audio input jack and a bracket
for the microphone. The fuel selector valve handle is located at the
base of the pedestal.
T182TPHBUS-00
7-13
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