-
SECTION
7
CESSNA
-.
AIRPLANE AND SYSTEMS DESCRIPTION
MODEL
2088
(675
SHP)
INSTRUMENT PANEL
The instrument panel (see Figure
7-2)
is designed around the basic
"T"
-.
configuration. The gyros are located immediately in front of the pilot,
and arranged vertically. The airspeed indicator and altimeter are
,a.
located to the left and right of the gyros respectively. The remainder of
the flight instruments are located around the basic
"T".
Immediately to
,-
the left of the flight instruments are the clock, propeller anti-ice
ammeter, slaving accessory,
volt/ammeter selector switch, propeller
overspeed governor test switch, left fresh air vent pull knob,
left fresh
air vent outlet, and, microphone and headset jacks.
The lower left side of the instrument panel contains a switch panel
which has many of the switches necessary to operate the airplane
systems. Located directly above the flight instrument panel are the
annunciator panel, annunciator panel day-night switch, annunciator
panel test switch, and the fire detector test switch. Below the flight
instrument panel are the suction gage, inertial separator control,
lighting switch panel and the parking brake.
Avionics equipment is placed vertically in dual stacks approximately in
the center and just right of center of the instrument panel. Located
directly above the avionics stacks in the top center of the instrument
panel are the engine instruments consisting of the torque indicator,
propeller RPM indicator,
ITT indicator, Ng% RPM indicator, oil pressure1
oil temperature gauge, fuel flow indicator, and left and right fuel quantity
indicators. The cabin heat switch and control panel, and provisions for
air conditioning controls are located directly below the avionics stacks.
The right side of the instrument panel contains additional flight
instruments. Directly to the right of these instruments are the hour
meter (if installed), right fresh air vent pull knob, right fresh air vent,
right front passenger's microphone and headset jacks, and map
compartment.
A control pedestal, extending from the center of the instrument panel to
the floor, contains the emergency power lever, power lever, propeller
control lever, fuel condition lever, wing flap selector and position
indicator, elevator, rudder and aileron trim controls with position
indicators, the fuel shutoff valve control, cabin heat
firewall shutoff
valve control, and a microphone.
1
7-14
U.S.
(Continued Next Page)
Revision 23
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