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Lavatory Switch Panel............................................................... 7-28
Lighting Control Unit (LCU) .................................................... 7-28
Passenger Interface Unit (PIU)................................................. 7-28
Master Control Unit (MCU) ..................................................... 7-28
Operation......................................................................................... 7-28
Cabin Management System Equipment/ Circuit Breaker Locations
(Typical) (Figure 7-10) ..................................................................... 7-29
Flight Phone ................................................................................ 7-30
Digital Airborne Telephone (Optional)................................... 7-30
AC Electrical Outlets (Optional) .............................................. 7-30
Window Shades.......................................................................... 7-30
Gasper Outlets ............................................................................ 7-30
Aft Cabin Stowage Compartment ........................................... 7-31
Lavatory/Vanity......................................................................... 7-31
Lavatory/Vanity (Typical) (Figure 7-11) .......................................... 7-32
Toilet............................................................................................. 7-33
Pilot’s Manual
PM-132A 7-1
COCKPIT DESCRIPTION
The cockpit (Figure 7-1) is configured in a standard side-by-side seating
arrangement with a center pedestal mounted between the seats. The
instrument panel is installed with an 18° forward cant which provides
an ergonomic view of the panel by either crew member. The throttle
quadrant is located between the center pedestal and the instrument
panel. The instrument panel, center pedestal and throttle quadrant are
easily accessible by both pilots.
The dual primary flight controls consist of a textured surface control
wheel mounted to a control column and an adjustable set of rudder
pedals. The control wheel and column operate with the normal pushpull
(pitch) and left/right rotation (roll) input commands. The control
wheels have a trim switch, microphone switch and a Control Wheel
Master Switch (MSW) installed on the outboard side of the wheel. A
checklist line advance switch, a transponder switch and a Touch Control
Steering (TCS) switch are installed on the inboard side of the control
wheels. The pilot’s control wheel is equipped with an aileron (roll)
disconnect lever. Each control column is equipped with an approach
plate holder that will secure an entire approach plate booklet. An
illuminated approach plate holder is available as an option. The left
and right rudder pedals provide yaw control during flight and are
electrically adjustable fore/aft for different sized pilots. The rudder
pedals also control nose wheel steering and braking while the wheels
are on the ground.
Secondary flight controls and thrust levers are mounted on the throttle
quadrant at the forward side of the pedestal. The elevator disconnect
handle, emergency gear freefall lever, flap control lever, emergency/
parking brake handle and spoiler control handle are all located in the
throttle quadrant. The system test control switch, pitch trim bias
switch, radio control hot bus switch, rudder boost switch and clearance
delivery radio are located at the forward end of the quadrant. Switches
for the enhanced ground proximity warning system are installed aft of
the clearance delivery radio. The Multi-Function Display (MFD) joystick
is located in the quadrant, aft of the thrust levers.
SECTION VII
INTERIOR EQUIPMENT
Pilot’s Manual
7-2 PM-132A
The instrument panel consists of three major horizontal tiers of
instruments and controls. Within each tier, the controls for each system
are grouped together on a separate panel and/or display. The
glareshield panels (upper tier) provide controls for operating the flight
director/autopilot and for managing information displayed on the
Primary Flight Displays (PFDs), Multi-Function Display (MFD) and
Engine Indicating and Crew Alerting System (EICAS) display. The
main instrument panel (middle tier) provides visual displays and controls
for communication/navigation, engine management and electronic
flight instrument systems management. The subpanel (lower
tier) provides control for several aircraft systems and for control of the
lights and landing gear.
The upper tier (glareshield panel) is located immediately below the
glareshield. It consists of the integrated flight guidance controller and
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