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cockpit for the comfort, convenience and safety of
the occupants.
OVERHEAD PANEL
The controls of most aircraft systems are located on
the overhead panel.
The overhead panel is divided into two main sections:
- a FWD section including the system panels.
- an AFT section mainly comprising the circuit
breaker panel.
GLARESHIELD
The Flight Control Unit (FCU), includes the Electronic
Flight Instrument System (EFIS) controls, and is used
for control and monitoring of the Auto Flight System
(AFS).
It is located on the glareshield.
The "Master Caution" and the "Master Warning" lights
are also located on the glareshield.
MAIN INSTRUMENT PANEL
Six interchangeable Cathode Ray Tubes are located on
the main instrument panel.
Two of them are dedicated to the ECAM.
The others are two Primary Flight Displays and two
Navigation Displays.
Stand-by instruments and landing gear controls are
also located on the main instrument panel.
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CENTER PEDESTAL
Several control panels are located on the center
pedestal as shown on the screen.
The mainly control panels are:
- thrust levers and thrust reverser levers,
- pitch trim wheels,
- flaps and slats control,
- brakes controls,
- MCDUs.
SIDE CONSOLES
The side sticks and nose wheel steering handles are
mounted on the side consoles.
The side consoles provide documentation stowage,
oxygen masks and communication devices.
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31 - INDICATING/RECORDING SYSTEMS
31-16-00 AVIONICS COMPARTMENT
CONTENTS:
Description
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AVIONICS COMPARTMENT
DESCRIPTION
The electronic avionics compartment is located below
the cockpit and cabin floors.
It includes:
- the electronic racks (90VU and 80VU),
- the weather radar shelf (109VU),
- the relay and contactor boxes (103VU and
107VU),
- the annunciator light test unit (70VU),
- AC and DC emergency power center (106VU).
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31-10-00 COCKPIT PHILOSOPHY
CONTENTS:
Philosophy
Push buttons
Indications
Color Philosophy
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COCKPIT PHILOSOPHY
PHILOSOPHY
All the aircraft and system controls are arranged to
be within easy reach of the two crew members. The
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