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third audio control panel.
Only the last 2 h of recording are retained.
The CVR system consists of :
‐ a remote microphone behind the overhead panel
‐ a “hot mike” function, which records the crew members voice directly from their microphone, even
if the push to talk switch is not activated.
‐ a crashproof four-track recorder, equipped with an underwater locating beacon, in the aft section
of the aircraft
‐ a control panel on the overhead panel.
It is energized automatically :
‐ on the ground during the first 5 min after the aircraft electrical network is energized
‐ on the ground with one engine running
‐ in flight
On the ground, it is stopped automatically 5 min after the last engine shutdown provided the CVR
jack is not used.
On the ground, the crew can energize the CVR manually by pressing the GND CTL pushbutton.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
COCKPIT VOICE RECORDER - DESCRIPTION
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
COCKPIT VOICE RECORDER - CONTROLS
AND INDICATORS ON OVERHEAD PANEL
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CONTROLS AND INDICATORS ON OVERHEAD PANEL
Applicable to: ALL
(1) GND CTL switch (spring-loaded)
ON : The CVR, DFDR, and QAR �� are on.
The ON light comes on blue.
AUTO : The CVR, DFDR, and QAR �� are on, according to the logic. (Refer to
DSC-23-30-10 DESCRIPTION).
(2) CVR ERASE pushbutton
Pressed for
2 s
: This completely erases the tape, if :
The aircraft ‐ is on the ground, and
‐ The parking brake is on.
(3) CVR TEST pushbutton
Pressed and
held
: This activates the test, if the CVR is on (the GND CTL pushbutton pressed,
or during the first 5 min after energization of the aircraft electrical network),
and the parking brake is on.
Refer to STLO-SOP-06-A OVERHEAD PANEL - WHITE LIGHTS ON
OVERHEAD PANEL for additional information.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
COCKPIT VOICE RECORDER - CONTROLS
AND INDICATORS ON OVERHEAD PANEL
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
COCKPIT VOICE RECORDER - ELECTRICAL SUPPLY
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BUS EQUIPMENT LIST
Applicable to: ALL
NORM EMER ELEC
AC DC AC
ESS
DC
ESS HOT
COCKPIT VOICE CVR CTL SHED
RECORDER CVR SHED
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
COCKPIT VOICE RECORDER - ELECTRICAL SUPPLY
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
EMERGENCY LOCATOR TRANSMITTER - CONTROLS AND INDICATORS
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CONTROLS AND INDICATORS
Applicable to:
OVERHEAD PANEL
EXTERNAL POWER PANEL
(1) ELT switch
ON : The ELT transmits an emergency signal.
ARMED : In the case of impact, the Emergency Locator Transmitter (ELT) transmits
an emergency signal (on 121.5, 243 and 406.025 MHz).
TEST/RESET: Starts the ELT autotest.
Note: If the ELT is unduly triggered in ARMED mode (by an external impact, hard
landing, etc), select the TEST/RESET position to reset the ELT and stop signal
transmission.
(2) ON TEST and ELT lights
These lights come on amber either when the emergency signal is transmitted, or during ELT
autotest.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
EMERGENCY LOCATOR TRANSMITTER - CONTROLS AND INDICATORS
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
COMMUNICATIONS
ACARS - GENERAL
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INTRODUCTION
Applicable to:
The Aircraft Communication Addressing and Reporting System (ACARS) allows the direct exchange
of data between aircraft and airline ground computers via VHF 3.
Aircraft to ground messages (downlink) comprise operational, maintenance, monitoring, performance
and cabin data.
　
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