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ON
AUTO
(~ CVR ERASE pushbutton
Pressed for 2 seconds
(~) CVR TEST pushbutton
Pressed and held
The CVR, DFDR, and QAR <~ are on.
The ON light comes on blue.
The CVR, DFDR, and QAR <~ are on, according to the
logic. (See page 1).
This completely erases the tape, if ~
- The aircraft is on the ground, and
- The parking brake is on.
This activates the test, if the CVR is on (the GND CTL
pushbutton pressed, or during the first 5 minutes after
energization of the aircraft electrical network), and the
parking brake is on.
Refer to the FCOM 3.03.06, p. 2 for additional
information.
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━━━┓
┃I -~ A318 ┃COMMUNICATIONS ┃1.23.40 P 1 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 100 I ┃I REV 25 ┃
┃ A~7-~'M" A321 ┃ ACABS ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━━┻━━━━━┛
INTRODUCTION
The Aircraft Communication Adressing
exchange of data between aircraft and a
Aircraft to ground messages (downlink)
performance and cabin data.
and Reporting System (ACABS) allows direct
rline ground computer through the VHF 3.
comprise operational, maintenance, monitoring,
Ground to aircraft messages (uplink) contain crew information (wind for example) or might
request for transmission of data which are sent automatically or by crew action.
Automatic downlink of reports is carried out by ACABS Management Unit [MU), which is
programmed according to airline needs (Buyer Furnishing Equipment).
Due to the highly customized programming, the ACABS functions may vary for different
airlines and therefore are not described in detail.
SYSTEM ARCHITECTURE
The ACARS system consists of a Management Unit (MU) connected to the following
elements ~
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.23.40 P 2 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I ~-~ A318 ┃I COMMUNICATACARS ┃SEQ 100 1 ┃I REV 25 ┃
┃ aw aw ,, ~L,~ .4319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual2(140)
