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Figure 21-63-01 SCH 01 P 0018 (Sheet 1/2) - Air Conditioning - Cockpit and Cabin Temperature Control - Sys 2 Signal Inputs and CTL On A/C FSN All

This document is a diagram and description of an aircraft air conditioning system. It shows the components of the system including the air conditioning system controller, temperature sensors, air packs, and control panels. The diagram identifies the connections between these different components that work together to control and monitor the cockpit and cabin temperatures.

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Sami Omran
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0% found this document useful (0 votes)
107 views1 page

Figure 21-63-01 SCH 01 P 0018 (Sheet 1/2) - Air Conditioning - Cockpit and Cabin Temperature Control - Sys 2 Signal Inputs and CTL On A/C FSN All

This document is a diagram and description of an aircraft air conditioning system. It shows the components of the system including the air conditioning system controller, temperature sensors, air packs, and control panels. The diagram identifies the connections between these different components that work together to control and monitor the cockpit and cabin temperatures.

Uploaded by

Sami Omran
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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4/24/2021 ASM - A318,A319,A320,A321 - LWA - Rev.

- Rev. num: 2 - 01-Feb-2021 - Figure 21-63-01 SCH 01 P 0018 (SHEET 1/2) - AIR CONDITIONING - COCKPIT AND CABIN TEMPERATURE CONTR…

B A B
A 92VU 91VU

HOT AIR

FAULT
94VU 93VU
OFF
A
I
PACK 2 R
96VU 95VU FAULT
C
OFF
A AIR CONDITIONING
O
N
SYSTEM CONTROLLER D
B
ACSC

A A
42 5
21-51
1
A SCH01
A 21-61 SCH01 2 A
401PP A 29 3 1 A 30VU AIR
28VDC 28 4 UNSD 2 A COND PANEL
ESS BUS 8
24-68 SCH08 58HH C/B SCH03 27 UNSD 7
21-51
AIR COND/TEMP/CTL/IND 41 30 6
A A SCH02 A
49VU
21-61 SCH01
21-21 SCH01
C 8LP BOARD 12LP BOARD
ANN LT TEST & INTFC ANN LT TEST & INTFC

GROUND FOR PRESSURE BETWEEN

GROUND FOR PRESSURE BETWEEN


70VU 70VU

BELOW 12PSIG AND ABOVE 60PSIG

BELOW 12PSIG AND ABOVE 60PSIG


33-14 SCH13 33-14 SCH19

OPEN CIRCUIT FOR PRESSURE

OPEN CIRCUIT FOR PRESSURE


3
UNSD 4 B
A A
AA
HOT AIR 10E A A
P/B OFF

12PSIG AND 60PSIG

12PSIG AND 60PSIG


AA 33-14 SCH19 8 FAULT 7
9 16HG RELAY
UNSD 6 OFF 4 FAN FAULT SUPPRESS
1WV1 SDAC-1 5 103VU
85VU A2 21-21 SCH01
31-54 SCH01 33-14 SCH19 A1 A3
D
UNSD B2

1HA2 BMC-2

1HA1 BMC-1

36-11 SCH01
36-11 SCH02
SCH03 B1 B3 14HK SCH02 / SCH03 A A F.O.
AA 1 A D A
HOT AIR 10E C2 UNSD 2 A UNSD C N
P/B OFF N.F.O.

96VU

95VU
AA UNSD C1 C3 A A A A

13B

13B
D2
1WV2 SDAC-2 UNSD D1 D3 4HU RELAY 6HV CROSSBLEED VALVE

AA

AA

AA

AA
86VU A A FAN FAULT 36-12 SCH01
31-54 SCH01 103VU
7HK P/BSW 21-23 SCH01
AIR COND/HOT AIR
2K UNSD

SCH03 30VU SCH03 SCH03


AB

AB
E
3E

6A

4K
8A

1B

1A

4J

2J

1J
BMC-1

CROSSBLEED VALVE
BMC-2

G&T FAN OFF


OVERHEAT

RECIRC.FAN LH OFF
RECIRC.FAN RH OFF
PIN PROG.

PIN PROG.
CIDS OPTION

SWITCH POS
HOT AIR
PARITY

WIRING DIAGRAM

21-63-04
L1+L2

21-63-05
21-63-06
F 21-63-07
31-54-61
57HH CONT 33-14-14
AIR COND SYSTEM 2 33-14-18
96VU 36-12-02
21-61 SCH01

N_SM_216301_S_010292__AD

Figure 21-63-01 SCH 01 P 0018 (SHEET 1/2) - AIR CONDITIONING - COCKPIT AND CABIN TEMPERATURE CONTROL - SYS 2 SIGNAL INPUTS
AND CTL
** ON A/C FSN ALL

1/1

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