R 52-41-00-410-002 Close the Avionics Compartment Doors after Access 22-66-34-991-002 Fig. 401
3. Job Set-up
__________
Subtask 22-66-34-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position at the access door 824 in zone 128.
(2)
Make sure that the access door 824 is open.
1EFF : ALL 1 22-66-34Page 404 1 1 Feb 01/02 1 1 1CES 1
Subtask 22-66-34-865-054
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 1CC1
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
FOR 1CC2 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
4. Procedure
_________
(Ref. Fig. 401/TASK 22-66-34-991-002)
Subtask 22-66-34-420-052
A. Installation of the FAC
NOTE : The procedure is the same for the FACS 1CC1 and 1CC2.
____
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Remove blanking caps from the electrical connectors (1).
(4)
Make sure that the electrical connectors are in the correct condition (1).
(5)
Install the FAC (5) on its rack (2).
(6)
Push the FAC (5) on its rack (2) to connect the electrical connectors (1).
(7) Engage the nuts (3) on the studs (4) and tighten. R CAUTION : MAKE SURE THAT THE OBRM(S) IS (ARE) CORRECTLY INSTALLED. IF
_______ R IT (THEY) IS(ARE) NOT INSTALLED CORRECTLY, PUSH THE OBRM(S) UNTIL THE LOCKING DEVICES ARE LOCKED.
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Subtask 22-66-34-865-055
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 1CC1 5CC1, 14CC1 FOR 1CC2 5CC2, 14CC2
Subtask 22-66-34-710-052
C. Do the Operational Test of the AFS (Ref. TASK 22-96-00-710-001). NOTE : If the aircraft is operated in CAT 3 conditions, you must also do
____ the test below: Land CAT 3 Capability Test (Ref. TASK 22-97-00-710-001).
NOTE : If you remove the FAC after this CFDS indication: AFS: YD ACTR
____ 3CC1(2), you must do the test with the hydraulic pressure available (Green for the FAC1, Yellow for the FAC2).
NOTE : As an alternative procedure, you can do this operational test
____
without the CFDS (Ref. TASK 22-62-00-710-001).
5. Close-up
________
Subtask 22-66-34-410-052
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) Close the access door 824, (Ref. TASK 52-41-00-410-002).
(3) Remove the access platform(s).
1EFF : ALL 1 22-66-34Page 406 1 1 Feb 01/02 1 1 1CES 1 ELECTRICAL AND HYDRAULIC POWER SUPPLY (FAC) - DESCRIPTION AND OPERATION
_______________________________________________________________________
1. Electrical Power Supply
_______________________
A. 28VDC Power Supply
(Ref. Fig. 001)
The FAC1 is supplied with 28VDC:
-
From the 28VDC ESS BUS 4PP through the 28VDC ESS BUS 801PP via 10A
circuit breaker 5CC1.
The FAC2 is supplied with 28VDC:
-
From the 28VDC BUS 2 2PP through the 28VDC BUS 2 206PP via 10A circuit
breaker 5CC2.
The 28VDC power supply generates:
-All the voltages associated with internal computation (+ 5VDC, + 15VDC and - 15VDC)
-The logic processing voltages (discretes, relays, etc.).
All these voltages derived from the 28V power are monitored by the FAC in
the command and monitoring channels.
B. 26V/400 Hz Power Supply (Ref. Fig. 002) The Rotary Variable Differential Transformers (RVDT) and the Linear Variable Differential Transformers (LVDT) associated with the FAC1 are supplied with 26V/400 Hz: 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM AUTO FLIGHT 自動飛行2(42)
