B. Referenced Information
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REFERENCE DESIGNATION
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24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
29-24-00-864-001 Depressurize the Yellow Hydraulic System
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
34-10-00-860-004 IR Alignment Procedure
R 34-10-00-860-005 ADIRS Stop Procedure
3. Job Set-up
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Subtask 27-64-00-860-050
A. Aircraft Maintenance Configuration.
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001).
(3)
On the panel 114VU, make sure that the flap and the slat control lever is set to 0.
(4)
On the center pedestal, make sure that the SPEED BRAKE control lever is set to RET.
R (5) On the overhead panel 50VU, make sure that:
R - the HYD/LEAK MEASUREMENT VALVES/G, B and Y pushbutton switches are
R pushed (on these pushbutton switches the OFF legends are OFF).
(6) On the overhead panel 20VU, push the ADR1, ADR2, ADR3 pushbutton switches.
R R R (7) On the overhead panel 23VU, make sure that the FLT CTL/ELAC1 and FLT CTL/FAC1 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).
R R R (8) On the overhead panel 24VU, make sure that the FLT CTL/ELAC2 and FLT CTL/FAC2 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).
Subtask 27-64-00-010-056
B. Get Access
(1) Put the access platform in position at the door 822.
(2) Open the access door 822.
(3) On the battery power center 105VU: - loosen the two screws and remove the protective cover.
Subtask 27-64-00-865-050
C. Make sure that this(these) circuit breaker(s) is(are) closed:
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PANEL DESIGNATION IDENT. LOCATION
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49VU FLIGHT CONTROLS/SLT FLP/POS/IND 1 49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 49VU FLIGHT CONTROLS/FCDC1/SPLY 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 49VU AUTO FLT/FAC1/28VDC 49VU AUTO FLT/FAC1/26VAC 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 105VU FLT CTL/ELAC1/STBY SPLY 105VU FLT CTL/SEC1/STBY SPLY 105VU ELEC/HOT BUS/702PP SPLY 105VU ELEC/HOT BUS/701PP SPLY 105VU ELEC/HOT BUS/702PP SPLY 105VU ELEC/HOT BUS/701PP SPLY 121VU AUTO FLT/RUDDER/TRIM/IND 121VU AUTO FLT/FAC2/28VDC 1CN 15CE1 20CE1 19CE2 21CE1 6CV 5CV 5CC1 14CC1 16CE2 16CE1 22CE 5PB2 5PB1 12PB2 12PB1 15CC 5CC2 B12B11B10B09B08B07B06B04B03A02A01B01D02D01E02E01M20M19
1EFF : ALL 1 27-64-00Page 503
1 1 Nov 01/03 1 1 1CES 1
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU AUTO FLT/RUDDER/ARTF/FEEL 14CA N17 121VU AUTO FLT/STICK/LOCK 13CA N16 121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20 121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19 121VU FLIGHT CONTROLS/SLT FLP/POS/IND2 2CN P16 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
4. Procedure_________
Subtask 27-64-00-710-050
A. Do this test :
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱6(105)
