R **ON A/C 401-499,
R 2XA P/BSW-ELEC/GALLEY 35VU 210 831 24-26-00 R 2XB CNTOR-STAT INV 105VU 126 822 24-28-55 R 3XB STAT INV 126 822 24-28-51 R 3XC CNTOR-AC ESS BUS SWITCHING 106VU 125 812 24-25-55 R 11XC P/BSW-ELEC/AC ESS FEED 35VU 210 831 24-25-00 R 1XE CONTROL UNIT-CSM/G 125 812 24-24-34 R 8XE CSM/G 148 734 24-24-51 R 14XE ANN-EMER ELEC PWR/RAT/&/EMER GEN 21VU 211 831 24-24-00 R 15XE CNTOR-AC ESS BUS SWITCHING 106VU 125 812 24-24-55 R 23XE P/BSW-EMER ELEC PWR/EMER GEN TEST 21VU 211 831 24-24-00 R 24XE P/BSW-EMER ELEC PWR/MAN ON 21VU 211 831 24-24-00 R 24XG GAPCU 92VU 122 24-41-00 R 2XS P/BSW-ELEC/APU GEN 35VU 210 831 24-23-00 R 3XS GLC-APU 120VU 212 831 24-23-55 R 8XS GEN-APU 310 24-23-51 R 42XS CT-AC, APU GEN 120VU 212 831 24-23-00 R 5XT P/BSW-ELEC/IDG 1 35VU 210 831 24-21-00 R 6XT P/BSW-ELEC/IDG 2 35VU 210 831 24-21-00 R 1XU1 GCU-1 91VU 121 811 24-22-34 R 1XU2 GCU-2 91VU 121 811 24-22-34 R 3XU1 P/BSW-ELEC/GEN 1 35VU 210 831 24-22-00 R 3XU2 P/BSW-ELEC/GEN 2 35VU 210 831 24-22-00 R 9XU1 GLC-1 120VU 212 831 24-22-55 R 9XU2 GLC-2 120VU 212 831 24-22-55 R 11XU1 BTC-1 120VU 212 831 24-22-55 R 11XU2 BTC-2 120VU 212 831 24-22-55 R 13XU P/BSW-EMER ELEC PWR/SMOKE DRILL 21VU 211 831 24-22-00 R 41XU1 CT-AC, 1 131 831 24-22-00 R 41XU2 CT-AC, 2 133 831 24-22-00 R 50XU1 SENSOR-TDC AC, 1 103VU 126 822 24-22-18 R 50XU2 SENSOR-TDC AC, 2 103VU 126 822 24-22-18
-------------------------------------------------------------------------------
FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
-------------------------------------------------------------------------------R 51XU1 CT 212 24-21-00 R 51XU2 CT 212 24-21-00 R 4000XU IDG 430 24-21-51
R **ON A/C ALL
-------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA I I I I DOOR I REF.
-------------------------------------------------------------------------------5XB HOLDER-FUSE 105VU 126 822 24-28-00 5XB1 FUSE-AC STAT INV BUS SPLY 105VU 126 822 24-28-00 2XE GLC-EMER 106VU 125 812 24-24-55
A. Spare Fuse
(Ref. Fig. 003)
If fuse 5XB1 melts, you can replace it by a spare 80A fuse which is on
the left side panel, in the cockpit.
Spare Fuse - Component Location
Figure 003
1EFF : ALL 1 24-20-00 Page 8
1 1 Aug 01/05
1 1
1CES 1
AC GENERATION - DEACTIVATION/REACTIVATION
_________________________________________
TASK 24-20-00-040-002
RAT Extension Control - Check of the RAT Manual Extension
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______
OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
__________________
Refer to the MMEL TASK: 24-20-06
AC Generation - RAT Extension Control
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notices
No specific access platform 1.8 m (5 ft. 11 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 R 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground R Power Supply
29-10-00-864-003 Depressurize the Blue Hydraulic System -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
**ON A/C 001-049, 051-061, 101-102, 201-202,
24-20-00-991-001 Fig. 401 R **ON A/C 062-099, 103-149, 151-199, 203-299, 301-399, 401-499,
24-20-00-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 24-20-00-860-053
A. Aircraft Maintenance Configuration
(1)
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM ELECTRICAL POWER 電源1(40)
