(2)
TORQUE the 3 captive screws (1) to between 4.43 and 6.20 lbf.in (0.05 and 0.07 m.daN).
Subtask 24-52-55-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3PC, 1XC, 2XC, 7XE, 4PE, 6XE, 1XH Subtask 24-52-55-710-050
C. Test of the AC Shed Essential Bus Contactor
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
(3)
Make sure that the AC SHED ESS BUS OFF warning does not come into view.
(4)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(5)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
5. Close-up
________ Subtask 24-52-55-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
In the avionics compartment, close the access panels of the AC/DC emergency power center 106VU and the BATTERY power center 105VU.
(3)
Close the access doors 812 and 822.
(4)
Remove the access platform(s).
GALLEY SUPPLY - DESCRIPTION AND OPERATION_________________________________________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
1. General_______
R The power supply provides the galleys with 115 V AC. There are 50 KVA
R available for all galleys. This power is divided into two parts, the AFT
R galley power with 30 KVA and the FWD galley power with 20 KVA. The galleys
R are electrically connected with cable lugs to the aircraft terminal blocks.
**ON A/C 301-399,
1. General_______
R The power supply provides the galleys with 115 V AC. There are 70 KVA
R available for all galleys. This power is divided into two parts, the AFT
R galley power with 30 KVA or 45 KVA and the FWD galley power with 40 KVA or
R 25 KVA. The galleys are electrically connected with cable lugs to the
R aircraft terminal blocks.
R **ON A/C 001-049, 101-149, 151-199, 211-299, 301-399, 401-499,
2. Component Location__________________
R (Ref. Fig. 001)
R -------------------------------------------------------------------------------
R FIN I FUNCTIONAL DESIGNATION I PANEL I ZONE I ACCESS
R I I I I DOOR
R -------------------------------------------------------------------------------
R 4MC CONTACTOR 220
R 5MC CONTACTOR 220
R 6MC CONTACTOR 220
R 13MC CONTACTOR 220
R 15MC CONTACTOR 220
R 17MC CONTACTOR 220
R 6475MM GALLEY (LOC.I) 222
R 6478MM GALLEY (LOC.II) 222
R 6483MM GALLEY (LOC.V) 262
R R Galley Supply - Component Location Figure 001 (SHEET 1)
1EFF : 1 1 1CES ALL 1 111 24-56-00 Page 2 Aug 01/05
R R Galley Supply - Component Location Figure 001 (SHEET 2)
R 1EFF : 1 1 1CES ALL 1 111 24-56-00 Page 3 Aug 01/05
**ON A/C 051-099, 201-210,
R 2. Component Location__________________ (Ref. Fig. 001)
R R R R -------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANEL I ZONE I ACCESS I I I I DOOR -------------------------------------------------------------------------------
R 4MC CONTACTOR 220
R 5MC CONTACTOR 220
R 6MC CONTACTOR 220
R 13MC CONTACTOR 220
R 15MC CONTACTOR 220
R 17MC CONTACTOR 220
R 6475MM GALLEY (LOC.I) 222
R 6483MM GALLEY (LOC.V) 262
R
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
3. System Description__________________
R **ON A/C 001-049, 101-149, 151-199, 211-299, 401-499,
R (Ref. Fig. 002)
R **ON A/C 051-099, 201-210,
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM ELECTRICAL POWER 电源2(126)