R EFF : 001-049, 101-105, 107-107, 151-199, 49-32-11Page 401 201-210, Config-2 Aug 01/05
CES Subtask 49-32-11-860-064
B. Aircraft Maintenance Configuration
(1)
Energize the ground service network
(Ref. TASK 24-42-00-861-001).
(2)
On the panel 25VU, make sure that the APU MASTER SW p/bsw is OFF.
(3)
Put a warning notice in the cockpit to tell persons not to start the APU.
(4)
Make sure that hydraulic systems are depressurized
(Ref. TASK 29-00-00-864-001).
(5)
Put the container below the Fuel Control Unit (FCU). Subtask 49-32-11-865-065
C.
Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
Subtask 49-32-11-010-057
D. Get Access
(1)
Put the access platform in position below the APU access doors 315AL and 316AR.
(2)
Open the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-010-001).
(3)
Set the LIGHT SW 11LJ to the ON position.
R EFF : 001-049, 101-105, 107-107, 151-199, 49-32-11Page 402 201-210, Config-2 Aug 01/05
CES 4. Procedure
_________
(Ref. Fig. 401/TASK 49-32-11-991-005) Subtask 49-32-11-020-054
A. Removal of the FCU
(1)
Disconnect the electrical connector (5) from the FCU solenoid.
(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Loosen the nut (1) and turn the plate (2) to release the union (3).
(4)
Disconnect the union (3) from the FCU (6).
(5)
Remove and discard the O-rings (4).
(6)
Loosen the captive bolts (12) and turn the plate (11) free from the pipes (10)
(7)
Disconnect the pipes (10) and (15) from the FCU.
(8)
Remove and discard the O-rings (9) and (14).
(9)
Loosen the clamp (8) and remove the FCU from the oil module.
(10)
Remove and discard the O-ring (7).
(11)
Put blanking plugs on the disconnected pipes (10), (15) and the FCU (6).
R EFF : 001-049, 101-105, 107-107, 151-199, 49-32-11Page 403 201-210, Config-2 Aug 01/05
CES
Fuel Control Unit
Figure 401/TASK 49-32-11-991-005
CES TASK 49-32-11-400-003
Installation of the Fuel Control Unit (FCU) (8022KM) (131-9(A))
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 03-002 GB DEF-STAN 91-101
LUBRICATING OIL TURBINE ENGINE SYNT BASE
(Ref. 20-31-00) Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
4 O-rings 49-32-09 01 -060 7 O-ring 49-32-09 01 -030 9 O-rings 49-21-09 05 -040 14 O-ring 49-21-09 05 -050
R EFF : 001-049, 101-105, 107-107, 151-199, 49-32-11Page 405 201-210, Config-2 Aug 01/05
CES
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
中國(guó)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(cè) AMM 機(jī)載輔助動(dòng)力 AIRBORNE AUXILIARY POWER4(46)
