(7)
Apply HYDRAULIC FLUIDS (Material No. 02-003) to the threads of the
pipe end-fittings.
(8)
Connect the pipe (25) to the union (27).
(9)
TORQUE the pipe end-fitting (26) to between 9.7 and 10.7 m.daN (71.53 and 78.90 lbf.ft).
(10)
Connect the pipe (21) to the union (23).
(11)
TORQUE the pipe end-fitting (22) to between 2.9 and 3.2 m.daN (21.38 and 23.59 lbf.ft).
(12)
Install the pipe (17) between the union (19) and the filter 2584GM.
(13)
TORQUE the pipe end-fittings (18),(54) to between 5.4 and 5.9 m.daN
(39.82 and 43.51 lbf.ft).
(14)
Connect the pipe (1) to the union (3).
(15)
TORQUE the pipe end-fitting (2) to between 7.5 and 8.3 m.daN (55.30 and 61.20 lbf.ft).
(16)
Install the pipe (32) between the union (43) and the check valve 1093GM.
(17)
TORQUE the pipe end-fittings (33),(42) to between 9.7 and 10.7 m.daN
(71.53 and 78.90 lbf.ft).
(18)
Install the pipe (7) between the unions (9),(41).
(19)
TORQUE the pipe end-fittings (8),(40) to between 9.7 and 10.7 m.daN
(71.53 and 78.90 lbf.ft).
(20)
TORQUE the nuts (11) to between 0.7 and 0.8 m.daN (61.94 and 70.79 lbf.in).
(21)
Connect the bonding jumper (51) to the structural attachment (52). Install the bolt (49), the washer (50) and the nut (53).
(22)
Tighten the nut (53).
(23)
Seal the connections of the bonding jumper (51) with SEALANTS (Material No. 09-013).
(24)
Apply STRUCTURE PAINTS (Material No. 16-003) (dyed blue) to the sealant.
R 1EFF : 059-099, 102-149, 151-199, 201-299, 1 29-11-15Page 420 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(25)
Remove the blanking caps from the electrical connections.
(26)
Make sure that the electrical connectors are clean and in the correct condition.
(27)
Connect the electrical connectors (29),(36) to the receptacles on the manifold (35).
**ON A/C ALL
Subtask 29-11-15-865-052
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1701GK, 1702GK.
Subtask 29-11-15-860-054
D. Preparation for Test
(1)
Connect the isolation coupling of the PTU (Ref. TASK 29-23-00-860-002).
(2)
Pressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-002).
Subtask 29-11-15-710-050
E. Test
(1)
Do the operational test of the PTU (Ref. TASK 29-23-00-710-003).
(2)
During the operational test examine the connections of the manifold
(35) and make sure that there are no leaks.
5. Close-up
________ Subtask 29-11-15-860-055
A. Put the aircraft back to the serviceable condition.
(1)
Remove the container from below the manifold.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
1EFF : ALL 1 29-11-15Page 421 1 1 May 01/05R 1 1 1CES 1
(3)
Remove the access platform(s).
(4)
Close the main doors of the main gear (Ref. TASK 32-12-00-410-001).
(5)
Remove the warning notice(s).
PRESSURE SWITCH - ENGINE PUMP (1074GK) - REMOVAL/INSTALLATION
_____________________________________________________________
TASK 29-11-17-000-041
Removal of the Engine-Pump Pressure Switch (1074GK)
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS FOR A SHORT TIME AFTER
_______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC
_______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) R No specific protective covers No specific warning notice(s)
中國(guó)航空網(wǎng) www.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 HYDRAULIC POWER 液壓2(28)
