TASK 29-13-49-400-007
 Installation of the Check Valve Restrictor Tubes (for Engine 2 1000EM2)
 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
__________________
 This task is effective post SB RA32178-1 This task is for the installation of the check valve restrictor tubes for engine 2 1000EM2. For the installation of the check valve restrictor tubes for engine 1 1000EM1 (Ref.Task 29-11-49-000-00700).
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice(s)
 No specific wrench
 No specific access platform 0.8 m (2 ft. 7 in.)

R No specific Torque Wrench : range 5.00 to 35.00 lbf.in R (0.05 to 0.40 m.daN) No specific Torque Wrench : range 36.00 to 220.00 lbf.in
 (0.40 to 2.60 m.daN)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
 after Operation of the PTU 71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 29-13-49-991-913 Fig. 410
 3. Job Set-up
__________
 Subtask 29-13-49-860-082
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the Yellow hydraulic system is depressurized (Ref. TASK 29-23-00-864-001).

 (2)
 Make sure that the Yellow hydraulic reservoir is depressurized (Ref. TASK 29-14-00-614-001).

 (3)
 Make sure that the warning notice(s) is (are) in position to tell persons not to pressurize the Yellow hydraulic system: - on the ground service panel 198CB.

 (4)
 Make sure that the warning notice(s) is (are) in position on the access door 195BB to tell persons not to pressurize the Yellow hydraulic reservoir.

 Subtask 29-13-49-941-082
 B. Safety Precautions
 (1)
 On the center pedestal, on the ENG panel 115VU:

 -make sure that the warning notice(s) is (are) in position to tell persons not to start the engine 2.

 (2)
 Make sure that the engine 2 shutdown occurred not less than 5 minutes before you do this procedure.

 (3)
 Make sure that the warning notice(s) is (are) in position to tell persons not to pressurize the Yellow hydraulic system:

 -in the cockpit, on the HYD section of the overhead panel 40VU.

 (4)
 On the overhead maintenance panel 50VU:

 -make sure that the ON legend of the ENG/FADEC GND PWR/2 pushbutton switch is off.

 (5)
 Make sure that the warning notice(s) is (are) in position to tell persons not to energize the FADEC 2.

 Subtask 29-13-49-865-064
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU HYDRAULIC/Y HYD/PUMP ENG2/MONG 3700GD Q37
 Subtask 29-13-49-010-070
 D. Get Access
 (1)
 Make sure that the fan-cowl doors are open:

 -447AL, 448AR (Ref. TASK 71-13-00-010-040).

 (2)
 Make sure that the access door 195BB is open.

 (3)
 Make sure that the access platform is in position at the engine.

 4. Procedure
_________
 (Ref. Fig. 410/TASK 29-13-49-991-913) Subtask 29-13-49-420-070
 A. Installation of the Check Valve Restrictor Tubes
 (1)
 Connect the tube (30) to the HCU. Do not torque the coupling nut at this time.

 (2)
 Put the clamps (10) on the tube (30). Install the bolts (5), washers

 (20) and nuts (25) that attach the clamps to the engine brackets at the flange STA199 (A2). (3 locations). Do not torque the nuts at this time.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM HYDRAULIC POWER 液壓4(84)