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FULL CHECK

1
MAKE SURE ALL SYSTEMS REQUIRED TO PERFORM THIS TEST ARE FUNCTIONAL.
Internal Leakage Check for the Right Hydraulic System - Empennage Flight Controls Figure 625 (Sheet 3)
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MAINTENANCE MANUAL

FULL CHECK
Internal Leakage Check for the Right Hydraulic System - Brake and Reserve Brake
Figure 626 (Sheet 1)

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STEP NO.  PROCEDURE  CHECK DONE WHEN  FLOW IN GPM  LEAKAGE CALC. NULL (+)  SEAL (-)  LEAKAGE APPROVED  COMPONENT/COMMENTS CORRECTIVE ACTION/BAD 
9  NANCE PAGE. MONITOR THE EICAS MAINTE- VALVE TO FIND WHICH ONE IS EXAMINE THE POSITION OF EACH MESSAGE WILL SHOW ON EICAS. SWITCH, A "RSV BRAKE VAL" POSITION OF THE RESERVE BRAKE VALVES DO NOT AGREE WITH THE SHUTOFF OR SUPPLY SHUTOFF IF THE ISOLATED ACMP PRESSURE BAD. 
10 TO THE OFF POSITION. SWITCH ON THE P1 PANEL PUT THE RESERVE BRAKE  THE RIGHT ACMP WILL STOP IN 1 SECOND. 

FULL CHECK Internal Leakage Check for the Right Hydraulic System - Brake and Reserve Brake Figure 626 (Sheet 2)
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 LEFT AND RIGHT SYSTEM ALTERNATING CURRENT MOTOR PUMP (ACMP) -
_____________________________________________________________ REMOVAL/INSTALLATION
____________________
 1.  General_______
　
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本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 液壓 CHAPTER 29 - HYDRAULIC POWER 1(172)