S 976-129
(19)
If Value No. 6 is less than -0.5 GPM, usually you must replace an aileron PCA because of high seal leakage.
S 976-130
(20)
If Value No. 6 is more than 0.5 GPM, usually you must replace an aileron PCA because of high null leakage.
S 976-131
(21)
If Value No. 6 is between the above limits, you can not make a decision about PCA replacement until you do the Full Hydraulic System Internal Leakage Check and Isolation of Components with High Leakage procedure.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-11-00
ALL ú ú 09 Page 638 ú Dec 20/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
S 976-132
(22) Subtract Value No. 2 from Value No. 1 and write the value, which is the empennage flight control null leakage, here:
Right Value No. 1
minus Value No. 2 = _______ GPM (Value No. 7)
S 976-133
(23)
If Value No. 7 is more than 1 GPM, usually you must replace a rudder or elevator PCA because of high null leakage.
S 976-134
(24)
If Value No. 7 is less than 1 GPM, you can not make a decision about PCA replacement until you do the Full Hydraulic System Internal Leakage Check and Isolation of Components with High Leakage procedure.
S 866-135
(25)
Move the R FLT CONTROL SHUTOFF switch on the P61 panel to the ON position.
S 866-136
(26)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P11 panel.
(a)
11C6, FLT CONT ELEC 1L AC
(b)
11C7, FLT CONT ELEC 1L DC
(c)
11C8, FLT CONT ELEC 2L AC
(d)
11C9, FLT CONT ELEC 2L DC
(e)
11G17, FLT CONT ELEC 1R AC
(f)
11G18, FLT CONT ELEC 1R DC
(g)
11G27, FLT CONT ELEC 2R AC
(h)
11G28, FLT CONT ELEC 2R DC
S 086-137
(27) Put the right hydraulic system back to its usual condition as follows:
(a) If you use the flowmeter technique, do these steps:
1) If you use an ACMP to the pressurize system, do these steps: a) Put the R HYD PUMPS ELEC pump switch to the OFF
position. b) Remove the flowmeter from the ACMP pressure line and connect the ACMP pressure line.
2) If you use the hydraulic service cart to pressurize the system, do these steps: a) Operate the hydraulic service cart to decrease the
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 液压 CHAPTER 29 - HYDRAULIC POWER 1(117)
