757 AMM 飞机维护手册液压 CHAPTER 29 - HYDRAULIC POWER 1(159)_航空信息_民用航空_通用航空

曝光台注意防骗网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

29-11-00
ALL ú ú 06 Page 680T ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
S 796-363
(17)
Do the Internal Leakage Check for the Right Hydraulic System - Brake and Reserve Brake (Fig. 626).

S 976-364

(18)
Right System Leakage Summary Sheet

(a) These are the conditions which you can use to make a decision about which components to replace. 1) If the leakage flow value of a rudder PCA is 2.0 GPM or
more, you must replace the PCA. 2) If the leakage flow valve of an elevator PCA is 1.0 GPM or more, you must replace the PCA.
3) If the total NULL leakage is more than 4.5 GPM, you must replace PCAs with high leakage until the total NULL leakage is less than 4.5 GPM.
(b) Use the summary sheet as follows:
1) For each component on the summary sheet, find the leakage flow value on the figure and step number shown below the component name.
2) Write the leakage flow values on the summary sheet opposite the component name as follows: a) If the leakage flow value is zero or a negative value,
write the value in the SEAL column. b) If the leakage flow value is a positive value, write the value in the NULL column. 3) Add the leakage flow values in the SEAL column and write the result in the space for the SEAL total.
4) If the SEAL total leakage or the NULL total leakage (Flow No. Fig. 624 Step 6) is 4.5 GPM or more, replace components with high leakage as necessary to decrease this leakage to less than 4.5 GPM.
(c) Right Leakage Summary Sheet ~............................................................
| Total Right System "Null" Leakage |
| [Flow No. Fig. 624 Step 6] ______ GPM |
| |
| Autopilot and Stab Trim "NULL" |
| ----------------------- |
| |
| Lateral and Pitch Autopilot |
| Null Leakage [Flow No. Fig.623 Step 5] ______ GPM |
| |
| Stab Trim Null Leakage |
| [Flow No. Fig. 634 Step 9] ______ GPM |
| |