(b)  
Read the amperage or the flow value and write it on the data sheet for step 16.

 (c)  
Put the yaw damper switch (on the P5 panel) in the OFF position.

 S 796-100
 (25) Do these steps to find the leakage of the feel computer for the elevator:
 (a)  
Open the No. 4 isolation valve (in the tail compartment).

 (b)  
Read the amperage or the flow value and write it on the data sheet for step 17.

 S 796-101
 (26) Do these steps to find the leakage of the right thrust reverser:
 (a)  Extend the right thrust reverser (AMM 78-31-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 29-00-00
 ALL  ú ú 01 Page 630 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (b)  Remove hydraulic power from system B (AMM 29-15-00/201).
 (c)  Move the reverse thrust lever forward and down.
 (d)  Wait at least 15 seconds but no more than 90 seconds and supply
 hydraulic power to system B (AMM 29-15-00/201).
 NOTE:____ The thrust reverser will now stow but the control valve
 will be timed out and remain open.

 (e)  
Wait 25 to 30 seconds and record the amperage or the flow value on the data sheet for step 18.

 (f)  
Cycle the thrust reverser to reset the control valve.

 S 866-102
 (27)
 Remove hydraulic power from system B (AMM 29-15-00/201).

 S 866-103

 (28)
 Put the FLT CONTROL B switch in the OFF position.

 S 486-104

 (29)
 Connect the equipment that is necessary to measure the flow to hydraulic system A.

 S 866-105
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES. THE AILERONS, RUDDER, ELEVATOR, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (30)
 Supply hydraulic power to system A.

 S 216-106

 (31)
 Make sure the pressure in system A is a minimum of 2800 psi.

 S 976-247

 (32)
 If you use the ammeter or amp-clamp method do this step:

 NOTE: This amperage is the System A Basic Current, and must
____ be subtracted from all other system A amperage readings before you use Fig. 603 to find the equivalent flow.
 (a) Read the amperage and write it on the data sheet for step 19.
 NOTE: Write down a flow value of zero for step 19.
____
 S 976-248
 (33) If you use the flow meter method, read the flow value and write it on the data sheet for step 19.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 29-00-00
 ALL  ú ú 01 Page 631 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 796-108
 (34) Do these steps to find the leakage of spoilers No. 3 and No. 6 when they are retracted:
 (a)  
Put the SPOILER A switch in the ON position.

 (b)  
Read the amperage or the flow value and write it on the data sheet for step 20.

 S 796-109
 (35) Do these steps to find the null leakage of spoiler No. 6:
 (a)  
Turn the control wheel approximately 40 degrees clockwise.

 (b)  
Read the amperage or the flow value and write it on the data sheet for step 21.

 S 796-110
 (36) Do these steps to find the null leakage of spoiler No. 3:
 (a)  
Turn the control wheel approximately 40 degrees
 counterclockwise (from its center position).

 (b)  
Read the amperage or the flow value and write it on the data sheet for step 22.

 S 796-111
 (37) Do these steps to find the null leakage for spoilers No. 3 and No. 6:
 (a)  
Put the control wheel in its center position.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊 液壓 HYDRAULIC POWER(26)