EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-15-00
ALL ú ú 01 Page 502 ú Jul 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
D. Procedure
S 215-009
(1) Make sure the four LOW PRESSURE lights for the HYD PUMPS (on the P5 panel) are on.
S 715-010
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. THE AILERONS, RUDDER, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Put the HYD PUMPS A ELEC 2 switch (to do a test of system A) or the HYD PUMPS B ELEC 1 switch (to do a test of system B) in the ON position.
(a)
Make sure the pressure for the applicable hydraulic system becomes stable between 2800 and 3200 psig.
(b)
Make sure the applicable LOW PRESSURE light goes out.
S 715-013
(3) Put the switch in the OFF position.
(a) Operate the rudder until the hydraulic pressure is zero. 1) Make sure the LOW PRESSURE light comes on.
S 715-014
(4)
Put the HYD PUMPS A ENG 1 switch (to do a test of system A) or the HYD PUMPS B ENG 2 switch (to do a test of system B) in the ON position.
S 985-016
(5)
Motor or operate the applicable engine (Ref 71-00-00/201).
(a)
Make sure the applicable LOW PRESSURE light goes out.
(b)
With the engine at idle speed or faster, make sure the pressure in the applicable hydraulic system is 2900 - 3200 psig.
S 715-017
(6) Put the switch in the OFF position.
(a) Operate the rudder until the hydraulic pressure is zero. 1) Make sure the LOW PRESSURE light comes on.
S 985-018
(7) Stop the engine (Ref 71-00-00/201).
E. Put the Airplane Back to Its Usual Condition
S 865-019
(1) Remove electrical power if it is not necessary (Ref 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-15-00
ALL ú ú 01 Page 503 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-020
(2) Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P6-2 Panel
1) PTU/LG BYP V CONT 1
2) PTU/LG BYP V CONT 2
(b)
P6-11 Panel
1) STBY HYD PUMP NORMAL
(c)
P6-12 Panel
1) STBY HYD PUMP ALTERNATE
TASK 29-15-00-715-021
3. Operational Test for the Standby Hydraulic System_________________________________________________
A. References
(1)
24-22-00/201, Manual Control
(2)
29-15-00/201, Hydraulic Systems A, B, and Standby
B. Access
(1) Location Zones
101/102 Control Cabin
216/217 Main Wheel Wells
C. Prepare for the Test
S 865-022
(1)
Supply electrical power (Ref 24-22-00/201).
S 865-023
(2)
Close these circuit breakers:
(a)
P6-2 Panel 1) NOSE GEAR AIR/GND 2) FLIGHT CONTROL SHUTOFF VALVE STBY RUD 3) LANDING GEAR AIR/GND RELAY & LIGHTS
(b) 中國(guó)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(cè) 液壓 HYDRAULIC POWER(73)
