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(1) If they are not installed, install the packings [2] and [3].
(a) Apply MCS 352B fluid, D00054 (recommended) or fluid, D00153 (alternative) to the new
packings [2] and [3].
(b) Install the packings [2] and [3] on the compensator cartridge [1].
SUBTASK 27-09-51-420-002
(2) Install the compensator cartridge [1]:
NOTE: Do not install 10-60560-3 Compensator on Flight Control Module if the Compensator has
serial number 20478A thru 20717A (Ref: AD 2002-19-51, Rev.1).
(a) Install the compensator cartridge [1] on the flight controls hydraulic module housing [4].
(b) Tighten the compensator cartridge [1] by hand until the compensator cartridge [1] bottoms
in the housing.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-010, 155-157, 201-999; AIRPLANES WITH 65-
44891-1 THRU -7 FCM
27-09-51
Page 406
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(c) Install the lockwire, G01912.
SUBTASK 27-09-51-860-003
(3) Do this task: Hydraulic Reservoirs Pressurization, TASK 29-11-01-860-801 or Hydraulic
Reservoirs Pressurization, TASK 29-09-00-860-801.
SUBTASK 27-09-51-860-004
WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE FLIGHT CONTROL
SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR. THESE
COMPONENTS CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER.
THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(4) For the applicable hydraulic system, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
NOTE: Pressurize hydraulic system A if you replace the compensator cartridge in the left main
wheel weel. Pressurize hydraulic system B if you replace the compensator cartridge in
the right main wheel weel.
SUBTASK 27-09-51-860-005
(5) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-09-51-860-006
(6) Make sure the applicable FLT CONTROL A or B switch, on the P5-3 Flight Controls panel, is set
to the ON position.
SUBTASK 27-09-51-790-001
(7) Operate the aileron control wheel, control column, and rudder pedals to bleed the hydraulic
system.
(a) Make sure there is no leakage of the hydraulic fluid at the compensator cartridge [1].
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-09-51-860-007
(1) Do this task: Hydraulic System A or B Power Removal, TASK 29-11-00-860-805.
SUBTASK 27-09-51-610-001
(2) If it is necessary to service the hydraulic reservoirs, do this task: Hydraulic Reservoir
Servicing, TASK 12-12-00-610-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-010, 155-157, 201-999; AIRPLANES WITH 65-
44891-1 THRU -7 FCM
27-09-51
Page 407
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
LOW PRESSURE WARNING SWITCH - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the low pressure warning switch
(2) An installation of the low pressure warning switch.
B. The low pressure warning switch is referred to as the "pressure switch" in this procedure.
C. The pressure switch is part of the flight controls hydraulic module. One flight controls hydraulic
module each is installed in the hydraulic systems A and B. The hydraulic module for hydraulic
system A is found in the left main wheel well. The hydraulic module for hydraulic system B is found in
the right main wheel well.
TASK 27-09-61-000-801
2. Low Pressure Warning Switch Removal
(Figure 401)
A. References
Reference Title
29-09-00-860-802 Hydraulic Reservoirs Depressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
29-11-01-860-802 Hydraulic Reservoirs Depressurization (P/B 201)
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
B. Tools/Equipment
Reference Description
STD-1110 Container - Hydraulic Fluid Resistant, 5 Gallon (19 Liters)
C. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Low Pressure Warning Switch Removal
SUBTASK 27-09-61-480-001
WARNING: MAKE SURE THE DOWNLOCK PINS ARE INSTALLED ON ALL THE LANDING GEARS.
WITHOUT THE DOWNLOCK PINS, THE LANDING GEARS COULD RETRACT AND
CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) If the downlock pins are not installed on all the landing gears, do this task: Landing Gear
　
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