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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 506
Oct 10/2003
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FLAP HYDRAULIC MOTOR - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the flap hydraulic motor
(2) An installation of the flap hydraulic motor.
B. The flap hydraulic motor is installed on the flap power drive unit (PDU) in the main landing gear
wheel well.
TASK 27-51-52-000-801
2. Flap Hydraulic Motor Removal
(Figure 401)
A. References
Reference Title
29-09-00-860-802 Hydraulic Reservoirs Depressurization (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. 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
C. Prepare for the Removal
SUBTASK 27-51-52-480-001
WARNING: MAKE SURE THE DOWNLOCK PINS ARE INSTALLED ON ALL THE LANDING GEAR.
WITHOUT THE DOWNLOCK PINS, THE LANDING GEAR CAN RETRACT AND CAUSE
INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) If the downlock pins are not installed in the nose and main landing gear, do this task: Landing
Gear Downlock Pins Installation, TASK 32-00-01-480-801.
SUBTASK 27-51-52-860-001
(2) Remove the pressure from the system B hydraulic reservoir. To remove the pressure, do this
task: Hydraulic Reservoirs Depressurization, TASK 29-11-01-860-802 or Hydraulic
Reservoirs Depressurization, TASK 29-09-00-860-802.
D. Flap Hydraulic Motor Removal
SUBTASK 27-51-52-020-001
(1) Disconnect the three hydraulic lines [1]:
(a) Disconnect the hydraulic lines [1] from the motor assembly [3].
(b) Install caps on the hydraulic lines [1].
(c) Install plugs in the ports on the motor assembly [3].
SUBTASK 27-51-52-020-002
(2) Remove the motor assembly [3]:
(a) Remove the bolts [6] and washers [7] that attach the motor assembly [3] to the PDU [2].
(b) Remove the motor assembly [3] from the PDU [2].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-52-020-003
(3) If you will install a new motor assembly [3], remove the reducers [4], elbow [9], valve [11] and
packings [5], packing [10] and packing [12] from the motor assembly [3].
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Jun 10/2005
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Flap Hydraulic Motor Installation
Figure 401 (Sheet 1 of 2)/27-51-52-990-801
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Flap Hydraulic Motor Installation
Figure 401 (Sheet 2 of 2)/27-51-52-990-801
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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TASK 27-51-52-400-801
3. Flap Hydraulic Motor Installation
(Figure 401)
A. References
Reference Title
12-12-00-610-801 Hydraulic Reservoir Servicing (P/B 301)
27-51-00-860-801 Trailing Edge Flap System Operation With Primary Control (P/B 201)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
B. Consumable Materials
Reference Description Specification
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D00054 Fluid - Hydraulic Assembly Lubricant - MCS 352B
(Formally Monsanto MCS 352B)
D00153 Fluid - Hydraulic, Erosion Arresting, Fire Resistant BMS3-11, Type
IV
(interchange~
able&
intermixable
with Type V)
D00633 Grease - Aircraft General Purpose BMS3-33
C. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
3 Motor assembly 27-51-51-01-110 GUN ALL
4 Reducer 27-51-51-01-100 GUN ALL
5 Packing 27-51-51-01-105 GUN ALL
6 Bolt 27-51-51-01-075 GUN ALL
11 Valve 27-51-51-01-095 GUN ALL
　
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