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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FLIGHT CONTROLS PANEL (P5-3) - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the flight controls panel, referred to as the flight controls module assy [1]
(2) An installation of the flight controls panel.
B. The flight controls panel (P5-3) is on the captain’s overhead panel. The flight controls panel has the
lights and switches used by the primary and auxiliary flight control system hydraulic supply valves.
TASK 27-09-45-000-801
2. Flight Controls Panel Removal
(Figure 401)
A. References
Reference Title
24-22-00-860-812 Remove Electrical Power (P/B 201)
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Prepare for the Removal
SUBTASK 27-09-45-860-001
(1) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
SUBTASK 27-09-45-860-002
(2) Open these circuit breakers and install safety tags:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 6 C01429 YAW DAMPER IND
D 2 C01045 AFCS SYS A FCC DC
D 6 C01354 YAW DAMPER 2 DC
F/O Electrical System Panel, P6-2
Row Col Number Name
A 6 C00566 FLIGHT CONTROL FLAP LOAD RELIEF
B 3 C01046 AFCS SYS B FCC DC
B 12 C00204 FLIGHT CONTROL SHUTOFF VALVES SPOILER
B 13 C00363 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
C 11 C00362 FLIGHT CONTROL SHUTOFF VALVES STBY RUD
C 13 C01074 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
D 13 C00841 FLIGHT CONTROL ALTN T.E. FLAP DRIVE
F/O Electrical System Panel, P6-3
Row Col Number Name
B 12 C00132 MASTER CAUTION ANNUNCIATOR BUS 1
B 13 C00131 MASTER CAUTION ANNUNCIATOR BAT
D 12 C00310 INDICATOR MASTER DIM BAT
D 13 C00311 INDICATOR MASTER DIM BUS 1
D 14 C00312 INDICATOR MASTER DIM BUS 2
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 401
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Row Col Number Name
E 14 C00316 INDICATOR MASTER DIM SECT 4
F/O Electrical System Panel, P6-4
Row Col Number Name
F 10 C01283 GENERATOR CONT UNIT 1
F 11 C01284 GENERATOR CONT UNIT 2
D. Procedure
SUBTASK 27-09-45-020-001
(1) Remove the flight controls :module assy [1]
(a) Loosen the quarter-turn fasteners [2] that hold the flight controls module assy [1].
(b) Lower the flight controls module assy [1].
(c) Disconnect the electrical connectors from the flight control module assy [1].
(d) Remove the flight controls module assy [1].
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-09-45
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Jun 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Flight Controls Panel (P5-3) Installation
Figure 401/27-09-45-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-09-45
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-09-45-400-801
3. Flight Controls Panel Installation
(Figure 401)
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
24-22-00-860-812 Remove Electrical Power (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)
34-21-00-820-801 Air Data Inertial Reference System - Alignment from the FMC CDU
(P/B 201)
34-21-00-820-802 Air Data Inertial Reference System - Alignment from the ISDU
(P/B 201)
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Procedure
SUBTASK 27-09-45-420-001
(1) Install the flight controls module assy [1]:
(a) Connect the electrical connectors to the flight control module assy [1].
NOTE: Make sure that the connectors match the mates on the flight control module
assy [1].
(b) Push the flight controls module assy [1] into the captain’s overhead panel.
(c) Install the screws [2] that hold the flight controls module assy [1].
SUBTASK 27-09-45-860-003
(2) Remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 6 C01429 YAW DAMPER IND
D 2 C01045 AFCS SYS A FCC DC
D 6 C01354 YAW DAMPER 2 DC
F/O Electrical System Panel, P6-2
Row Col Number Name
A 6 C00566 FLIGHT CONTROL FLAP LOAD RELIEF
　
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