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Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-51-61-420-009
(11) Install the locking clips [49] on the turnbuckles [50] for cables [48] WFFA and WFFB (Figure 402).
SUBTASK 27-51-61-420-010
(12) Install the flap limit switches [39] in the flap control unit assembly [9]:
(a) For the Landing Warning Switch, S138, do this task: Flap Landing Warning Switch
Installation, TASK 31-51-01-400-801.
(b) For the Flap UP limit switch, S245, the Flap DOWN limit switch, S246 and the Flap UP limit
switch, S1051, do this task: Flap Limit Switch Installation, TASK 27-51-63-400-801.
SUBTASK 27-51-61-420-011
(13) Do the adjustment of the flap limit switches [39] in the flap control unit assembly [9]:
(a) For the Landing Warning Switch, S138, do this task: Flap Landing Warning Switch
Adjustment, TASK 31-51-01-820-801.
(b) For the Flap UP limit switch, S245, the Flap DOWN limit switch, S246 and the Flap UP limit
switch, S1051, do this task: Flaps Limit Switch Adjustment, TASK 27-51-63-820-801.
SUBTASK 27-51-61-860-004
(14) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 6 C00566 FLIGHT CONTROL FLAP LOAD RELIEF
SUBTASK 27-51-61-730-001
(15) Do this task: Trailing Edge Flap System Test, TASK 27-51-00-730-801.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-61-410-002
(1) Install the lower pan [37] on the flap control unit assembly [9]:
(a) Put the lower pan [37] in its location on the flap control unit assembly [9].
(b) Apply compound, C00913 to the shank and threads of the screws [36].
(c) Install the washers [55] and screws [36] to attach the lower pan [37].
SUBTASK 27-51-61-410-003
(2) Install the switch cover [31] on the flap control unit assembly [9]:
(a) Put the switch cover [31] in its location on the flap control unit assembly [9].
(b) Apply compound, C00913 to the shank and threads of the screws [40].
(c) Install the washers [56] and screws [40] to attach the switch cover [31].
SUBTASK 27-51-61-410-004
(3) Install the floor panel above the flap control unit assembly [9], do this task: Passenger Cabin
Floor Panel Installation, TASK 53-21-00-400-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FLAP CONTROL QUADRANT - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the flap control quadrant
(2) An installation of the flap control quadrant.
TASK 27-51-62-000-801
2. Flap Control Quadrant Removal
(Figure 401)
A. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
53-21-00-000-801 Passenger Cabin Floor Panel Removal (P/B 401)
B. Location Zones
Zone Area
114 Area Above and Outboard of Nose Landing Gear Wheel Well - Right
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
240 Subzone - Passenger Compartment - Body Station 663.75 to Body
Station 1016.00
C. Access Panels
Number Name/Location
112A Forward Access Door
114AC Fwd Nose Wheel Well Upper Access Panel
D. Prepare for the Removal
SUBTASK 27-51-62-860-001
(1) If the trailing edge flaps are not in the retracted position, do this task: Retract the Trailing Edge
Flaps, TASK 27-51-00-860-804.
SUBTASK 27-51-62-480-001
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.
(2) 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 27-51-62-040-001
(3) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-51-62-010-001
(4) Remove the floor panel to get access to the top of the flap control unit [9], do this task:
Passenger Cabin Floor Panel Removal, TASK 53-21-00-000-801.
NOTE: The floor panel is located between stations 706 and 727B on the right side of the
airplane.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
　
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