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Flaps, TASK 27-51-00-860-804.
------------------------- END OF TASK ---------------------------
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FLAP CONTROL UNIT - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the flap control unit
(2) An installation of the flap control unit.
B. The flap control unit includes the flap control valves for the leading edge and the trailing edge, the
control linkage, follow-up linkage, and the flap limit switch cams.
C. The flap limit switches are installed on the flap control unit. It is necessary to remove the flap limit
switches from the flap control unit.
TASK 27-51-61-000-801
2. Flap Control Unit Removal
A. References
Reference Title
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-51-63-000-801 Flap Limit Switch Removal (P/B 401)
29-09-00-860-802 Hydraulic Reservoirs Depressurization (P/B 201)
29-11-01-860-802 Hydraulic Reservoirs Depressurization (P/B 201)
31-51-01-000-801 Flap Landing Warning Switch Removal (P/B 401)
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 27-51-61-860-001
(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 27-51-61-860-002
(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.
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SUBTASK 27-51-61-860-003
(3) Open this circuit breaker and install safety tag:
F/O Electrical System Panel, P6-2
Row Col Number Name
A 6 C00566 FLIGHT CONTROL FLAP LOAD RELIEF
SUBTASK 27-51-61-480-001
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.
(4) 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 27-51-61-010-001
(5) Remove the floor panel to get access to the top of the flap control unit assembly [9], do this task:
Passenger Cabin Floor Panel Removal, TASK 53-21-00-000-801
(Figure 401).
NOTE: The floor panel is located between stations 706 and 727B on the right side of the
airplane.
E. Flap Control Unit Removal
SUBTASK 27-51-61-020-001
(1) Disconnect the cable assembly [1], WFA and WFB from the quadrant [5]:
(a) To get access to the turnbuckles [3], do this task:
Open this access panel:
Number Name/Location
112A Forward Access Door
or remove this access panel:
Number Name/Location
114AC Fwd Nose Wheel Well Upper Access Panel
(b) Remove the locking clips [2] and loosen the turnbuckles [3] on the cable assembly [1].
(c) Remove the pin [8], pin [6] and the two spacers [7] from the quadrant [5].
(d) Remove the straps [10] that attach the cable assembly [1] to the quadrant [5].
(e) Remove the pins [4] that attach the cable assembly [1] to the quadrant [5].
(f) Remove the cable assembly [1] from the quadrant [5].
SUBTASK 27-51-61-020-002
(2) Remove the quadrant [5] from the flap control unit assembly [9]:
(a) Remove the nut [11] and washer [17] that attach the quadrant [5] to the flap control unit
assembly [9].
(b) Remove the quadrant [5] from the flap control unit assembly [9].
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SUBTASK 27-51-61-020-003
(3) Remove the flap limit switches [39] from the flap control unit assembly [9] (Figure 402):
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(97)
