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SUBTASK 27-61-00-080-001
(3) Remove the ground lock assemblies from the nose gear. To remove them, do this task: Landing
Gear Downlock Pins Removal, TASK 32-00-01-080-801.
------------------------- END OF TASK ---------------------------
TASK 27-61-00-800-802
4. Remove Pressure from the Spoiler Hydraulic Systems A and B
(Figure 201, Figure 202)
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)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1675 Assembly - Lock, Flight Controls
(Part #: F80049-18, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: F80049-12, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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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
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
D. Procedure
SUBTASK 27-61-00-860-007
(1) Set the SPOILER A and B switches on the forward overhead panel to the OFF position.
SUBTASK 27-61-00-860-008
(2) Open this circuit breaker and install safety tag:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 12 C00204 FLIGHT CONTROL SHUTOFF VALVES SPOILER
SUBTASK 27-61-00-860-009
(3) Set the ELEC 2, HYD PUMPS A and the ELEC 1, HYD PUMPS B switches on the forward
overhead panel to the OFF position.
SUBTASK 27-61-00-870-001
(4) Operate the rudder pedals to decrease the remaining hydraulic system pressure.
SUBTASK 27-61-00-860-010
(5) If it is necessary to open a hydraulic line, you must release pressure from the reservoir for the
applicable hydraulic system. To release it, do this task: Hydraulic Reservoirs
Depressurization, TASK 29-11-01-860-802 or Hydraulic Reservoirs Depressurization,
TASK 29-09-00-860-802.
SUBTASK 27-61-00-480-002
(6) Install the flight controls hydraulic module locks (Figure 202):
(a) Disconnect the electrical connector from the spoiler shutoff valve at the flight controls
hydraulic modules A and B.
(b) Put the manual override lever at the two spoiler shutoff valves in the position 2 (OFF
position).
(c) Install the lock, SPL-1675 on the two spoiler shutoff valves.
1) Install the lockpins.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Spoiler Control System Installation
Figure 202 (Sheet 1 of 3)/27-61-00-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Spoiler Control System Installation
Figure 202 (Sheet 2 of 3)/27-61-00-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
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Spoiler Control System Installation
Figure 202 (Sheet 3 of 3)/27-61-00-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 208
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TASK 27-61-00-840-802
5. Put the Spoiler Systems A and B Back to the Condition Before the Pressure Removal
(Figure 201, Figure 202)
A. References
Reference Title
12-12-00-610-801 Hydraulic Reservoir Servicing (P/B 301)
SWPM 20-60-03 Standard Wiring Practices Manual
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
　
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