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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-61-15-400-801
3. Flight Spoiler Hinge Link Installation
(Figure 401)
A. References
Reference Title
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-61-00-000-801 Flight Spoiler System Test (Alternate Method) (P/B 501)
27-61-00-800-801 Spoiler Hydraulic Systems A and B Pressurization (P/B 201)
27-61-00-820-803 Flight Spoiler Adjustment (P/B 501)
27-61-00-840-801 Put the Spoiler Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
27-61-00-840-802 Put the Spoiler Systems A and B Back to the Condition Before the
Pressure Removal (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (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-1745 Set - Lock, Flight Spoiler Actuator (Contains 8 Lock Assemblies)
(Part #: C27047-19, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -BBJ)
C. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
562 Left Wing - Spoiler No. 5
563 Left Wing - Spoiler No. 4
564 Left Wing - Spoiler No. 3
565 Left Wing - Spoiler No. 2
662 Right Wing - Spoiler No. 8
663 Right Wing - Spoiler No. 9
664 Right Wing - Spoiler No. 10
665 Right Wing - Spoiler No. 11
D. Flight Spoiler Hinge Link Installation
SUBTASK 27-61-15-420-001
(1) Install the bolt [6], washer [7], bushing [8], washer [9], nut [10] and pin [11] to install the hinge link
[5].
SUBTASK 27-61-15-860-006
(2) Make sure hydraulic power is not on. To remove it, do this task: Hydraulic System A or B Power
Removal, TASK 29-11-00-860-805.
SUBTASK 27-61-15-080-001
(3) Remove set, SPL-1745.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-15
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Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-61-15-860-011
(4) Do this task: Put the Spoiler Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-61-00-840-802.
SUBTASK 27-61-15-860-007
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(5) Do this task: Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801.
SUBTASK 27-61-15-860-008
(6) Move the speed brake lever to the DOWN position to lower the spoilers.
SUBTASK 27-61-15-860-009
(7) Do this task: Retract the Trailing Edge Flaps, TASK 27-51-00-860-804.
SUBTASK 27-61-15-860-010
(8) Do this task: Put the Spoiler Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-61-00-840-801.
SUBTASK 27-61-15-820-001
(9) Do this task: Flight Spoiler Adjustment, TASK 27-61-00-820-803.
SUBTASK 27-61-15-720-001
(10) Do this task: Flight Spoiler System Test (Alternate Method), TASK 27-61-00-000-801.
------------------------- END OF TASK ---------------------------
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
SPOILER MIXER - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the spoiler mixer.
(2) An installation of the spoiler mixer.
TASK 27-61-21-000-801
2. Spoiler Mixer Removal
(Figure 401)
A. References
Reference Title
27-61-00-800-801 Spoiler Hydraulic Systems A and B Pressurization (P/B 201)
27-61-00-840-801 Put the Spoiler Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
27-62-00-800-802 Remove Pressure from the Speed Brake Hydraulic Systems A and B
(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.
　
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