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Flight Spoiler Cable Installation
Figure 401/27-61-61-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Flight Spoiler Actuator Quadrant
Figure 402 (Sheet 1 of 2)/27-61-61-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Flight Spoiler Actuator Quadrant
Figure 402 (Sheet 2 of 2)/27-61-61-990-802
737-600/700/800/900
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TASK 27-61-61-400-801
3. Flight Spoiler Actuator Quadrant Installation
(Figure 401, Figure 402)
A. References
Reference Title
12-22-61-600-802 Flight Spoiler Actuator Quadrant and Rod End Lubrication (P/B 301)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-61-00-800-801 Spoiler Hydraulic Systems A and B Pressurization (P/B 201)
27-61-00-800-802 Remove Pressure from the Spoiler Hydraulic Systems A and B
(P/B 201)
27-61-00-820-801 Spoiler Control Cables Adjustment (P/B 501)
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-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
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
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 Actuator Quadrant Installation
SUBTASK 27-61-61-420-001
(1) Install the quadrant [37]:
(a) Put the quadrant [37] in its position on the structure.
(b) Install the bolt [22], washer [23], washer [24] and nut [25].
(c) Install the bolt [30], washer [31], nut [32] and pin [33] to attach the quadrant [37] to the
actuator input arm [21].
SUBTASK 27-61-61-420-002
(2) Connect the wing spoiler cables WSA [2] and WSB [4] to the quadrant [37]:
737-600/700/800/900
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(a) Install the rig pins A/S-8 thru A/S-11 from the test set rig pin kit, SPL-1585 in the applicable
rig pin hole.
(b) Install rig pin A/S-14 from the test set rig pin kit, SPL-1585 in the spoiler mixer [1].
(c) Remove the turnbuckle clamps and tags from the wing spoiler cables WSA [2] and WSB [4].
(d) Attach the wing spoiler cables WSA [2] and WSB [4] to the quadrant [37].
1) Install retainers [29], nuts [28], washers [27] and bolts [26].
2) Install pin [36], guard [35], and guard pin [34].
(e) Tighten the wing spoiler cables WSA [2] and WSB [4] at the turnbuckles [3] in the wheel
well.
SUBTASK 27-61-61-820-001
(3) Do this task: Spoiler Control Cables Adjustment, TASK 27-61-00-820-801.
SUBTASK 27-61-61-820-002
(4) Do this task: Flight Spoiler Actuator Quadrant and Rod End Lubrication,
TASK 12-22-61-600-802.
SUBTASK 27-61-61-720-001
(5) Do this task: Flight Spoiler Actuator Quadrant Functional Test, TASK 27-61-61-000-802.
SUBTASK 27-61-61-410-001
(6) Put the Airplane Back to Its Usual Condition
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.
(a) Do this task: Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801.
(b) Do this task: Retract the Trailing Edge Flaps, TASK 27-51-00-860-804.
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737-600-700-800-900 飞机维护手册6 AIRCRAFT MAINTENANCE MANUA(53)
