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27-11-00-820-801 Aileron Cables Adjustment (P/B 501)
27-61-00-800-801 Spoiler Hydraulic Systems A and B Pressurization (P/B 201)
51-31-00-390-801 Non-Removable Faying (Mated) Surface Seal Application (P/B 201)
53-21-00-400-801 Passenger Cabin Floor Panel Installation (P/B 401)
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. Consumable Materials
Reference Description Specification
G01048 Lockwire - Corrosion Resistant Steel (0.032 In. Dia.) NASM20995~
C32
D. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
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
231 Forward Passenger Compartment - Forward Entry Door to Sta 663.75
- Left
232 Forward Passenger Compartment - Forward Entry Door to Sta 663.75
- Right
E. Access Panels
Number Name/Location
112A Forward Access Door
F. Spoiler Control Quadrant Installation
SUBTASK 27-61-41-020-003
(1) If you will install a new spoiler control quadrant, remove the spoiler cable quadrant [5] from the
quadrant shaft [36].
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SUBTASK 27-61-41-200-001
(2) Do a check of the shear rivets [32] on the quadrant shaft [36] at the aileron input crank [26]:
(a) Make sure the witness hole in the aileron input crank [26] and the quadrant shaft [36] align
correctly.
NOTE: The marker instructions are located on the quadrant shaft [36].
SUBTASK 27-61-41-420-001
(3) Connect the spoiler cable quadrant [5] to the quadrant shaft [36]:
(a) Put the quadrant shaft [36] through the opening in the wheel well ceiling [37].
(b) Engage the quadrant shaft [36] with the spoiler cable quadrant [5].
SUBTASK 27-61-41-420-002
(4) Attach the quadrant shaft [36] to the wheel well ceiling [37]:
(a) Apply a pressure seal to the bearing retainer [38] and the wheel well ceiling [37], to apply
seal, do this task: Non-Removable Faying (Mated) Surface Seal Application,
TASK 51-31-00-390-801.
NOTE: Make sure that the bearing housing is aligned with the correct bolt holes in the
wheel well ceiling.
(b) Install bolts [11] with the heads up through the wheel well ceiling [37] to attach the bearing
retainer [38].
(c) Install the washers [12], washers [13] and nuts [14] on the bolts [11].
(d) Tighten the nuts [14] to 20-25 pound-inches (2.3-2.8 newton-meters).
SUBTASK 27-61-41-420-003
(5) Install the quadrant shaft support bracket [25] on the wheel well forward bulkhead [20]:
(a) Put the quadrant shaft support bracket [25] in its position.
(b) Install the bolts [21], washers [22], washers [23] and nuts [24] to attach the quadrant shaft
support bracket [25].
SUBTASK 27-61-41-420-004
(6) Install the aileron spring cartridge [31]:
(a) Do this task: Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801.
(b) Install the rig pins A/S-4 and A/S-3 from the test set rig pin kit, SPL-1585.
(c) If you cannot easily install and remove the rig pin A/S-3. adjust the aileron spring cartridge
[31].
1) Loosen the checknut [40].
2) Use the collar nut [41] to adjust the length of the spring cartridge [31] until you can
easily install and remove rig pin A/S-3.
a) Make sure the internal spring does not deflect.
b) Make sure there is no backlash.
3) Tighten the checknut [40] to 10 - 20 pound-inches (1.1 - 2.3 newton-meters).
4) Install lockwire, G01048 on the checknut [40] and collar nut [41].
(d) Connect the aileron spring cartridge [31] to the aileron input crank [26]:
1) Make sure the drain holes [39] on the aileron spring cartridge [31] are down.
2) Install the bolt [27] with the bolt head up.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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