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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
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Prepare for the Removal
SUBTASK 27-11-54-860-001
(1) Put the captain’s and first officer’s control wheels in the neutral position.
SUBTASK 27-11-54-860-002
WARNING: MAKE SURE THE DOWNLOCK PINS ARE INSTALLED ON ALL THE LANDING GEAR.
WITHOUT THE DOWNLOCK PINS, THE LANDING GEAR COULD RETRACT AND CAUSE
INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Do this task: Remove Pressure from the Aileron Hydraulic Systems A and B,
TASK 27-11-00-860-801.
SUBTASK 27-11-54-480-001
(3) Install the rig pin A/S-15, from the rig pin kit, SPL-1585, in the aileron trim mechanism.
E. Aileron Trim Actuator Removal
SUBTASK 27-11-54-020-001
(1) Disconnect the electrical connector from the aileron trim actuator [1].
SUBTASK 27-11-54-020-002
(2) Remove the aileron trim actuator [1] from the aileron trim mechanism:
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(a) Remove the nut [11], bushing [10], washer [9], washer [8], and bolt [7].
(b) Remove the nut [2], bushing [3], washer [4], washer [5], and bolt [6].
(c) Remove the aileron trim actuator [1].
------------------------- END OF TASK ---------------------------
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Aileron Trim Actuator Installation
Figure 401 (Sheet 1 of 2)/27-11-54-990-801
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Aileron Trim Actuator Installation
Figure 401 (Sheet 2 of 2)/27-11-54-990-801
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TASK 27-11-54-400-801
3. Aileron Trim Actuator Installation
(Figure 401)
A. References
Reference Title
27-11-00-730-801 Aileron Trim Response Test (P/B 501)
27-11-00-860-802 Put the Aileron Hydraulic Systems A and B Back to the Condition
Before Pressure Removal (P/B 201)
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
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
G50171 Compound - Corrosion Inhibiting Compound,
Interior Application - D5026NS or ZC-026
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 Aileron trim actuator 27-11-54-01-045 GUN 001-028, 101-121,
155-157, 201-999
E. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
211 Flight Compartment - Left
212 Flight Compartment - Right
F. Aileron Trim Actuator Installation
SUBTASK 27-11-54-420-001
(1) Install the aileron trim actuator [1]:
(a) Make sure that the rig pin A/S-15, from the rig pin kit, SPL-1585, is installed in the aileron
trim mechanism.
(b) Put the aileron trim actuator [1] in position.
(c) Install the bolt [6], bushing [3], washer [5], washer [4], and nut [2].
(d) Install the bolt [7], bushing [10], washer [8], washer [9], and nut [11].
SUBTASK 27-11-54-420-002
(2) Do the following steps to connect the electrical connector:
(a) Before you connect the electrical connector, examine the connector for corrosion.
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