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(g) Remove the nuts [11], washers [10], bolts [9] to remove the bracket [7].
(h) Move the control wheel drum assembly [19] down while, at the same time, you put the
cable ACBA [1] and cable ACBB [2] through the openings.
(i) Remove the control wheel drum assembly [19] from the airplane structure.
------------------------- END OF TASK ---------------------------
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Figure 401 (Sheet 1 of 5)/27-11-51-990-801
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Aileron Control Wheel Drum Installation
Figure 401 (Sheet 2 of 5)/27-11-51-990-801
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Aileron Control Wheel Drum Installation
Figure 401 (Sheet 3 of 5)/27-11-51-990-801
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Aileron Control Wheel Drum Installation
Figure 401 (Sheet 4 of 5)/27-11-51-990-801
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Figure 401 (Sheet 5 of 5)/27-11-51-990-801
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TASK 27-11-51-400-801
3. Aileron Control Wheel Drum Installation
(Figure 401)
A. References
Reference Title
22-11-11-740-801 Roll Force Transducer Test (P/B 501)
27-11-00-700-802 First Officer’s Control Wheel Lost Motion Test (P/B 501)
27-11-00-700-803 Manual Reversion Control Friction Test (P/B 501)
27-11-00-700-804 Control Wheel Centering Check (P/B 501)
27-11-00-700-805 Aileron Control Wheel Force Test (P/B 501)
27-11-00-700-807 Control Wheel Travel Stop Test (P/B 501)
27-11-00-710-801 Aileron Response (Operational) Test (P/B 501)
27-11-00-820-801 Aileron Cables Adjustment (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)
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. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
19 Drum assembly 27-11-61-01-330 GUN ALL
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
211 Flight Compartment - Left
212 Flight Compartment - Right
E. Access Panels
Number Name/Location
112A Forward Access Door
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F. Aileron Control Wheel Drum Installation
SUBTASK 27-11-51-210-001
CAUTION: MAKE SURE THAT IT IS THE SELF-LOCKING SHEAR NUT AND NOT THE TENSION
TYPE SELF-LOCKING NUT THAT CONNECTS THE FORK TO THE CONTROL WHEEL
DRUM. IF AN INCORRECT NUT IS INSTALLED, THE CAPTAIN’S CONTROL COLUMN
CAN BECOME DISENGAGED FROM THE FORK, THIS CAN CAUSE INJURY TO
PERSONS OR DAMAGE TO EQUIPMENT.
(1) Make sure the fork is connected to the control wheel drum with correct self-locking shear nut.
NOTE: You must see a completed bolt chamfer at the end of the nut.
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(2)
