B.
References
(1)
27-11-81/401, Aileron Artificial Feel, Centering and Trim Mechanism
(2)
25-22-00/201, Passenger Seats
(3)
25-27-15/401, Carpets
C.
Access
(1)
Location Zone
202 Lower Nose Compartment
216 Main Wheel Well, LH
217 Main Wheel Well, RH
D.
Prepare for Removal
S 024-002
(1) Do this task: "Aileron Artificial Feel, Centering and Trim Mechanism Removal" (Ref 27-11-81/401).
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27-11-91
ALL ú ú 01 Page 401 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CABLE AB
SEE A
TURNBUCKLES
CABLE AA RIGGING PIN A/S-4SEE B
POWER CONTROL SHAFT
AILERON ARTIFICIAL FEEL, CENTERING AND TRIM MECHANISM
SEE C FWD INBD
A
Aileron Body Quadrant Installation Figure 401 (Sheet 1)
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27-11-91
ALL ú ú 01 Page 402 ú Feb 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AILERON RETAINING PLATE
BODY NUT
QUADRANT WASHER
SEAL DISC CABLE AA
BOLT
RETAINING
PLATE MOUNTING BOLT
AILERON (4 LOCATIONS)
BODY QUADRANT
PRESSURE SHAFT
DECK
CABLE AB
PACKING
RING SEAL
SEAL HOUSING
BEARING
INNER SPHERE
PIN
WASHER
NUT
BEARING
(4 LOCATIONS)
HOUSING
B
AILERON TRIM ACTUATOR
FWD INBD PIN A/S-15 RIGGING
C
Aileron Body Quadrant Installation Figure 401 (Sheet 2)
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27-11-91
ALL ú ú 01 Page 403 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(2) S 424-003Do this task: "Passenger Seats Removal" (Ref 25-22-00/201).
E. S 424-014 (3) Do this task: Procedure "Carpets Removal" (Ref 25-27-15/401).
S 024-004
(1)
Remove the aileron body quadrant (Fig. 401):
(a)
Put the aileron in the neutral position.
(b)
Install the rig pin A/S-4 in the aileron bus drums.
(c)
Disconnect the left cables AA and AB at the turnbuckles.
(d)
Remove the retaining plates.
(e)
Safety the disconnected cables with clamps.
(f)
Remove the cables AA and AB from the aileron body quadrant.
(g)
Attach identification tags to the disconnected cables for easier assembly.
(h)
Remove the nuts, washers and bolts that hold the aileron body quadrant to its shaft.
(i)
Remove the nuts, washers and bolts to remove the bearing housing from the shaft of the aileron body quadrant.
(j)
Remove the shaft of the aileron body quadrant from the structure.
TASK 27-11-91-404-005
3. Aileron Body Quadrant Installation
__________________________________
A. Special Tools and Equipment
(1)
SE27-0001 - Straightedge
(2)
F72790 - Control Wheel Protractor Mount
(3)
4MIT65B80307-1 - Control Surface Protractor
(4)
F72867-1 - Adapter Torque and Force Test Control Wheel
(5) F70207-93 or -97 Rig Pins Kit: ~............................................................................... | | | DIAMETER | LENGTH | | | REF NO. | F70207-( ) | (INCHES) |(INCHES) | FUNCTION | ................................................................................. | A/S-1 | -13 | 0.309-0.311 | 2.35 |0.06 | AIRLEON TRANSFER MECHANISM| | A/S-1A | -19 | 0.309-0.311 |8.25 +/- 0.25| AILERON TRANSFER MECHANISM| | | | | | | | A/S-4 | -11 | 0.309-0.311 | 6.7 |0.25 | AILERON BUS DRUM | | A/S-15 | -85 | 0.309-0.311 | 2.5 |0.25 | AILERON TRIM MECHANISM | 2.........…............…..............….............…...........................1
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