27-11-91
ALL ú ú 01 Page 404 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
TABLE I
1 TEMP `F CABLE TENSION (POUNDS)
2 3 CABLES AA AND AB CABLES ACBA AND ACBB 4 5
90 70 50 30 -10 -30 -40 +10 110 133 124 115 107 82 74 68 99 90 93 84 75 70 61 53 49 46 44
TEMPERATURE TO BECOME STABLE
THE CABLE LOADS MUST NOT BE MORE THAN +10/0 POUNDS OF THE NOTED TABLE I VALUES WHEN YOU ADJUST THE SYSTEM
FOR THE NECESSARY REGULAR CHECKS WITHOUT THE SYSTEM DISCREPANCY REPORTS, THE CABLE TENSIONS CAN CHANGE +15/-30 POUNDS FROM THE TABLE I VALUES. FOR CABLE TENSION CHECKS THAT ARE THE RESULT OF THE SYSTEM DISCREPANCY REPORTS, THE TENSIONS CAN CHANGE |15 POUNDS FROM THE TABLE I VALUES. WHEN YOU ADJUST THE CABLES, TABLE I VALUES MUST BE MET WITH THE CABLE LOADS MUST NOT BE MORE THAN |15 POUNDS OF THE TABLE I VALUES WHEN YOU ADJUST THE SYSTEM
FOR THE NECESSARY REGULAR CHECKS WITHOUT THE SYSTEM DISCREPANCY REPORTS, THE CABLE TENSIONS CAN CHANGE +15/-30 POUNDS FROM THE TABLE I VALUES. FOR CABLE TENSION CHECKS THAT ARE THE RESULT OF THE SYSTEM DISCREPANCY REPORTS, THE TENSIONS CAN CHANGE |15 POUNDS FROM THE TABLE I VALUES. WHEN YOU ADJUST THE CABLES, TABLE I VALUES MUST BE MET WITH
Aileron System Cable Tension Requirements
Figure 402
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27-11-91
ALL ú ú 01 Page 405 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FIRST OFFICER'S CONTROL WHEEL
SEE A
CAPTAIN'S
CONTROL WHEEL
FIRST OFFICER'S
CONTROL WHEEL
CABLE AB
AILERON CONTROL BUS DRUM
LOST MOTION DEVICE
AILERON CONTROL DRUM
CABLE AA
CABLE ACBB CABLE ACBA
RIGGING PIN A/S-1
RIGGING PIN A/S-1A
FWD
A
Aileron Control Wheel Neutral Position
Figure 403
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27-11-91
ALL ú ú 01 Page 406 ú Oct 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
B. Consumable Materials
(1)
A00000 Cement - BMS 5-14
(2)
A00794 Sealant - BMS 5-95
C.
References
(1)
27-11-91/601, Aileron Body Quadrant
(2)
51-31-00/201, Seals and Sealing
(3)
27-11-81/401, Aileron Artificial Feel, Centering and Trim Mechanism
(4)
27-11-71/501, Aileron Power Control Unit
(5)
25-22-00/201, Passenger Seats
(6)
25-27-15/401, Carpets
D.
Access
(1)
Location Zone
101 Control Cabin, LH
216 Main Wheel Well, LH
102 Control Cabin, RH
217 Main Wheel Well, RH
E.
Install the Aileron Body Quadrant
S 434-013
(1)
Assemble the bearing housing assembly (Fig. 401):
(a)
Install the inner sphere in the bearing housing.
(b)
Install the pin.
(c)
Install the bearing, seal housing, ring seal, and packing into the bearing housing.
CONTROL WHEEL
TORQUE WRENCH ADAPTER
Figure 404
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27-11-91
ALL ú ú 01 Page 407 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
POINT B
____ WITH THE AILERON SYSTEM ADJUSTED,
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