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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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
B.
C.
D.
E.
A
737-300/400/500MAINTENANCE MANUAL
(2) F70207-93 or -97 Rigging Pins Kit:
~...................................................................... | | | DIAMETER | LENGTH | | | REF NO. | F70207-( )| (INCHES) | (INCHES) | FUNCTION | ........................................................................ | A/S-1 | -13 | 0.309-0.311 | 2.35 |0.06 | AILERON TRANSFER | | | | | | MECHANISM | | A/S-1A | -19 | 0.309-0.311 |8.25+/- 0.25| AILERON TRANSFER | | | | | | MECHANISM | | A/S-15 | -85 | 0.309-0.311 | 2.5 |0.25 | AILERON TRIM | | | | | | MECHANISM | 2.........…...........….............…............….....................1
Standard Tools and Equipment
(1)
Vinyl Plastic Tape - 2 inches wide, Permacel Cold Weather Vinyl Tape
No. 295Consumable Materials
(1)
D00000 Solvent - BMS 3-2
(2)
D00000 Grease - MIL-G-25760References
(1)
AMM 27-11-51/601, Aileron Control Wheel Drum
(2)
AMM 22-11-11/401, Roll Control Wheel Steering Force Transducer
(3)
AMM 22-11-13/401, Aileron Force Limiter
(4)
AMM 32-31-00/501, Landing Gear Control System
(5)
AMM 32-41-00/501, Hydraulic Brake System
(6)
AMM 27-62-00/501, Speed Brake Control System
(7)
AMM 27-11-51/501, Aileron Control Wheel Drum
(8)
AMM 22-11-11/501, Roll Control Wheel Steering Force Transducer
(9)
AMM 22-11-13/501, Aileron Force LimiterAccess
(1)
Location Zone 101 Control Cabin, LH 102 Control Cabin, RH 202 Lower Nose Compartment
(2)
Access Panel 1103 Forward Access Door
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A STRAIGHT EDGE
SEE B FIRST OFFICER'S CONTROL WHEEL
CAPTAIN'S CONTROL WHEEL
A
LOST MOTION DEVICE CABLE AA CABLE AB AILERON CONTROL AILERON CONTROL BUS DRUM DRUM
CABLE ACBB CABLE ACBA
RIG PIN A/S-1
RIG PIN A/S-1A
B FWD
Aileron Control Wheel Adjustment Figure 403
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