27-11-00
ALL ú ú 01 Page 506 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
2) The cable tension is as specified (Fig. 501). 3) If it is necessary, adjust the cables ACBA and ACBB in the lower nose compartment.
(b) Aileron Control Cables AA and AB
1) These are the results with the rig pins A/S-1, A/S-1A, and A/S-15 installed: a) The trim roller is correctly installed against the cam. b) The rig pin A/S-3 is easily installed.
2) The cable tension is as specified (Fig. 501). 3) If it is necessary, adjust the cables AA and AB in the lower nose compartment.
(c) Aileron Power Control Unit Valve Rods 1) With the aileron trim actuator in the neutral position, you can easily install the rig pin A/S-15.
2) With the two aileron control wheels in the neutral position and hydraulic power are ON, you can easily install the rig pin A/S-4.
3) If it is necessary, adjust the valve rods of the power control unit.
(d) Aileron Bus Cables ABSA and ABSB 1) With the rig pin A/S-4 installed, the left and right ailerons are in the neutral position (Fig. 506).
2) If it is necessary, adjust the cables ABSA and ABSB in the two wings.
(5)
After the replacement or installation of an aileron, aileron tab, or aileron tab control rod, it may be necessary to do a flight test. Refer to the "Flight Test to Find and Correct Asymmetrical Flight Control Forces" for details.
B.
Special Tools and Equipment
(1)
F80222-1 - Aileron Tab Alignment Protractor
(2)
SE27-0001- Straightedge
(3)
F70207-93 or -97 Rig Pins Kit
~.............................................................................. |REF NO. | F70207-( ) | DIAMETER | LENGTH | | | | | (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-3 | -8 | 0.309-0.311| 3.7 |0.25 |SPOILER CONTROL | | | | | | QUADRANT LOWER LEVER | |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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27-11-00
ALL ú ú 01 Page 507 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C.
D.
E.
A
737-300/400/500MAINTENANCE MANUAL
References
(1)
AMM 27-11-00/201, Aileron and Aileron Trim Control System
(2)
IPC 27-11-14-01, Fig. 1
(3)
OHM 27-37-09Access
(1)
Location Zone 101 Control Cabin, LH 102 Control Cabin, RH 202 Lower Nose Compartment 216 Main Wheel Well, LH 217 Main Wheel Well, RH 306 Wing Trailing Edge Aileron and Control Tab, LH 406 Wing Trailing Edge Aileron and Control Tab, RH
(2)
Access Panel 1103 Forward Access Door
Adjust the Aileron and Aileron Trim Control System
NOTE: If you adjust the aileron trim control system without hydraulic
____ power, the drag will permit the aileron system (without power) to stay out of the center. This will push the cam follower of the trim and centering mechanism out of the cam detent. When you apply hydraulic power, the control wheels and the ailerons will quickly move to the new adjusted position.
S 825-004
(1)
Adjust the aileron control cables ACBA and ACBB:
(a)
Open the access door 1103 at the lower nose compartment.
(b) 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 1(83)
