(3)
F72790 Aileron Control Wheel Protractor Mount
(4)
SE27-0001 Control Wheel Straightedge
(5)
Rig Pin Kit - F70207-107:
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-61-00
ALL ú ú 01 Page 502 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
~............................................................................... | | | Diameter | Length | | | Ref No. | F70207-( ) | (inches) | (inches) | Function | ................................................................................. | A/S-1 | -11 | 0.309-0.311 | 7.5 |0.25 |TRANSFER MECHANISM | | A/S-1A | -19 | 0.309-0.311 | 8.8 |0.25 |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 | 7.5 |0.25 |AILERON BUS DRUM | | A/S-8 | -23 | 0.246-0.248 | 3.8 |0.25 |SPOILER ACTUATOR QUADRANT | | | | | | (LEFT WING) | | A/S-9 | -23 | 0.246-0.248 | 3.8 |0.25 |SPOILER ACTUATOR QUADRANT | | | | | | (LEFT WING) | | A/S-10 | -23 | 0.246-0.248 | 3.8 |0.25 |SPOILER ACTUATOR QUADRANT | | | | | | (RIGHT WING) | | A/S-11 | -23 | 0.246-0.248 | 7.5 |0.25 |SPOILER ACTUATOR QUADRANT | | | | | | (RIGHT WING) | | A/S-14 | -11 | 0.309-0.311 | 6.7 |0.25 |SPOILER MIXER | | S/B-2 | -101 | 0.309-0.311 | 3.7 |0.25 |SPEED BRAKE INPUT | | | | | | QUADRANT | 2.........….............…..............….............…..........................1
B. Standard Tools and Equipment
(1)
Cable Tensiometer - 0- to 150-pound range for 1/8-inch cable
(2)
Feeler gage set - with a minimum total thickness of 0.30 inch
C.
Consumable Materials
(1)
A00247 Sealant BMS 5-95
(2)
B00365 Solvent - Methyl-Ethyl-Ketone TT-M-261
(3)
C00308 Compound - Corrosion Preventive, MIL-C-11796, Class 3
D.
References
(1)
24-22-00/201, Manual Control
(2)
27-61-00/201, Spoiler Control System
E.
Access
(1)
Location Zone 101 Control Cabin - Left 102 Control Cabin - Right 202 Lower Nose Compartment 216 Left Main Wheel Well 217 Right Main Wheel Well 307 Left Wing Trailing Edge Outboard Flap and Spoilers 407 Right Wing Trailing Edge Outboard Flap and Spoilers
(2)
Access Panels
1103 Forward Access Door
3104 Forward Nose Wheel Well Panel
F.
Procedure
S 865-011
(1) Make sure the pressure in hydraulic systems A and B is removed (Ref 27-61-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-61-00
ALL ú ú 02 Page 503 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 835-012
(2)
Adjust the right aileron control cables (AA and AB):
(a)
Open the forward access door.
(b)
If you installed new aileron control cables AA and AB, adjust the tension (Fig. 501): 1) Use the turnbuckles to tighten the cables to two times the
tension shown in table 1 on Fig. 501. 2) Move the aileron control system through 20 full cycles.
(c)
Install the rig pins A/S-1 and A/S-1A in the transfer mechanism for the first officer's control column (Fig. 502).
NOTE: Make sure the rig pin A/S-1 is fully installed in the
____ transfer mechanism and will not fall out.
1) Make sure you can easily install the rig pin A/S-1 through the bearing housing and the lost motion device in the transfer mechanism.
(d)
Make sure that you can easily install the rig pin A/S-3 in the lower lever at the spoiler control quadrant (Fig. 503).
(e)
Make sure the tension in the aileron control cables AA and AB is in the limits shown in Fig. 501.
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護(hù)手冊 飛行操縱 FLIGHT CONTROLS 5(28)
