(10)
Pull the adjustment shaft and the support bracket forward to disengage the adjustment shaft.
S 034-014
(11)
Remove the bolts that hold the jackshaft support channel to the structure, and remove the channel.
NOTE:____Hold the weight of the quadrant during this step. The quadrant is free to fall from the top housing after you disconnect the bolts.
S 034-015
(12) If it is necessary, disconnect the four bolts that hold the bearing housing to the jackshaft support channel, and replace the lower bearing.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-51
ALL ú ú 01 Page 402 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
FORWARD RUDDER ADJUSTMENT CRANK CONTROL QUADRANT FOR THE (LEFT) ADJUSTMENT SHAFT
RUDDER PEDAL SUPPORT BRACKET
STRUCTURE
JACKSHAFT
SUPPORT
CHANNEL RUDDER
ADJUSTMENT SHAFTPEDALS
ASSEMBLY FOR THE SEE A
RUDDER PEDAL JACKSHAFT AND FORWARD QUADRANT
PUSHROD
(EXAMPLE) SEE B
CABIN
FLOOR RIG PIN
BEAM
(R-1 CAPTAIN'S PEDALS)
(R-2 FIRST OFFICER'S PEDALS)
FWD
RUDDER PEDALS A
BUSROD
FORWARD QUADRANT
PUSHROD
RUDDER CABLE
RIG PIN INSTALLATION
SEE C
RUDDER PEDAL
TENSION ROD
CABLE GUARD BLOCK FORWARD RIG
RUDDER PEDAL STEERING ARM PIN HOLE
(LEFT QUADRANT ONLY) JACKSHAFT RIG PIN (R-3 FOR THE CAPTAIN'S QUADRANT)SUPPORT CHANNEL FWD (R-4 FOR THE FIRST OFFICER'S QUADRANT)
JACKSHAFT AND
FORWARD QUADRANT
B
Rudder Forward Quadrant Installation
Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-51
ALL ú ú 01 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 024-016
(13) Move the jackshaft assembly and the quadrant to the aft and outboard direction, and remove it from the airplane.
TASK 27-21-51-424-002
3. Rudder Forward Quadrant Installation____________________________________
A. Special Tools and Equipment
(1) Rigging Pins Kit - F70207-93:
RIG PIN INSTALLATION
C Rudder Forward Quadrant Installation Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-51
ALL ú ú 03 Page 404 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 | ................................................................................. | R-1 | -14 | 0.309-0.311 | 12.7 |0.25 |CAPTAINS RUDDER PEDAL | | R-2 | -14 | 0.309-0.311 | 12.7 |0.25 |FIRST OFFICERS RUDDER PEDAL| | R-3 | -11 | 0.309-0.311 | 6.7 |0.25 |CAPTAINS RUDDER FORWARD | | | | | | QUADRANT | | R-4 | -11 | 0.309-0.311 | 6.7 |0.25 |FIRST OFFICERS RUDDER | | | | | | FORWARD QUADRANT | | R-5 | -11 | 0.309-0.311 | 6.7 |0.25 |RUDDER FEEL AND CENTERING | | | | | | UNIT | 2.........…............…..............….............…...........................1
B. Standard Tools and Equipment
(1)
Cable Tensiometer -0 to 300 Pound Range for 1/8-inch Diameter Cable
C.
Consumable Materials
(1)
D00015 Grease, Corrosion Preventive - BMS 3-24
D.
References
(1)
12-31-11/201, Body Section 41 Access Doors and Panels
(2)
27-21-00/201, Rudder and Rudder Trim Control System
(3)
31-24-42/401, Rudder Pedal Position Sensor
E.
Access
(1)
Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 2(52)
