(b)  
Remove the cable clamps and keep a record of their location.

 NOTE: The clamp locations are not the same for the captain's
____ and the first officer's cables.
 (c)  Hold the cable retaining nut and washer and pull the cable forward to remove it from the rudder jackshaft.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-41
 ALL  ú ú 02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
RUDDER PEDALS
SEE A
RUDDER PEDAL
CRANK
BEARING SUPPORT BRACKET
HOUSING

RUDDER PEDAL
ADJUSTMENT CRANK
BOLT (4 LOCATIONS)
GROMMET
CABLE CLAMP
RUDDER PEDAL
ADJUSTMENT
CABLE

CABLE GUARD (ON THE FIRST OFFICER'S CABLE ONLY)
SEE C
FWD
CABLE RETAINING
RUDDER NUT
JACKSHAFT
SEE B
RUDDER PEDALS (CAPTAIN'S PEDALS SHOWN, FIRST OFFICER'S PEDALS ARE OPPOSITE)
A
Rudder Pedal Adjustment Crank Installation
Figure 401 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-41
 ALL  ú ú 01 Page 402 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

WASHER

RETAINING NUT
RUDDER JACKSHAFT

RUDDER PEDAL ADJUSTMENT CABLE
CABLE GUARD
(ON THE FIRST OFFICER'S CABLE ONLY)

Rudder Pedal Adjustment Crank Installation
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-41
 ALL  ú ú 02 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 034-005
 (4)  
Disconnect the top part of the cable:

 (a)  
Remove the four bolts that connect the bearing housing to the crank support bracket.

 (b)  
Move the adjustment crank fully down to get clearance between the adjustment crank and the crank support bracket.

 (c)  
Pull the crank, bearing housing, and cable rearward to remove it from the airplane.

 S 034-006
 (5)  On the first officer's cable,
 remove the 13-inch long nylon tube from the cable.

 TASK 27-21-41-424-007
 3.  Rudder Pedal Adjustment Crank Installation__________________________________________
 A.  References
 (1)  
12-31-11/201, Access Doors

 (2)  
27-21-00/501, Rudder and Rudder Trim Control System

 B.  
Access

 (1)  
Location Zones
 202 Lower Nose Compartment

 (2)  
Access Panel
 1103 Forward Access Door

 C.  
Procedure (Fig. 401)

 S 434-008
 (1)  
Connect the top part of the cable:

 (a)  
Push the cable through the crank support bracket.

 (b)  
Move the bottom end of the cable near the rudder jackshaft.

 (c)  
Install the four bolts that connect the bearing housing to the crank support bracket.

 S 434-009
 (2)
Install the lower part of the rudder pedal adjustment cable:

 (a)  
Push the cable through the jackshaft support. 1) Put the cable retaining nut and washer on the cable.

 (b)  
Put the end of the cable in the jackshaft.

 1)  Turn the cable until the cable engages the pin in the rudder jackshaft.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-21-41
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 2(50)