(b)  
Put the POWER DRIVE SYSTEM switch in the ON position for the aft compartment or in the FWD or AFT DRIVES position for the forward compartment.

 (c)  
Put the LATERAL GUIDE switch in the RETRACT position for the aft compartment or in the RETRACT FWD or RETRACT BOTH for the forward compartment as applicable.

 (d)  
Put the POWER DRIVE SYSTEM switch in the OFF position and open the applicable circuit breakers.

 S 025-020
 (2)  
Remove the ball-transfer panels if it is necessary to get access to the lateral guide actuator and linkage (AMM 25-53-15/401).

 S 825-021

 (3)  
Adjust the retractable guide rails.

 NOTE: Use this procedure to adjust each set of retractable guide
____ rails in the forward and aft cargo compartment. Adjusting one guide rail can change the adjustment of other guide rails in the same set. Thus, if one guide rail needs adjustment, adjust the full set of guide rails.
 (a)  Disconnect the preset rod assembly that holds the crank assembly to the crank arm linkage of the guide rail.
 NOTE: Skip these three step (for the preset rod assembly) when
____ you adjust the aft guide rails in the forward cargo compartment. These guide rails do not have a preset rod assembly.
 (b) Adjust the preset rod to 6.20 (+/- 0.01) inches.
 NOTE: Push-fit bushings are used in the rod and crank arm
____ assembly. If you remove these bushings, clean and lubricate them with grease before you install them again.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 25-53-00
 ALL  ú ú 01A Page 508 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
GUIDE RAIL
(EXTENED)

2.67-2.88 INCHES
(DIMENSION B)

CRANK ARM LINKAGE
SEE D
1
PRESET ROD ASSEMBLY GUIDE RAIL (RETRACTED)
SEE B
0.80 |0.06 INCH (DIMENSION A)
ROD ASSEMBLY
INBD
CRANK ASSEMBLY GUIDE RAIL FWD
SUPPORT
ACTUATOR
ROD END
BEARING

CRANK ARM
ROD ASSEMBLY SEE C LINKAGE
SEE D
ACTUATOR
RETRACTABLE GUIDE RAIL LINKAGE
A
2

0.80 |0.06 INCH (DIMENSION A) ROD ASSEMBLY
CRANK ARM1 THE GUIDE RAIL CONFIGURATION LINKAGE
IN THE AFT CARGO COMPARTMENT
AND THE FORWARD GUIDE RAIL SEE E
CONFIGURATION IN THE FORWARD
CARGO COMPARTMENT

ROD
ACTUATOR
ASSEMBLY
ROD END
2
THE AFT GUIDE RAIL CONFIGURATION
IN THE FORWARD CARGO COMPARTMENT

BEARING
Lateral Guide Rail Adjustment
Figure 502 (Sheet 1)

L46262
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 25-53-00
 ALL  ú ú 01A Page 509 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

WASHER
PRESS-FIT
BUSHING

NUT
WASHER
SPACER

BOLT BUSHING CRANK
PRESET ROD ASSEMBLY
PUSH-FIT  (NON-ADJUSTABLE WASHER
BUSHING END) CRANK NUT
ROD ASSEMBLY
(ADJUSTABLE END)
PRESET ROD ASSEMBLY
B  PRESS-FIT
BUSHING
ROD ASSEMBLY  WASHER
(ADJUSTABLE END) PRESS-FIT ACTUATOR
BUSHING ROD END
(2 LOCATIONS)  PUSH-FIT BEARING
BUSHINGWASHER
BOLT
NUT 1.02-1.31 INCHES (DIMENSION X)
3
WASHER  ACTUATOR ROD END BEARING
SPACER
BUSHING
C
ROD ASSEMBLY BOLT (NON-ADJUSTABLE END)
CRANK ARM PRESS-FIT AND SPACER BUSHINGPRESS-FIT
PUSH-FIT
(2 LOCATIONS)BUSHING
BUSHING
PRESS-FIT(2 LOCATIONS)
(PRESS-FIT  CRANK ARMBUSHING BUSHING ON LINKAGE FAR SIDE)
CRANK ARM LINKAGE
D

BOLT
ROD ASSEMBLY
WASHER
WASHER ROD ASSEMBLY (ADJUSTABLE NUT END)
ACTUATOR ROD END BEARING
1.02-1.31 INCHES
(DIMENSION X)
3
CRANK ARM LINKAGE
3
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 EQUIPMENT/FURNISHINGS 1(138)