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时间:2011-03-31 23:57来源:蓝天飞行翻译 作者:航空
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1

SIDE LOAD ROLLERS FLUSH
BMS 3-33 (4 LOCATIONS) 6 10
A
737-300/400/500MAINTENANCE MANUAL
CARRIAGE BEARING SUPPORT
ACCESS PANEL
CARRIAGE
SUPPORT
FITTING

BMS 3-33
(1 LOCATION)
BORE OF CARRIAGE
5

SUPPORT FITTING
BMS 3-27
12 13 14
11
11  TRACK ROLLERS
11
11

11  FLUSH
BMS 3-33
11 POINTS
(4 LOCATIONS)
3 410
TOGGLE DETENT ROLLER  D
FLUSH
TOGGLE ROLLER BMS 3-33
FLUSH
(1 LOCATION)

11
10

BMS 3-33
(4 LOCATIONS)
11
SEQUENCE
10
CARRIAGE
RUB STRIP
ROLLER 11 FLUSH
BMS 3-33 SLIDER (2 LOCATIONS)
FLAP TRACK  7 10
FLAP TRACK FWDBMS 3-33
(1 LOCATION) FLAP TRACK UPPER
8 POINTS
AND LOWER SURFACE INBD
1
E
Outboard Trailing Edge Flap Lubrication
Figure 302 (Sheet 3)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ROD END
ACTUATOR LINKAGE
(1 LOCATION)


FOREFLAP

ACTUATOR MECHANISM

(2 LOCATIONS)


HINGE EXHAUST GATE HINGE

 

ROD
(1 LOCATION)
(1 LOCATION)

AIRPLANES WITH THREE PUSHRODS


NOTE:REMOVE THE ACCESS PANEL 8215L (LEFT WING) AND 8715R (RIGHT WING) ON LOWER SURFACE OF THE OUTBOARD MIDFLAP FOR ACCESS.
Outboard Trailing Edge Flap Lubrication
Figure 302 (Sheet 4)

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 ú  01  Page 321
 ú  Nov 12/01 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL 
FLUSH ROD END 
MECHANISM ACTUATION EXHAUST GATE  PUSHROD FOREFLAP  BMS 3-33 (1 LOCATION) 4  EXHAUST GATE PUSHROD 
FLUSH ACTUATOR LINKAGE 
BMS 3-33 (1 LOCATION) HINGE 4  FLUSH ACTUATOR LINKAGE 
FLUSH EXHAUST GATE EXHAUST GATE HINGE  BMS 3-33 (2 LOCATIONS) 4 
NOTE:____  BMS 3-33 (2 LOCATIONS) 4 REMOVE THE ACCESS PANEL 8215L (LEFT WING) AND 8715R (RIGHT WING) ON LOWER SURFACE OF THE OUTBOARD MIDFLAP FOR ACCESS.  HINGE 
AIRPLANES WITH TWO PUSHRODS 
6 POINTS 

FLUSH ROLLER BEARING 
ROLLER BEARING 1 POINT  (1 LOCATION) BMS 3-33 

Outboard Trailing Edge Flap Lubrication Figure 302 (Sheet 5) 

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

 

A 737-300/400/500MAINTENANCE MANUAL
APPLY A LARGER AMOUNT OF GREASE TO ALL THE WEAR SURFACES OF THE FLAP TRACKS, FOREFLAP TRACKS, AFTFLAP TRACKS, AND SEQUENCE CARRIAGE TRACKS.
THE LUBRICATION FITTING IS INSTALLED IN THE THREADED END OF THE CAM FOLLOWERS.
LUBRICATE THE ROLLER ASSEMBLY THROUGH THE FITTING IN THE BOLT END.
_______  DO NOT LOOSEN OR REMOVE THE CASTELLATED NUT IMMEDIATELY AFTER YOU LUBRICATE. YOU WILL
CAUTION: MOVE THE SEAL PLATES IN AN OUTWARD DIRECTION.
CAUTION: ON SEALED BEARINGS, DO NOT APPLY GREASE WITH A PRESSURE MORE THAN 1000 PSI AND AT A RATE MORE THAN 0.25 LITER PER MINUTE. WHEN YOU USE A HAND-OPERATED GREASE GUN, DO NOT USE AN EXTENSION HANDLE. YOU CAN CAUSE DAMAGE TO SEALED BEARINGS WITH TOO MUCH PRESSURE.
NOTE:TURN THE ROLLER SLOWLY DURING LUBRICATION.
ON SEALED BEARING, LUBRICATE THE BEARING UNTIL A SMALL AMOUNT OF GREASE CAN BE SEEN AROUND THE EDGE OF THE END PLATE. GREASE WILL NOT FLOW OUT OF THIS BEARING IN LARGE AMOUNTS, SUCH AS YOU SEE ON UNSEALED BEARINGS. THE BEARING CAN BE DIFFICULT TO MOVE BY HAND BECAUSE OF INTERNAL PRESSURE, WHICH WILL DECREASE IN APPROXIMATELY 30 MINUTES. TO DECREASE PRESSURE IMMEDIATELY, PUT A SHORT INSTRUMENT INTO THE LUBE FITTING TO UNSEAT THE SPRING-LOADED CHECK BALL.
 
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