曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

ON UNSEALED BEARINGS, LUBRICATE THE BEARING UNTIL LUBRICANT FLOWS FREELY AROUND THE EDGES OF THE END PLATE.
APPLY A LARGE QUANTITY OF GREASE AROUND THE SLOTTED HOLE AND ON THE EDGES OF THE BEARING
THE LUBE FITTING CAN BE INSTALLED ON THE UPPER SIDE OR ON THE LOWER SIDE OF THE ROLLER ASSEMBLY.
EXTEND THE FLAPS UNTIL THE MAIN CARRIAGE MOVES 0.10 INCH PAST THE SEQUENCE CARRIAGE (APPROXIMATELY 9.0 UNITS FOR THE INBOARD CARRIAGE AND 9.5 UNITS FOR THE OUTBOARD CARRIAGE). USE ALEMITE NUMBER 6783 GREASE NOZZLE ON GREASE GUN.
THERE ARE THREE LUBRICATION FITTINGS ON THE BOLT. ONLY 1 OF THE 2 LOCATED IN THE BOLT HEAD AND 1 LOCATED IN THE THREADED END REQUIRES LUBRICATION.
USE A NEEDLE NOSE GREASE GUN.
LUBRICATION FITTINGS ARE NOT INSTALLED ON ALL AIRPLANES. AIRPLANES WITHOUT LUBRICATION FITTINGS HAVE SELF-LUBRICATED ROLLERS.
ONE MORE LUBE POINT IS ON THE OPPOSITE SIDE (NOT SHOWN).
APPLY BMS 3-27 (MASTINOX 6856K) BETWEEN THE CARRIAGE SUPPORT FITTING AND THE OUTER RACE OF THE THE SPHERICAL BEARING WHEN YOU INSTALL THE SPHERICAL BEARING. APPLY AT WBL 254 AND WBL 355 ON THE OUTBOARD FLAP (AMM 27-51-44/401).
WARNING:  USE NITRILE GLOVES FOR SKIN PROTECTION AGAINST BMS 3-27 (MASTINOX 6856K). IF MASTINOX GETS ON YOUR SKIN, IMMEDIATELY REMOVE IT WITH WATER. IF THIS MATERIAL GETS IN YOUR EYES, IMMEDIATELY FLUSH YOUR EYES WITH WATER AND GET MEDICAL AID. THIS MATERIAL CONTAINS VERY POISONOUS AND FLAMMABLE AGENTS WHICH CAN CAUSE INJURIES TO PERSONS.
CAUTION:  REMOVE UNWANTED MASTINOX FROM SURFACES WHICH WILL BE LUBRICATED AND FROM SURFACES THAT MOVE. YOU CAN CAUSE FAILURE OF MOVING PARTS IF YOU APPLY MASTINOX TO SURFACES THAT MOVE.
Outboard Trailing Edge Flap Lubrication
Figure 302 (Sheet 6)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-22-51
 ALL  ú ú 01 Page 323 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

INBOARD FLAPS SEE A
INBOARD CARRIAGE SEE B
A
AFTFLAP TRACKS SEE D
A
FLAP TRACKS
FOREFLAP TRACK
SEE F

BMS 3-33
FOREFLAP TRACK
ALL CONTACT

SURFACES OF THE
SEE E
TWO FLAP TRACKS
(2 LOCATIONS)
INBD

6
FOREFLAP TRACK
FWD

SEE F OUTBOARD CARRIAGE
2 POINTS
NOTE:UNLESS OTHERWISE NOTED, YOU
EXHAUST GATE SEE C CAN GET ACCESS TO ALL OF THE MECHANISM LUBRICATION POINTS WHEN THE A
SEE GFLAPS ARE EXTENDED.
Inboard Trailing Edge Flap Lubrication
Figure 303 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-22-51
 ALL  ú ú 02 Page 324 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SIDE ROLLERS FLUSH
BMS 3-33 UNDER ROLLER (2 LOCATIONS)
9
MAIN TRACK ROLLERS
28 FLUSH
TOGGLE ROLLER (NOT SHOWN) FLUSH BMS 3-33 9
(2 LOCATIONS)
BMS 3-33  INBD  1  2  5  8 
(1 LOCATION) 
2 
9 
FWD 
9 
TOGGLE ROLLERS 
BOOM ROLLER  FLUSH 
FLUSH 
9  BMS 3-33  BMS 3-33 
(4 LOCATIONS) 
FOREFLAP CAM TRACKS  MAIN TRACK ROLLERS FLUSH  ONLY ACCESSIBLE INBOARD CARRIAGE  2  8 
WITH FLAPS AT 
40-UNIT POSITION 
BMS 3-33  (1 LOCATION) 
BMS 3-33  (2 LOCATIONS)  2 
(2 LOCATIONS)  1  2  5 
6 
8 
INBOARD CARRIAGE 
SIDE ROLLERS (NOT SHOWN)  14 POINTS 
FLUSH  B 

BMS 3-33 (2 LOCATIONS)
TOGGLE ROLLERS
928
FLUSH
TOGGLE ROLLERS BMS 3-33
FLUSH (1 LOCATION) 9 28
BMS 3-33 (4 LOCATIONS)
FOREFLAP CAM
28
TRACKS
MAIN TRACK ROLLERS FLUSH
BMS 3-33 INBD  OUTBOARD CARRIAGE
BMS 3-33
(2 LOCATIONS)  13 POINTS
(4 LOCATIONS)
6 125
C
FWD
Inboard Trailing Edge Flap Lubrication
Figure 303 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
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 SERVICING(109)