12-22-51
 ALL  ú ú 03 Page 325 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500MAINTENANCE MANUAL
AFTFLAP TRACK
FLIGHT ROLLER
BMS 3-33

FWD
FLUSH (1 LOCATION) 6
BMS 3-33 (1 LOCATION)
INBD FLIGHT ROLLERS 8
FLUSH
BMS 3-33

(EXAMPLE, 4 LOCATIONS)
(2 LOCATIONS) 7 8 4 POINTS
D
FOREFLAP TRACK FOREFLAP TRACK
ROLLERS FLUSH BMS 3-33
BMS 3-33 (1 LOCATION)
(2 LOCATIONS)FOREFLAP
6
8 SUPPORT TRACK MIDFLAP
FOREFLAP TRACK
ROLLER

FWD FLUSH
BMS 3-33
INBD
(1 LOCATION)

4 POINTS
38
E
Inboard Trailing Edge Flap Lubrication
Figure 303 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-22-51
 ALL  ú ú 01 Page 326 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

AFTFLAP MECHANISM ROLLER
FLUSH 
BMS 3-33 

REMOVE THE ACCESS PANELS 8403L AND 8404L (LEFT WING) OR 8503R AND 8504R (RIGHT WING) ON LOWER SURFACE OF THE INBOARD MIDFLAP FOR ACCESS(1 LOCATION)

A-A

Inboard Trailing Edge Flap Lubrication
Figure 303 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-22-51
 ALL  ú ú 02 Page 327 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FOREFLAP FITTING
LINKAGE
EXHAUST GATE MECHANISM
FLUSH 
BMS 3-33 

(1 LOCATION) EXHAUST
FLUSH 
BMS 3-33 

FOREFLAP
(2 LOCATIONS)
HINGE
(1 LOCATION)

AIRPLANES WITH THREE PUSHRODS

NOTE:  REMOVE THE ACCESS PANEL 8407L (LEFT WING) AND 8507R (RIGHT WING) ON THE LOWER SURFACE OF THE INBOARD MIDFLAP FOR ACCESS.
Inboard Trailing Edge Flap Lubrication
Figure 303 (Sheet 5)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-22-51
 ALL  ú
 ú  01  Page 328
 ú  Nov 12/01 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FOREFLAP FITTING

AIRPLANES WITH TWO PUSHRODS

____REMOVE THE ACCESS PANEL 8407L (LEFT
NOTE: WING) AND 8507R (RIGHT WING) ON THE LOWER SURFACE OF THE INBOARD MIDFLAP FOR ACCESS.
Inboard Trailing Edge Flap Lubrication
Figure 303 (Sheet 6)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-22-51
 ALL  ú
 ú  01  Page 329
 ú  Nov 12/01 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
REMOVE THE INBOARD FLAP TRACK FAIRING PER AMM 27-51-32/401. LUBRICATE THE ROLLER ASSEMBLY
THROUGH THE FITTING IN THE BOLT END.
USE THE LUBRICATION TOOL SET (REF EQUIPMENT AND MATERIALS) TO SIMPLIFY LUBRICATION.
THE FITTING IS ACCESSIBLE THROUGH A SMALL HOLE IN THE LOWER SURFACE OF THE FLAP PANEL.

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.
_______ON SEALED BEARINGS, DO NOT APPLY GREASE WITH A PRESSURE MORE THAN 1000 PSI AND ATCAUTION: A RATE MORE THAN 0.25 LITER PER MINUTE. WHEN YOU USE A HAND-OPERATED GREASE GUN,
DO NOT USE AN EXTENSION HANDLE TO GET MORE FORCE. SEALED BEARINGS CAN BE DAMAGED BY
TOO MUCH PRESSURE.
____EXTEND AND RETRACT THE FLAPS UNTIL THE BEARINGS TURN FREELY AND RELUBRICATE.
NOTE:
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 BLEED PRESSURE IMMEDIATELY, PUT A SHORT INSTRUMENT INTO THE LUBE FITTING TO UNSEAT THE SPRING-LOADED BALL CHECK.
　
中國航空網 www.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(110)