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

 S 643-005
 CAUTION:_______ BE CAREFUL WHEN YOU DISENGAGE THE GREASE GUN FROM THE LUBRICATION FITTING. THE GREASE GUN CAN CAUSE DAMAGE TO THE FITTING.
 (2)  Lubricate the upper end of the main landing gear (Fig. 301).
 (3)  S 643-010Lubricate the lower end of the main landing (Fig. 302).
 (4)  S 643-011Lubricate the uplock assembly (Fig. 303).
 S 643-012 (5) Lubricate the Brake assembly on the main landing gear (Fig. 304). F. Put the Airplane Back to Its Usual Condition
 (1)  S 413-009Install the main gear actuator panels 551BB/651BB (AMM 06-44-00/201).
 S 093-006
 WARNING:_______ OBEY THE REMOVAL PROCEDURE FOR THE DOOR LOCKS. THE DOORS OPEN AND CLOSE QUICKLY. THE MOVEMENT OF THE DOORS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  Remove the door locks and close the doors (AMM 32-00-15/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-14
 ALL  ú ú 01.1 Page 302 ú Sep 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

TRUNNION LINK TRUNNION LINK

 

7 POINTS

ONE MORE LUBE POINT IS ON THE OPPOSITE SIDE (NOT SHOWN).
Lubrication on the Upper End of the Main Landing Gear
Figure 301 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-14
 ALL  ú
 ú  01  Page 303
 ú  May 28/01 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

757
MAINTENANCE MANUAL

ACTUATOR RETRACT  SUPPORT TRUNNION FORWARD 
SEE  F  SHT 6  LINK REACTION SHT 4CSEE  LINK REACTION 
SUPPORT LINK SIDE STRUT 
ACTUATOR DOWNLOCK  SEE  E  SHT 5 
ASSEMBLY DOWNLOCK SHT 7HSEE  I SHT 8 SEE  JOINT REACTION LINK SIDE STRUT/ SHT 4DSEE 
SIDE STRUT ZERK  1 1  SIDE STRUT ZERK 
BMS 3-33  1  BMS 3-33 
(2 LOCATIONS)  SIDE STRUT  (4 LOCATIONS) 
ZERK 
BMS 3-33 
(2 LOCATIONS) 

INBD
LEFT MAIN LANDING GEAR 8 POINTS
1 ONE MORE LUBE POINT IS ON THE OPPOSITE SIDE (NOT SHOWN).
Lubrication on the Upper End of the Main Landing Gear Figure 301 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-14
 ALL  ú ú 01 Page 304 ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

AFT
TRUNNION

AFT TRUNNION BEARING ZERK
BMS 3-33 (1 LOCATION) 23
FLAP TRACK FAIRING
REACTION LINK (REF)
AFT TRUNNION BEARING
(VIEW IN THE FORWARD DIRECTION)
1 POINT

A
FORWARD TRUNNION BEARING ZERK
BMS 3-33 (1 LOCATION) FWD
23
FORWARD TRUNNION BEARINGTRUNNION LINK (REF)
FORWARD TRUNNION BEARING
2
LUBRICATE TO 400 PSI  1 POINT
MAXIMUM PRESSURE
3
THE AFT TRUNNION BEARING LUBE FITTING  B
IS ACCESSIBLE WITH THE FLAPS EXTENDED.
Lubrication on the Upper End of the Main Landing Gear
Figure 301 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 12-21-14
 ALL  ú ú 01 Page 305 ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

REACTION LINK
ATTACH FITTING REACTION LINK
ZERK
BMS 3-33
(1 LOCATION ON
TOP OF FITTING
REACTION LINK
NOT SHOWN)

ZERK
1
BMS 3-33 (2 LOCATIONS)
TRUNNION
LINK (REF)
FORWARD
TRUNNION
BEARING

FWD REACTION LINK
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 SERVICING 2(40)