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CAUTION:  ON SEALED BEARINGS, DO NOT APPLY GREASE WITH A PRESSURE GREATER THAN 1000 PSI AND AT A RATE GREATER THAN 0.25 LITER PER MINUTE. WHEN USING A HAND-OPERATED GREASE GUN, DO NOT USE EXTENSION HANDLE TO GAIN MORE FORCE. SEALED BEARINGS MAY BE DAMAGE BY EXCESSIVE PRESSURE.
NOTE:  EXTEND AND RETRACT FLAPS UNTIL BEARINGS TURN FREELY AND RELUBRICATE.
ON SEALED BEARING LUBRICATE BEARING UNTIL TINY AMOUNT OF GREASE CAN BE SEEN FORMING AROUND PERIPHERY OF END PLATE. GREASE WILL NOT FLOW OUT OF THIS BEARING IN LARGE AMOUNTS, SUCH AS OBSERVED ON UNSEALED BEARING. BEARING MAY BE DIFFICULT TO MOVE BY HAND BECAUSE OF INTERNAL PRESSURE, WHICH WILL DISSIPATE IN APPROXIMATELY 30 MINUTES. TO BLEED OFF PRESSURE IMMEDIATELY INSERT A SHORT INSTRUMENT INTO LUBE FITTING TO UNSEAT SPRING-LOADED BALL CHECK.
CAUTION:  DO NOT LOOSEN OR REMOVE CASTELLATED NUT IMMEDIATELY AFTER LUBRICATION. TO DO SO WILL DESPLACE SEAL PLATES IN AN OUTWARD DIRECTION.
ON UNSEALED BEARINGS, LUBRICATE BEARING UNTIL LUBRICANT FLOWS FREELY AROUND PREIPHERY OF END PLATE.
500  Inboard Trailing Edge Flap Lubrication 
Aug 01/95  Figure 203 (Sheet 3)  12-22-51 
Page 211 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

G42306
Inboard Trailing Edge Flap Lubrication  500 
12-22-51  Figure 203 (Sheet 4)  May 01/03 
Page 212 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

554  Inboard Trailing Edge Flap Lubrication 
May 01/03  Figure 203 (Sheet 5)  12-22-51 
Page 213 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

H21556
Hinged Flap Lubrication  500 
12-22-51  Figure 204  May 01/03 
Page 214 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

500  Spoiler Lubrication 
May 01/01  Figure 201 (Sheet 1)  12-22-61 
Page 201 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

 Spoiler Lubrication  500 
12-22-61  Figure 201 (Sheet 2)  May 01/01 
Page 202 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

500  Spoiler Actuator Quadrant Lubrication 
May 01/01  Figure 202  12-22-61 
Page 203 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

H21562
500  Leading Edge Slat Lubrication 
May 01/01  Figure 201  12-22-71 
Page 201 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

500  Speed Brake Forward Drum and Level Brake Lubrication 
Oct 20/91  Figure 201  12-22-81 
Page 201 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

Ground Spoiler Interlock Value Cable Installation  574 
12-22-81  Figure 202 (Sheet 1)  Oct 20/91 
Page 202 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

1.  Completely Lubricate the Ground Spoiler Interlock Valve Cable
A.  Remove flexible cable. Replace cable if corroded or worn (Ref\27-62-51 R/I).
B.  Apply a liberal coating of grease to entire length of cable and to faying surfaces of swivel tube and guide tube at each end of cable.
C.  Reinstall flexible cable (Ref 27-62-51).
D.  With bolt removed that attaches lower rod end to landing gear torsion link, cycle cable through full travel a minimum of 6 times. Force required to push cable should be less than 18.0 pounds at fully extended position. Force required to extend the cable should be less than 15.0 pounds at fully compressed position. Replace cable if force is excessive.
E.  Wipe off excess grease on upper end. Leave a generous grease coating on all components within boot.
F.  Reposition and reclamp protective boot on lower end. Install lower rod end bolt. Adjust and test cable (Ref 27-62-51).
2.  Partially Lubricate the Ground Spoiler Interlock Valve Cable at Each End
A.  Remove bolt attaching lower rod end to landing gear torsion link.
B.  Remove protective boot on lower end.
C.  Apply grease to fitting, if installed, at each end of cable.
NOTE: Some grease may extrude out on cable outer surface.
D.  Apply a liberal coating of grease to faying surfaces of swivel tube and guide tube at each end of cable.
　
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