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 (1) D00633 Grease - BMS 3-33 (Preferred) (2) D00015 Grease - BMS-3-24 (Optional) (3) D00071 Lubricating Oil MIL-L-7808 C. References
 (1) AMM 27-09-83/801, Flight Control Hinge Bearing Dust Seals (2) AMM 27-31-00/201, Elevator and Tab Control System D. Access
 (1) Location Zone 711, 712 Elevator and Tab (2) Access Panels 9107/9207 Access Panel Trailing Edge 9108/9208 Access Panel Trailing Edge 9109/9209 Access Panel Trailing Edge 9313/9413 Elevator Mast Fitting Fairing E. Procedure
 S 863-013
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS
 AND DAMAGE TO EQUIPMENT.
 ú  (1) Pressurize the elevator hydraulic systems A and B (AMM 27-31-00/201).
 ú  S 863-002
 ú ú ú  (2) Move a control column full aft and hold both control columns in thefull aft position so that they cannot move. Attach DO-NOT-MOVE tagsto the control columns.

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 ALL  ú ú 01.1 Page 301 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

(1 LOCATION PER
MASTER ARM FITTING
HINGE, 1 HINGE)

1 POINT

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 TO GET MORE FORCE. SEALED BEARINGS CAN BE DAMAGED BY TOO MUCH PRESSURE.
Elevator Control System Lubrication
Figure 301 (Sheet 1)

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 ALL  ú
 ú  01  Page 302
 ú  Mar 12/00 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
ELEVATOR
FRONT SPAR ELEVATOR BEARING PLATE
ELEVATOR HINGE
FLUSH
BMS 3-33
(2 LOCATIONS PER
HINGE, 2 HINGES)

1
AIRPLANES WITH PILLOW BLOCK
NO. 1 AND 2 ELEVATOR HINGE FITTINGS

2 POINTS

C

ELEVATOR FRONT SPAR
ELEVATOR
BEARING
PLATE

ELEVATOR HINGE
ELEVATOR HINGE FLUSH
FLUSH
BMS 3-33
BMS 3-33
(1 LOCATION PER

(1 LOCATION PER HINGE, 1 HINGE)
HINGE, 3 HINGES) 1
1
NO. 6 ELEVATOR HINGE FITTING
NO. 3 THRU NO. 5 ELEVATOR HINGE FITTINGS 1 POINT
1 POINT
E
D
Elevator Control System Lubrication
Figure 301 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
2  TO GET ACCESS TO THE PUSHROD  OUTOUT TORQUE 
OR OUTPUT TORQUE TUBE, GO  TUBE 
THE TOP OF THE HORIZONTAL  FLUSH 
STABILIZER AND PUSH DOWN ON 
THE STABILIZER TO EMPANNAGE  BMS 3-33 
AERODYNAMIC SEAL. 
(1 LOCATION) 
3  REMOVE ACCESS PANEL.  REMOVE  2  4 
BOLTS HOLDING FORWARD PORTION 
OF EACH BALANCE PANEL HINGE TO 
THE IDLER HINGE.  LET FORWARD  ELEVATOR CONTROL 
PORTION OF BALANCE PANEL HANG  PUSHROD  OUTPUT 
DOWN.  GAIN ACCESS TO HINGE AND  FLUSH  TORQUE 
LUBRICATE.  CYCLE HINGE DURING  TUBE 
LUBRICATION.  INSTALL BALANCE 
PANEL BOLTS AND ACCESS PANEL.  BMS 3-33 
CYCLE ELEVATOR FULL TRAVEL BY  (1 LOCATION) 
HAND TO CHECK FOR BINDING. 
2  4 
CAUTION:  WHEN INSTALLING BALANCE 
PANEL BOLTS ENSURE IDLER 
HINGE IS POSITIONED DOWNWARD  ELEVATOR 
　
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