IDLER HINGE
HINGE SEAL
BALANCE ELEVATOR BALANCE PANEL
ACCESS BOLT PANEL 3 POINTS
PANEL
Elevator Control System Lubrication
Figure 301 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
12-22-31
ALL ú ú 01 Page 304 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ELEVATOR
(1 LOCATION PER TAB HINGE, 4 TAB HINGES)
G
AIRPLANES WITH LUBRICATION FITTINGS IN ELEVATOR TAB HINGE FITTINGS
Elevator Control System Lubrication Figure 301 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
12-22-31
ALL ú ú 02 Page 305 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ELEVATOR FEEL COMPUTER INPUT ROD
Elevator Control System Lubrication
Figure 301 (Sheet 5)
L14026
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
12-22-31
ALL ú
ú 02 Page 306
ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ú ú ú ú ú (3) S 423-015Install the elevator PCU input rod lock equipment, C27066, on theelevator PCU input rod to prevent the elevator from moving whilelubricating the elevator hinge bearings.
(4) S 863-006Set the FLT CONTROL A and B switches to OFF.
(5) S 013-009Remove the access panels 9107, 9108, 9109, or 9207, 9208, 9209.
(6) S 643-003Lubricate the elevator hinge bearings (Fig. 301).
NOTE:____ In case of the dust cap dislocation, do the temporary repair of the dust seal (AMM 27-09-83/801).
(7) S 643-004Lubricate the balance panel hinges (Fig. 301): (a) Remove the access panel 9313 or 9413. (b) Remove the bolts that hold the aft part of the balance panel hinge to the elevator nose. (c) Let the aft balance panel hang down. (d) Get access to the balance panel hinges. (e) Lubricate the balance panel hinges. 1) Move the hinges during the lubrication. (f) Install the balance panel bolts. (g) Install the access panel 9313 or 9413. (h) Move the elevator through the full travel by hand to make sure it moves freely.
ú ú ú ú ú ú ú ú S 643-005 (8) Lubricate the hinge fittings of the elevator tab (Fig. 301).S 023-016(9) Remove the elevator PCU input rod lock equipment, C27066, from theelevator PCU input rod.S 863-008(10) Release the control columns to the neutral position and remove theDO-NOT-MOVE tags from the control columns.
S 413-010 (11) Install the access panels 9107, 9108, 9109, or 9207, 9208, 9209.
S 863-011 (12) Set the FLT CONTROL A and B switches to ON.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
12-22-31
ALL ú ú 02.1 Page 307 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
1.
2.
ú ú ú
ú
A
737-300/400/500MAINTENANCE MANUAL
STABILIZER CONTROL SYSTEM LUBRICATION - SERVICING
_________________________________________________General
_______
A. There are three tasks in this procedure. There is one task each for the lubrication of the stabilizer trim jackscrew and the gimbal fittings, the stabilizer trim indicator flexible shaft and the stabilizer trim control system chain. The procedure has these parts:
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(98)
