B.
Access
(1)
Location Zone
101, 102 Control Cabin
C.
Procedure
(1)
Connect the electrical connectors to the module.
(2)
Install the module in the aft overhead panel with the 4 fasteners.
S 434-006
S 424-007
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-32-21
ALL ú ú 01 Page 402 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 864-014
(3) AIRPLANES WITH DIGITAL STALL WARNING COMPUTER P/N 65-52819;
Close these circuit breakers:
(a) P6 Panel
1) STALL WARN 2 AC
2) STALL WARN 2 DC
(b) P18 Panel
1) STALL WARN 1 AC
2) STALL WARN 1 DC
S 864-015
(4) AIRPLANES WITH STALL MANAGEMENT COMPUTER P/N 65-52822;
Close these circuit breakers:
(a) P6 Panel
1) SMC 2 CMPTR DC
(b) P18 Panel
1) SMC 1 CMPTR DC
S 864-009
(5) Supply electrical power (AMM 24-22-00/201).
S 714-010
(6) Do a test of the module:
(a) Push and hold the STALL WARNING TEST NO. 1 switch on the
module.
(b) Make sure that the captain's control column shaker operates.
(c) Release the switch.
(d) Make sure that the shaker stops.
(e) Push and hold the STALL WARNING TEST NO. 2 switch on the
module.
(f) Make sure that the first officer's control column shaker
operates.
(g) Release the switch.
(h) Make sure that the shaker stops.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-32-21
ALL ú ú 01 Page 403 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 864-011
(7) Remove electrical power (Ref 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-32-21
ALL ú ú 01 Page 404 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CONTROL COLUMN SHAKER - REMOVAL/INSTALLATION
____________________________________________
1. General_______
A. This subject contains two tasks, one for the removal and one for the installation of the control column shaker. The procedure is the same for the captain's or the first officer's control column shaker.
TASK 27-32-31-004-001
2. Control Column Shaker Removal (Fig. 401)_____________________________
A. Access
(1)
Location Zone
101, 102 Control Cabin
B.
Procedure
S 864-012
(1)
AIRPLANES WITH DIGITAL STALL WARNING COMPUTER P/N 65-52819; Open these circuit breakers:
(a)
P6 Panel
1) STALL WARN 2 AC
2) STALL WARN 2 DC
(b)
P18 Panel
1) STALL WARN 1 AC
TYPICAL CAPTAIN OR FIRST OFFICER
Control Column Shaker Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-32-31
ALL ú ú 02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
2) STALL WARN 1 DC
S 864-013
(2)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(63)
