(2)  
31-26-00/501, Aural Warning System
 B.  Access
 (1)  Location Zone
 101/102 Control Cabin
 C.  Procedure
 S 864-002
 (1)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a) P6 Load Control Center - Right 1) LANDING GEAR LIGHTS 2) ANTI-SKID FAIL WARN AND PARK BRAKE 3) AURAL WARN
 (2) 
Remove the crew seat if it is necessary (Ref 25-11-11/201).
 (3) 
Remove the tie rod nut from the left stabilizer trim wheel.
 S 864-003
 S 014-004
 NOTE: It is necessary to remove the trim wheel before you remove
____ the lower access doors on the control stand.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 31-26-21
 ALL  ú ú 01 Page 401 ú Jul 15/96 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A
737-300/400/500
MAINTENANCE MANUAL
THRUSTTHRUST LEVERDRUM 
UPPER 
MOUNTING 
SCREW 
FORWARD CAM 
STOP FOLLOWER ARM 
LOWER MOUNTING SWITCH SCREW BRACKET 
ASSEMBLY ENGINE NO. 2 SWITCH BRACKET ASSEMBLY 
SEE A 
ENGINE NO. 1 SWITCH BRACKET ASSEMBLY 
TAKEOFF WARN SWITCH S815 [INBOARD OF WING ANTI-ICE SWITCH S823 (REF) ON ENG CAM FOLLOWER NO. 2 BRACKET ASSY] ARM 
STOP 
TAKEOFF WARN SWITCH S814 
STOW SWITCH [OUTBOARD OF WING ANTI-ICE 
(S827)(REF) SWITCH S822 (REF) ON ENG NO. 1 BRACKET ASSY] 
ARM SWITCH 
(S826)(REF) 
SWITCH MOUNTING  ARM SWITCH (S824)(REF)  
SCREW  
STOW SWITCH  
BRACKET  (S825)(REF)  
ADJ SLOT  
1  REF. CHAPTER 30-11-52 FOR ADJ/TEST  
OF WING ANTI-ICE SWITCHES S822 AND  
823, REF. CHAPTER 78-34-05 MP FOR  
ADJ/TEST OF THRUST REV ARM/STOW SWITCHES S824-S827  A  1 
Control Stand Thrust Lever Takeoff Warn Switch Installation 
Figure 401 (Sheet 1)
E80217
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT EFIS ú
 31-26-21
 ú ú 02 Page 402 ú Mar 15/95 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A 737-300/400/500MAINTENANCE MANUAL
REF. CHAPTER 30-11-51 FOR ADJ/TEST OF WING ANTI-ICE SWITCHES S822 AND S823 REF. CHAPTER 78-34-05 MP FOR ADJ/TEST OF THRUST REV ARM/STOW SWITCHES S824-S827 
Control Stand Thrust Lever Takeoff Warn Switch Installation Figure 401 (Sheet 2) 
E80219
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
 31-26-21
 ú ú 01 Page 403 ú Mar 15/97 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A 
 
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 仪表 INSTRUMENTS(155)