33-11-71
 ALL  ú ú 01 Page 402 ú Oct 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (e)  
Loosen the fasteners that attach the floodlight to the bracket.

 (f)  
Pull the assembly through the space between the MCP and the lightshield.

 (g)  
Disconnect the string from the floodlight wires.

 NOTE: Keep the string in its position for the installation of
____ the new floodlight wires.
 TASK 33-11-71-404-011
 3.  AFDS Floodlight Installation (Fig. 401)
____________________________
 A.  References
 (1)  AMM 24-22-00/201, Manual Control
 B.  Equipment
 (1)  String, ten foot length
 C.  Access
 (1)  Location Zone
 101 Control Cabin - Left
 102 Control Cabin - Right

 D.  Procedure
 S 424-027
 (1)  Install the Floodlight:
 (a)  
Install the sleeve on the wires of the replacement floodlight.

 (b)  
Attach the string to the wires of the replacement floodlight.

 (c)  
Use the string to pull the replacement floodlight wires into the wire bundle.

 (d)  
Install the replacement floodlight assembly.

 (e)  
Tighten the fasteners that attach the floodlight to the light shield.

 (f)  
Remove the string.

 (g)  
Connect the floodlights assembly wires.

 (h)  
Tighten the screws that hold the MCP.

 (i)  
Remove the DO-NOT-CLOSE tag and close this circuit breaker:

 1)  P6 Load Control Center - Right a) AFDS FLOOD LT
 S 714-029
 (2)  Do a test of the AFDS floodlight:
 (a)  Supply electrical power (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 33-11-71
 ALL  ú ú 01 Page 403 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (b) (c) (d)  Turn the AFDS FLOOD switch on the P1 panel to the full BRIGHT position.Make sure that the floodlight comes on.Remove the electrical power if it is not necessary (AMM 24-22-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 33-11-71
 ALL  ú ú 01 Page 404 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 STABILIZER TRIM WARNING LIGHT - MAINTENANCE PRACTICES
_____________________________________________________
 1.  General_______
 A.  The Korry 432 series stabilizer trim warning light is made up of two components: a removable cap assembly that contains four lamps and a base assembly. The base assembly contains a logic module and switches for the warning light press to test light function. To relamp the warning light you withdraw the cap assembly from the base, replace the faulty lamps and insert the cap assembly into the base.
 B.  This procedure contains this task:
 (1) The replacement of the stabilizer trim warning light lamps.
 TASK 33-11-80-962-007
 2.  Stabilizer Trim Warning Light Lamp Replacement (Fig. 201)______________________________________________
 A.  References
 (1)  
WDM 22-13-11

 (2)  
WDM 22-13-12

 (3)  
WDM 33-18-03

 (4)  
WDM 33-18-11

 (5)  
WDM 33-18-13

 B.  Access
 (1)  Location Zone
 101 Control Cabin - Left

 C.  Procedure
 S 862-002
 (1)  Prepare To Relamp
 (a)  
Provide electrical power (AMM 24-22-00/201).

 (b)  
Momentarily press and hold the master dim and test LIGHTS switch (P1-3) to the TEST position to identify the faulty lamp(s).

 (c)  
Open these circuit breakers and attach DO-NOT-CLOSE tags: 1) Load Control Center, P6-3 a) MASTER DIM SECT 2
　
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 燈 LIGHTS(10)