(2)
AMM 27-81-00/201, Leading Edge Flap and Slat Control System
B. Access
(1)
Location Zones
302 Left Wing Outboard Leading Edge
402 Right Wing Outboard Leading Edge
(2)
Access Panels
6212L Left Wing Slat Access Panel
6512R Right Wing Slat Access Panel
C. Procedure
S 494-008
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO INSTALL
_______ THE LEADING EDGE FLAPS AND SLATS LOCKS. IF YOU DO NOT INSTALL THE LOCKS CORRECTLY, THE LEADING EDGE FLAPS CAN MOVE QUICKLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(1)
Do this task: "Leading Edge Flaps and Slats Locks Installation" (AMM 27-81-00/201).
S 864-009
(2)
Open this circuit breaker:
(a) P18 Panel
1) ENG 1 & WING ANTI-ICE CONTROL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
30-11-21
ALL ú ú 02 Page 401 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
FWD
INBD
A
Wing Anti-Icing Ground Overheat Thermal Switch Installation
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
30-11-21
ALL ú ú 01 Page 402 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 014-019
(3) Remove the access panels as required (AMM 12-30-00/201).
(a)
Remove the 6212L panel from the left wing.
(b)
Remove the 6512R panel from the right wing.
S 034-011
(4)
Disconnect the electrical connector from the thermal switch.
S 024-012
(5)
Remove the thermal switch. Discard the gasket.
TASK 30-11-21-424-007
3. Wing Anti-Icing Ground Overheat Thermal Switch Installation (Fig. 401)
___________________________________________________________
A. References
(1)
AMM 24-22-00/201, Manual Control
(2)
AMM 12-30-00/201, Wing Lower Surface Access Panels
(3)
AMM 27-81-00/201, Leading Edge Flap and Slat Control System
B. Access
(1)
Location Zones
302 Left Wing Outboard Leading Edge
402 Right Wing Outboard Leading Edge
(2)
Access Panels
6212L Left Wing Slat Access Panel
6512R Right Wing Slat Access Panel
C. Thermal Switch Installation
S 434-013
(1)
Install the gasket on the thermal switch and install the switch into the duct boss.
S 434-014
(2)
Connect the electrical connector to the thermal switch.
NOTE: If you will do the Test of the Thermal Switch Circuit, do not
____ connect the electrical connector until after that test.
D. Test of the Thermal Switch Circuit
S 864-013
(1)
Supply electrical power (AMM 24-22-00/201):
S 714-016
(2)
Do a test of the thermal switch circuit:
(a)
Set the WING ANTI-ICE switch (P5 overhead panel) to ON.
(b)
Use a jumper to connect the pins 1 and 2 of the switch connector (D738 - left wing, D736 - right wing).
(c)
Make sure that the L VALVE OPEN and R VALVE OPEN lights come on brightly and continuously.
(d)
Remove the jumper from the thermal switch connector.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
30-11-21
ALL ú ú 03 Page 403 ú Jul 12/01
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 防冰和排雨(21)
