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 CONTROL PANEL, M10397 
RELAY - R WING DISAGREE, K2  -- 1 FLT COMPT, P5, ANTI-ICE  *
 CONTROL PANEL, M10397 
SWITCH-LIGHT - WING ANTI-ICE, S3  -- 1  FLT COMPT, P5, ANTI-ICE CONTROL  * 
PANEL, M10397 
VALVE - L WING ANTI-ICE, V52  -- 1  521UBX, FIXED WING LOWER PANEL  30-11-02
VALVE - R WING ANTI-ICE, V57 -- 1  621UBX, FIXED WING LOWER PANEL  30-11-02 

* SEE THE WDM EQUIPMENT LISTTHIS CIRCUIT BREAKER CAN BE IN ONE OF THESE LOCATIONS

Wing Thermal Anti-Ice System - Component Index
Figure 101

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757
FAULT ISOLATION/MAINT MANUAL

P11 PANEL WING AND ENGINE
P5 PANEL
ANTI-ICE CONTROL PANEL, M10397
SEE A
VALVE LIGHT, L2
FLIGHT COMPARTMENT
WING  ANTI-ICE 
SWITCH-LIGHT, S3 
ON  ENGINE 
w  L  R 
L  R 
w  ON  ON 
w  w 
VALVE LIGHT, L1  VALVE  a  VALVE  a  a VALVE  a VALVE 

WING AND ENGINE ANTI-ICE CONTROL PANEL, M10397
A
LEFT OR RIGHT WING THERMAL ANTI-ICE VALVE, V52 OR V57
SEE B
521UBX 621UBX
HP2
HP6 FWD
INBD
LEFT OR RIGHT WING THERMAL ANTI-ICE TAI VALVE, V52 OR V57
B
Wing Thermal Anti-Ice System - Component Location Figure 102
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757 MAINTENANCE MANUAL
 WING THERMAL ANTI-ICING - ADJUSTMENT/TEST
_________________________________________
 1.  General_______
 A.  This procedure contains four tasks. The first two tasks are a test of the left and right wing thermal anti-ice (TAI) system. The second two tasks are an alternate test of the left and right wing TAI system that allows the use of a hotter ground air supply.
 TASK 30-11-00-735-001
 2.  Test - Left Wing TAI System___________________________
 A.  Equipment
 (1)  
Timing Device - 15 seconds minimum

 (2)  
Ground Air Supply (80 lbs/min at 13 to 20 psig)

　
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