* SEE THE WDM EQUIPMENT LISTTHIS CIRCUIT BREAKER CAN BE IN ONE OF THESE LOCATIONS
Wing Thermal Anti-Ice System - Component Index
Figure 101
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
30-11-00
ALL ú
ú 01 Page 101
ú May 28/99
A
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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
30-11-00
ALL ú ú 01 Page 102 ú May 28/99
A
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)
