S 435-039
(12)
Connect the electrical connector on the low pressure switch.
S 215-040
(13)
Make sure the right engine anti-ice VALVE light on the P5 panel comes on.
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MAINTENANCE MANUAL
S 215-041
(14)
Make sure the EICAS level C alert message R ENG ANTI-ICE is shown on the EICAS display.
S 485-085
(15)
Put a jumper between pins 1 and 2 of the high pressure electrical connector. Make sure the EICAS message R ENG TAI VALVE is shown on the EICAS display.
S 085-086
(16)
Remove the jumper from between pins 1 and 2 of the high pressure switch electrical connector.
S 435-097
(17)
Connect the electrical connector to the high pressure switch.
S 435-045
(18)
Connect the electrical connector to the TAI valve.
S 865-090
(19)
Put the R ENGINE ANTI-ICE switch-light on the P5 panel in the OFF position.
H. Put the Airplane Back to Its Usual Condition
S 415-091
(1)
Close the left fan cowl on the left or right engine (Ref 71-11-04).
S 865-088
(2)
Put the engine shutdown inhibit back on the EICAS computers (Ref 31-41-00).
S 445-092
(3)
Do the Thrust Reverser Activation procedure (Ref 78-31-00).
S 865-087
(4)
Remove electrical power, if it is not necessary (Ref 24-22-00).
TASK 30-21-00-735-053
3. Operational Test - Engine Inlet TAI High Pressure Switch Circuitry
__________________________________________________________________
NOTE: This procedure is a scheduled maintenance task.
____
A. References
(1)
24-22-00/201, Electrical Power - Control
(2)
31-41-00/201, Engine Indication and Crew Alerting System (EICAS)
(3)
71-11-04/201, Fan Cowl Panels
(4)
78-31-00/201, Thrust Reverser System
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