S 865-045
(14) Do this task to simulate engine running for the left engine speed card, M10298 : Simulate the Engine Operation (AMM 77-12-03/201).
(a) Do not open the pitot heat system circuit breakers as stated in the referenced procedure.
S 215-024
(15) Make sure the CAPT PITOT, L AUX PITOT, F/O PITOT, and R AUX PITOT annunciator lights are off.
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S 215-025
(16)
Make sure the EICAS messages, CAPT PITOT HEAT; L AUX PITOT HEAT; F/O PITOT HEAT; and R AUX PITOT HEAT, do not show on the EICAS display.
S 865-047
(17)
Do the steps in this task to stop the engine running simulation: Simulate the Engine Operation (AMM 77-12-03/201).
S 865-027
(18)
Do the previous steps for engine running simulation again, for the right engine speed card, M10311.
(a) Make sure the annunciators and EICAS messages are not on, as described in the previous steps.
E. Put the Airplane Back to Its Usual Condition
S 445-037
(1)
Put the safety-sensitive systems back to their initial conditions (Ref 32-09-02/201).
S 445-039
(2)
Do the activation procedure for the spoilers if you did the
deactivation procedure (Ref 27-61-00/201).
(3)
Remove electrical power if it is not necessary (Ref 24-22-00/201).
S 865-028
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ANGLE OF ATTACK PROBE HEAT - DESCRIPTION AND OPERATION
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General
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A. Two angle of attack (AOA) probes (one on each side) are electrically heated to prevent erroneous readings due to ice conditions. AOA probe heat system components include: AOA probes, the auxiliary annunciator panel, and the miscellaneous test panel.
B. System electrical power comes from the 28v dc buses, and the 115v ac buses. Circuit breakers are on overhead circuit breaker panel P11, and main power distribution panel P6.
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本文鏈接地址：757 AMM 飛機維護手冊 防冰和排雨 CHAPTER 30 - ICE AND RAIN PROTECTION(93)
