757 AMM 飞机维护手册 自动飞行 AUTOFLIGHT 2(171)

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 17) AIRPLANES WITHOUT CONTROL WHEEL STEERING; 16 XDCR WHL a) This test does not apply to this aircraft
 configuration. If test selected, MCDP displays 16 NO TEST THIS A/C CONFIG.
 18) AIRPLANES WITH CONTROL WHEEL STEERING; 16 XDCR WHL a) Displays any FCC self-test faults and FCC interface
 faults related to control wheel transducer. b) Provides action message to verify hydraulic power on (VFY HYD ON).
 c)  Instructs operator to move the control wheel to the full clockwise position. The transducer output force is monitored for a plus 15 pounds.
 d)  Instructs operator to move the control wheel to the full counterclockwise position. The transducer output force is monitored for a minus 15 pounds.
 e)  Instructs operator to release the control wheel. The transducer output is monitored for a force of between plus and minus 2 pounds.
 19) GUN 011-999; 17 PVDC a) This test does not apply to this airplane
 configuration. If test selected, MCDP displays 17 NO TEST THIS A/C CONFIG.
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MAINTENANCE MANUAL

 (b) System Tests Description 1) 30 CURRENT FAULT REPORT a) Displays all LRU and interface faults detected and stored in the FCCs and TMC while the MCDP operates in the ground test mode. Ground fault messages and diagnostic codes are the same as flight fault messages except the flight deck effect and intermittent bit status are not displayed. b) Provides interaction message to allow operator to skip Interface Fault messages. c) Provides interaction message to allow operator to select current Ground Fault display. 2) 40 AUTOLAND a) Displays the current ground faults and interface faults related to the autoland system. The autoland related interfaces are automatically monitored. It automatically performs LRU and support tests related to the autoland system that do not require interaction with the operator. b) Automatically performs LRU and support tests related to the autoland system that require no manual preconditioning except for applying electrical power. c) Automatically performs LRU and support tests related to the autoland system that require manual preconditions but no hydraulic power.
 d)  Performs manual interface checks related to the autoland system. e) Performs manual LRU and support tests related to the autoland system. f) Performs A/P servo and stab trim tests.
 (c) Support Test Description 1) 51 AIR/GRD RLY a) Displays any FCC and TMC self-test faults and any interface faults related to air/ground relay. b) Interaction test of the landing gear system 1 air/ground relay and its interface to the FCCs and TMC.
 c)  Interaction test of the landing gear system 2 air/ground relay and its interface to the FCCs.
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52 TMC RLY/SW
 a)  Displays any TMC self-test faults and TMC interface faults related to Environmental Control System (ECS) cards, pneumatic system, anti-ice, and thrust reverser lever position.
 b)  Tests for discrete output signals from the Electrical Systems Card File #1 (P-50 Panel) left and right Electronic Engine Controls (EEC) discrete cards, from the autothrottle microswitch pack assembly, pneumatic shutoff and isolation valves, and anti-ice valves.
56 FCC CONFIG/OPT
 a)  Displays any FCC self-test faults and FCC interface faults related to parity.
 b)  Checks the status of the FCC program pin wiring for airplane and hardware configurations and customer selected options.
57 TMC CONFIG/OPT
 a)  Displays any TMC self-test faults and TMC interface faults related to parity.
 b)  Checks status of TMC program strapping for engine and airplane configuration, autothrottle, and thrust limit customer selected options.
59 FCC INSTR
 a)  Displays any FCC self-test faults.
 b)  Sends test routine command and parameters to FCCs, and displays operator interaction message.
　
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