5. Single Right ACS Test
SUBTASK AMM-31-40-00-071-701-002
A. Single Right ACS Test
(1) Remove power to the left hand ACS.
(2) On the INSTRUMENT PANEL, LEFT, Pull the following breaker:
• L Aircraft Computer System (L-ACS)
(3) On the MFD ECB synoptic page, use the inner DCK to select the AVIONICS system,
and the outer DCK to highlight the following ECB:
• ECB - L AIRCRAFT COMPUTER (R FWD Bus)
(4) On the MFD ECB synoptic page, select the PULL LSK.
(5) On the MFD ECB synoptic page, make sure the following ECBs show as PULLED:
• ECB - L AIRCRAFT COMPUTER (R FWD Bus)
(6) On the throttle quadrant, move the rudder trim knob to NOSE LEFT and/or NOSE
RIGHT hold.
(7) Make sure that trim tab moves and display shows movement.
(8) Return trim tab to neutral.
(9) Push the Pilots control grip trim switch to NOSE DOWN
(10) Make sure that right elevator trim tab moves and display shows movement.
(11) Return trim tab to neutral.
(12) Push the Pilots control grip trim switch to LWD and hold.
(13) Aileron DOES NOT move and the display shows no movement.
(14) Make sure that all three green lights for landing gear indicator are illuminated.
(15) Make sure flap handle is in the UP position if not already accomplished.
(16) Make sure that flap position displayed on MFD is UP.
(17) Set flap handle to T/O position.
(18) Make sure that flap position displayed on MFD is TO and make sure flaps move.
(19) Set flap handle in UP position.
(20) Make sure that flaps return to up position.
(21) Select electrical synoptic page on MFD.
(22) Make sure that voltages and contactor settings that follow are correct:
(a) System battery is 28 ±0.5 VDC
(b) System battery monitor is green outlined
(c) System battery contactor is engaged (green)
(d) Start battery is 28 ±0.5 VDC
Eclipse 550 Aircraft Maintenance Manual — 06-123838
Temporary Revision No. 31-3
EFFECTIVITY: ALL
31-40-00
Page 508
Aug 19/19
© 2019 Eclipse Aerospace, Inc.
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