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Eclipse 550 - Aircraft Computer Systems Adjustment and Test Procedures; General Aircraft Computer System Information; Left APC Component Test Matrix

Eclipse 550
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AIRCRAFT COMPUTER SYSTEMS - ADJUSTMENT/TEST
AMM-31-40-00-071-801
1. General
A. This task lists the procedures to do an adjustment/test of the Aircraft Computer System.
The Avio Processing Center (APC) consists of two sub-components:
Aircraft Computer System (ACS)
Full Authority Digital Engine Controller (FADEC)
These sub-components cannot be replaced individually during line maintenance. The
APC must be replaced if one of the sub-components is defective.
Table 501. Component Test Matrix (Use for Left APC)
Left APC Tests
MFD Electrical Synoptic Page Test AMM-31-10-00-071-801 – Displays and Control
Panels - Adjustment/Test.
MFD ECB Synoptic Page Test AMM-31-10-00-071-801 – Displays and Control Panels -
Adjustment/Test.
MFD FUEL Synoptic Page Test AMM-31-10-00-071-801 – Displays and Control Panels -
Adjustment/Test.
MFD ENG Synoptic Page Test AMM-31-10-00-071-801 – Displays and Control Panels -
Adjustment/Test.
MFD ICE Synoptic Page Test AMM-31-10-00-071-801 – Displays and Control Panels -
Adjustment/Test.
MFD Flap System Test AMM-31-10-00-071-801 – Displays and Control Panels -
Adjustment/Test.
MFD FLCS (Flight Control) Synoptic Page - Trim System Test AMM-31-10-00-071-801 –
Displays and Control Panels - Adjustment/Test.
ACS Maintenance Practices AMM-31-40-00-051-801 – Aircraft Computer Systems -
Maintenance Practices.
CAS Monitoring System Test AMM-31-10-00-071-801 – Displays and Control Panels -
Adjustment/Test.
Single Left ACS Test SUBTASK AMM-31-40-00-071-701-001
GPS Operation Test SUBTASK AMM-31-40-00-071-701-012
Vapor Cycle System (VCS) Doors Adjustment Test AMM-21-10-10-071-801 – Vapor
Cycle System (VCS) Doors - Adjustment/Test
Left VORE Calibration AMM-21-40-00-071-801 – Heating System - Adjustment/Test
Left FACV Calibration AMM-21-40-00-071-801 – Heating System - Adjustment/Test
Eclipse 550 Aircraft Maintenance Manual — 06-123838
Temporary Revision No. 31-3
EFFECTIVITY: ALL
31-40-00
Page 501
Aug 19/19
© 2019 Eclipse Aerospace, Inc.

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