Eclipse EA500 - Page 140

G. On the MFD ECB page, reset ECB - INTEGRATED SENSOR 1 (BATT Bus).
5. GPS 2 Test
SUBTASK AMM-34-50-10-071-C-801-003
A.
Do Job Set-Up. Refer to SUBTASK AMM-34-50-10-071-C-921-001.
B. Do MFD Set-Up. Refer to SUBTASK AMM-34-50-10-071-C-701-001.
C. On the MFD ECB page, ensure that the ECB - GPS 2 (L FWD Bus) and the ECB -
INTEGRATED SENSOR 2 (L AFT Bus) are AUTO-ON.
D. On the MFD ECB page, pull ECB - GPS 2 (L FWD Bus). After 5 seconds, make sure that
GPS 2 is displaying satellite-status information
E. On the MFD ECB page, reset ECB - GPS 2 (L FWD Bus).
F. On the MFD ECB page, pull ECB - INTEGRATED SENSOR 2 (L AFT Bus). After 5
seconds, make sure that GPS 2 is displaying satellite-status information.
G. On the MFD ECB page, reset ECB - INTEGRATED SENSOR 2 (L AFT Bus).
6.
Job Close-Up
SUBTASK AMM-34-50-10-071-C-921-002
A.
Remove all tools, equipment, and unwanted material from work area.
B. Disconnect external power. Refer to AMM-24-40-00-051-801 – External Power -
Maintenance Practices.
C. If all other maintenance is complete, return aircraft to service. Refer to
AMM-20-00-02-051-801 – Return To Service (After Maintenance).
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: ALL POST MB 500-31-007 OR MB
500-31-008
34-50-10
CONFIG C
Page 502
Sep 30/20
© 2020 Eclipse Aerospace, Inc.