Eclipse EA500 Maintenance Manual 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
B. Do MFD Set-Up. Refer to
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
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).
EFFECTIVITY: ALL POST MB 500-31-007 OR MB
500-31-008
EA500 Aircraft Maintenance Manual — 06-117751
SUBTASK AMM-34-50-10-071-C-921-001.
SUBTASK AMM-34-50-10-071-C-701-001.
AMM-24-40-00-051-801 – External Power -
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
34-50-10
CONFIG C
Page 502
Sep 30/20