Eclipse EA500 Maintenance Manual page 146

access hole at the bottom of the unit face. Rotate the hex tool clockwise while
pressing on the left side of the bezel until the unit is firmly seated in the rack.
(2) Be sure not to overtighten the unit into the GPS bracket assembly
application of hex drive tool torque exceeding -15 lbf.in can damage the locking
mechanism.
5. Job Close-Up
SUBTASK AMM-34-50-11-041-B-921-002
A. Remove all tools, equipment, and unwanted material from work area.
B. Close circuit breakers that follow:
• ECB - GPS 1 (R FWD Bus)
• ECB - GPS 2 (L FWD Bus)
C. Complete GPS 400W configuration (if not previously accomplished), refer to
AMM-34-50-10-051-801 – GPS - Maintenance Practices.
D. Do an adjustment/test of the GPS. Refer to
Adjustment/Test
If ADS-B function is installed, perform ADS-B Out Functional Test. Refer to
AMM-34-50-20-071-C-701-006
E. If all other maintenance is complete, return aircraft to service. Refer to
AMM-20-00-02-051-801 – Return To Service (After Maintenance).
EFFECTIVITY: 0001-0262 POST SB 500-99-005; AND
0266-0267; ALL POST MB 500-31-018
EA500 Aircraft Maintenance Manual — 06-117751
AMM-34-50-10-071-C-801 – GPS -
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
(6) . The
SUBTASK
34-50-11
CONFIG B
Page 402-Inst
Sep 30/20