Gps 3 - Installation - Eclipse EA500 Maintenance Manual

AMM-34-50-11-041-C-801
1. General
A. This task gives procedures to install the Global Positioning System (GPS 3) unit.
B. There is one GPS 3 installed on the aircraft under 131 CZ-B - Floor Panel, Aft Short, Left
Cabin.
2. Job Set-Up
SUBTASK AMM-34-50-11-041-C-921-001
A. Make sure aircraft is in same configuration as it was when removal task was completed.
Refer to AMM-34-50-11-001-C-801 – GPS 3- Removal
B. Complete GPS 3 configuration (if not previously accomplished), refer to
AMM-34-50-10-051-B-801 – GPS 3- Maintenance Practices
C. Make sure that mount backplate has the 50 ohm/5 watt termination load is installed on
coax receptacle BTM.
3. Procedure
SUBTASK AMM-34-50-11-041-C-411-001
(Refer to Fig. 401.)
A. Slide the GPS 3 unit
B. Lift the lock down arm
C. Secure 131 CZ-B - Floor Panel, Aft Short, Left Cabin with four screws. Refer to
AMM-25-11-30-041-801 – Cockpit Floor Panels - Installation
4. Job Close-Up
SUBTASK AMM-34-50-11-041-C-921-002
A. Remove all tools, equipment, and unwanted material from work area.
B. Do a system test of the ADS-B. Refer to
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 500-34-030
EA500 Aircraft Maintenance Manual — 06-117751

GPS 3 - INSTALLATION

(1) straight into the rack until it stops.
(2) over the right angled hook on the unit and hand tightened.
SUBTASK
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
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AMM-34-50-20-071-C-701-005.
Page 401-Inst
34-50-11
CONFIG C
Sep 30/20