Eclipse EA500 - GPS 2 Antenna Splitter - Installation; General; Job Set-Up; Procedure

GPS 2 ANTENNA SPLITTER - INSTALLATION
AMM-34-50-14-041-801
1. General
A.
This task gives procedures to install the GPS 2 Antenna Splitter.
B. There is one GPS 2 Antenna Splitter installed on the aircraft under 231 NZ - Floor Panel,
Baggage Compartment.
2.
Job Set-Up
SUBTASK AMM-34-50-14-041-921-001
A.
Make sure the aircraft is in the same configuration as it was when the removal task was
completed. Refer to AMM-34-50-14-001-801 – GPS 2 Antenna Splitter - Removal
3.
Procedure
SUBTASK AMM-34-50-14-041-411-001
(Refer to Fig. 401.)
A.
Remove the protective caps from the three coaxial connectors (3) .
B. Put the GPS 2 Antenna Splitter (1) on the structure and align the screw holes.
C. Attach the GPS 2 Antenna Splitter (1) to the aircraft with two screws (2) . Torque the
screws (2) to 30-40 lbf.in (3.4-4.5 Nm).
D. Connect the three coaxial connectors (3) on the splitter (1) .
E. Electrically bond the GPS 2 Antenna Splitter to the structure. Refer to
AMM-20-03-00-051-801 – Electrical Bonding - Maintenance Practices. Resistance must
be 2.5 milliohms or less.
4.
Job Close-Up
SUBTASK AMM-34-50-14-041-921-002
A.
Install 231 NZ - Floor Panel, Baggage Compartment. Refer to AMM-06-50-00-051-801 –
Aircraft Access Panels for location and installation instructions.
B. Remove all tools, equipment, and unwanted material from the work area.
C. Do GPS 2 Adjustment/Test. Refer to SUBTASK AMM-34-50-10-071-C-801-003.
D. Do a system test of the ADS-B. Refer to SUBTASK AMM-34-50-20-071-C-701-005.
E. If all other maintenance is complete, return the 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 500-34-030
34-50-14
Page 401-Inst
Sep 30/20
© 2020 Eclipse Aerospace, Inc.