GPS 3 MOUNT - INSTALLATION
AMM-34-50-13-041-801
1. General
A.
This task gives the procedures to install the Global Positioning System (GPS 3) mount.
B. There is one GPS 3 mount installed under the baggage floor panel.
2.
Job Set-Up
SUBTASK AMM-34-50-13-041-921-001
A.
Make sure the aircraft is in the same configuration as it was when the removal task was
completed. Refer to AMM-34-50-13-001-801 – GPS 3 Mount - Removal .
3.
Procedure
SUBTASK AMM-34-50-13-041-411-001
(Refer to Fig. 401.)
A.
Remove the protective caps from the electrical connectors.
B. Connect jumper (8) to stud and install nut (9) .
C. Connect wiring harness plug (4) to the mount (3) with two screws (7) . Torque screws (7)
to 15-12 lbf.in (1.35-1.69 Nm).
D. Connect fan electrical molex connector (10) to harness molex connector (11) .
E. Connect the GPS antenna coax cable connector to the GPS coax receptacle (6) marked
GPS.
F. Connect 50 ohm/5 watt termination load (5) to coax receptacle marked BTM.
G. Position mount on to 131 CZ-B - Floor Panel, Aft Short, Left Cabin (2) and align holes.
H. Secure mount to 131 CZ-B - Floor Panel, Aft Short, Left Cabin (2) with four screws (1) .
Torque screws to 15-12 lbf.in (1.35-1.69 Nm.
4.
Job Close-Up
SUBTASK AMM-34-50-13-041-921-002
A.
Install GPS 3 (GDL 88) unit. Refer to AMM-34-50-11-041-C-801 – GPS 3 - Installation .
B. Install 131 CZ-B - Floor Panel, Aft Short, Left Cabin (2) .
C. Remove all tools, equipment, and unwanted material from the work area.
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: ALL POST MB 500-34-030
34-50-13
Page 401-Inst
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
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