Gps 3 Mount - Installation - Eclipse EA500 Maintenance Manual

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
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)
C. Connect wiring harness plug
to 15-12 lbf.in (1.35-1.69 Nm).
D. Connect fan electrical molex connector
E. Connect the GPS antenna coax cable connector to the GPS coax receptacle
GPS.
F. Connect 50 ohm/5 watt termination load
G. Position mount on to 131 CZ-B - Floor Panel, Aft Short, Left Cabin
H. Secure mount to 131 CZ-B - Floor Panel, Aft Short, Left Cabin
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
B. Install 131 CZ-B - Floor Panel, Aft Short, Left Cabin
C. Remove all tools, equipment, and unwanted material from the work area.
EFFECTIVITY: ALL POST MB 500-34-030
EA500 Aircraft Maintenance Manual — 06-117751

GPS 3 MOUNT - INSTALLATION

AMM-34-50-13-001-801 – GPS 3 Mount - Removal
to stud and install nut (9)
(4) to the mount
(10) to harness molex connector
(5) to coax receptacle marked BTM.
AMM-34-50-11-041-C-801 – GPS 3 - Installation
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
.
(3) with two screws (7) . Torque screws
(2) and align holes.
(2) with four screws
(2) .
.
(7)
(11) .
(6) marked
(1) .
.
34-50-13
Page 401-Inst
Sep 30/20