Eclipse EA500 Maintenance Manual page 151

AMM-34-50-11-041-801-D
1. General
A. This task gives the procedure to install the Global Positioning System/Wide Area
Augmentation System (GPS/WAAS) sensors.
B. There are two GPS/WAAS sensors installed in the aircraft. Installation steps are the
same for the light and right sides, unless specified.
2. Job Set-Up
SUBTASK AMM-34-50-11-041-D-921-001
A. Make sure the aircraft is in the same configuration it was when the removal task was
completed. Refer to
3. Procedure
SUBTASK AMM-34-50-11-041-D-411-001
(Refer to Fig. 401.)
A. Put the GPS/WAAS sensor
(1) Make sure the electrical connectors are facing forward.
(2) For the left side sensor, make sure the GPS/WAAS sensor
toward the outboard side of the aircraft and against the mounting bracket
(3) For the right side sensor, make sure the GPS/WAAS sensor
toward the inboard side on the aircraft and away from the mounting bracket
B. Attach the GPS/WAAS sensor
(1) For the left side GPS/WAAS sensor
bracket (5) with the four bolts
(2) For the right side GPS/WAAS sensor
bracket (5) with the four bolts
C. Torque the bolts
D. Bond the GPS/WAAS sensor
Electrical Bonding - Maintenance Practices.
(1) Make sure the resistance is not more than 2.5 millohms.
E. Remove the protective caps from the electrical connector
Concelman (TNC) connector
F. Connect the electrical connector
G. Apply power to the aircraft. Refer to
Maintenance Practices.
EFFECTIVITY: ALL POST MB 500-31-007 OR MB
500-31-008
EA500 Aircraft Maintenance Manual — 06-117751
GPS - INSTALLATION
AMM-34-50-11-001-801 – GPS - Removal.
(4) on the mounting bracket
(4) to the mounting bracket
(4)
(1) .
(4)
(1) and spacers
(1) to between 30-40 lbf.in (3.4-4.5 Nm).
(4) to the aircraft. Refer to
(3) .
(2) and Coax TNC connector
AMM-24-40-00-051-801 – External Power -
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
(5) and align the bolt holes.
(4) mounting flange is
(4) mounting flange is
(5) .
, attach the sensor (4) to the mounting
, attach the sensor (4) to the mounting
(6) .
AMM-20-03-00-051-801 –
(2) and Coax Threaded Neil-
(3) .
(5) .
(5) .
34-50-11
CONFIG D
Page 401-Inst
Sep 30/20