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GPS - REMOVAL

AMM-34-50-11-001-D-801

1. General

This task gives the procedure to remove the Global Positioning System/Wide Area

Augmentation System (GPS/WAAS) sensors.

B. There are two GPS/WAAS sensors installed in the aircraft. Removal steps are the same

for the light and right sides, unless specified.

Job Set-Up

SUBTASK AMM-34-50-11-001-D-921-001

Make the aircraft safe for maintenace. Refer to AMM-20-00-01-051-801 – Make Safe For

Maintenance..

B. Remove power from the aircraft. Refer to AMM-24-40-00-051-801 – External Power -

Maintenance Practices..

C. Remove the 231 JZ – Cabin Headliner Assembly. Refer to AMM-06-50-00-051-801 –

Aircraft Access Panels.

Procedure

SUBTASK AMM-34-50-11-001-D-011-001

(Refer to Fig. 401.)

Remove the four bolts (1) that attach the GPS/WAAS sensor (4) to the mounting bracket

(5) .

(1) For the right side sensor, remove the four spacers (6) .

B. Disconnect the electrical connector (2) and Coax Threaded Neill-Concelman (TNC)

connector (3) from the GPS/WAAS sensor (4) .

C. Remove the GPS/WAAS sensor (4) from the mounting bracket (5) .

D. Install protective caps on the electrical connector (2) and Coax TNC connector (3) .

EA500 Aircraft Maintenance Manual — 06-117751

Temporary Revision No. 34-21

EFFECTIVITY: ALL POST MB 500-31-007 OR MB

500-31-008

34-50-11

CONFIG D

Page 401-Rem

Sep 30/20

Eclipse EA500 User Manual

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