Eclipse EA500 - Page 297

ADS-B FAIL INDICATOR - REMOVAL
AMM-34-50-26-001-801
1. General
A.
This task gives procedures to remove the ADS-B Fail Indicator.
B. There is one ADS-B Fail Indicator installed on the lower left instrument panel.
2.
Equipment and Materials
Table 401. Special Tools and Equipment
Name & Part Number
Extraction Tool (Aerospace Optics 18–234)
Cap Extractor Tool (Aerospace Optics 17–150)
3. Job Set-Up
SUBTASK AMM-34-50-26-001-921-001
A.
Make aircraft safe for maintenance. Refer to AMM-20-00-01-051-801 – Make Safe For
Maintenance.
B. Make sure all power is removed from the aircraft.
4.
Procedure
SUBTASK AMM-34-50-26-001-011-001
(Refer to Fig. 401.)
A.
Remove the ADS-B Fail Indicator as follows:
(1) Remove two screws (2) that secure bracket (1) to the Instrument panel.
(2) Disconnect electrical connector (3) from switch body (6) with extraction tool 18–234.
(3) Identify the two extraction slots positioned on either side of the cap (7) . Extract the
switch cap (7) by using the Cap Extractor Tool (Part Number: 17-150) or by applying
finger pressure on two sides of the switch cap pulling the switch cap from the switch
body.
(4) Remove switch cap (7) from the switch body (6) by gently removing the cap pins from
the hinged slide retainer.
(5) From the front of the switch body (6) locate the two slot head integral mounting
screws (8) in the base of the body. Loosen the two screws until the Integral Mounting
Hardware releases the mounting sleeve from the mounting panel.
(6) From behind the bracket (1) , remove the locking sleeve (4) and spacer (5) from the
switch body by sliding aft from the bracket (1) .
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: ALL POST MB 500-34-030
34-50-26
Page 401-Rem
Sep 30/20
© 2020 Eclipse Aerospace, Inc.