Eclipse EA500 - Page 301

ADS-B FAIL INDICATOR - INSTALLATION
AMM-34-50-26-041-801
1. General
A.
This task gives procedures to install the ADS-B Fail Indicator.
B. There is one ADS-B Fail Indicator installed on the lower left instrument panel.
2.
Job Set-Up
SUBTASK AMM-34-50-26-041-921-1
A.
Make sure the aircraft and Fail Indicator (disassembled) are in the same configuration as
it was when the removal task was completed. Refer to AMM-34-50-26-001-801 – ADS-B
Fail Indicator - Removal
3.
Procedure
SUBTASK AMM-34-50-26-041-411-1
(Refer to Fig. 401.)
A.
Install the ADS-B Fail Indicator as follows:
(1) Insert the back of the switch body (6) into the mounting bracket (1) by sliding it
through the bracket (1) from the front. Ensure the switch body label “TOP” is
positioned up.
(2) From behind the mounting bracket (1) , place the locking sleeve (4) onto the switch
body (6) and sliding it forward against the mounting bracket (1) .
(3) From the front of the switch body (6) locate the two slot head integral mounting
screws (8) in the base of the body. Tighten the two screws (8) until the Integral
Mounting Hardware pulls the mounting sleeve (4) against the mounting bracket (1) .
Torque screws to 18-25 ounce.in.
(4) Replace the switch cap (7) by inserting the cap pins into the slide retainer (6) and
push the cap (7) into the switch body (6) .
(5) Align keyways and push electrical connector (3) on to the back of the switch body (6)
until it clicks.
B. Position bracket (1) with assembled ADS-B Fail Indicator on to the left lower instrument
panel and align screw holes.
C. Attach bracket (1) with ADS-B Fail Indicator with two screws (2) . Torque screws (2) to
18-23 lbf.in.
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: ALL POST MB 500-34-030
34-50-26
Page 401-Inst
Sep 30/20
© 2020 Eclipse Aerospace, Inc.