Eclipse EA500 Maintenance Manual page 301

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
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
through the bracket
positioned up.
(2) From behind the mounting bracket
body (6) and sliding it forward against the mounting bracket
(3) From the front of the switch body
screws (8) in the base of the body. Tighten the two screws
Mounting Hardware pulls the mounting sleeve
Torque screws to 18-25 ounce.in.
(4) Replace the switch cap
push the cap
(5) Align keyways and push electrical connector
until it clicks.
B. Position bracket (1)
panel and align screw holes.
C. Attach bracket (1)
18-23 lbf.in.
EFFECTIVITY: ALL POST MB 500-34-030
EA500 Aircraft Maintenance Manual — 06-117751
ADS-B FAIL INDICATOR - INSTALLATION
(6) into the mounting bracket
(1) from the front. Ensure the switch body label "TOP" is
(1) , place the locking sleeve
(6) locate the two slot head integral mounting
(7) by inserting the cap pins into the slide retainer
(7) into the switch body (6)
with assembled ADS-B Fail Indicator on to the left lower instrument
with ADS-B Fail Indicator with two screws
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
AMM-34-50-26-001-801 – ADS-B
(1)
(4)
(1) .
(8) until the Integral
(4) against the mounting bracket
.
(3) on to the back of the switch body
(2) . Torque screws
by sliding it
onto the switch
(1) .
(6) and
(6)
(2) to
34-50-26
Page 401-Inst
Sep 30/20