Eclipse EA500 Maintenance Manual page 289

AMM-34-50-21-041-801
1. General
A. This task gives the procedures to install the transponder.
B. There are two transponders, one is behind the left PFD and the other is behind the right
PFD. The installation procedure is given for the left transponder and is the same for the
right transponder.
C. If the aircraft has ADS-B OUT function, ensure this transponder has Extended Capability
(ES) enabled and software version is at 8.02 or above.
NOTE: Make sure that the transponder software is in same configuration as it was when
the removal task was completed. If necessary, update transponder software to
the required level.
2. Job Set-Up
SUBTASK AMM-34-50-21-041-921-001
A. Make sure that the aircraft is in same configuration as it was when the removal task was
completed. Refer to
B. As required, make sure that transponder is configured for ADS-B. Refer to
AMM-34-50-20-051-801 – Transponder with ADS-B Out – Maintenance Practices
3. Procedure
SUBTASK AMM-34-50-21-041-411-001
(Refer to Fig. 401 .
A. Loosen the captive screw
transponder.
B. Slide the transponder
and tighten the screw
C. Electrically bond the transponder
Electrical Bonding - Maintenance Practices.
EFFECTIVITY: ALL
EA500 Aircraft Maintenance Manual — 06-117751
TRANSPONDER - INSTALLATION
AMM-34-50-21-001-801 – Transponder - Removal.
(2) and rotate the lever
(1) into the mount (4) . Rotate the lever
(2) .
(1) to the structure. Refer to
Resistance must be 2.5 milliohms or less.
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
(3) to the open position on the
(3) to the closed position
AMM-20-03-00-051-801 –
.
34-50-21
Page 401-Inst
Sep 30/20