Eclipse EA500 User Manual

TRANSPONDER - ADJUSTMENT/TEST
AMM-34-50-20-071-C-801
1. General
A.
This task gives procedures to do the adjustment/test of the:
• Dual Standard (Non-Diversity) Transponder System and components or Dual
Diversity Transponder System and components.
NOTE: An adjustment/test is only required for the transponder that is being installed. The
opposite transponder, if it has not been removed, does not require an
adjustment/test
B. Perform ADS-B Out System Test only if ADS-B function is enabled.
NOTE: Perform ADS-B Out Fail Indicator Functional Test only if the indicator is being
replaced or removed and reinstalled.
Limitation: If the aircraft is equipped with Garmin GPS 400W, ADS-B OUT System Test
test applies to Transponder 1 (XPDR 1) only.
(1)
Refer to Table 501 for testing procedures.
Table 501. Test Matrix
System Test Procedures
Dual Standard Transponder
System Test
Std. Transponder 1 Adjustment/Test: SUBTASK
AMM-34-50-20-071-C-701-001-A
or SUBTASK
AMM-34-50-20-071-C-701-001-B, and
Std. Transponder 2 Adjustment/Test: SUBTASK
AMM-34-50-20-071-C-701-002-A or SUBTASK
AMM-34-50-20-071-C-701-002-B.
Transponder Cooling Adjustment/Test: TASK
AMM-34-50-24-071-801 .
Dual Diversity Transponder
System Test
Diversity Transponder 1 Adjustment/Test: SUBTASK
AMM-34-50-20-071-C-701-003-A or SUBTASK
AMM-34-50-20-071-C-701-003-B, and
Diversity Transponder 2 Adjustment/Test: SUBTASK
AMM-34-50-20-071-C-701-004-A or SUBTASK
AMM-34-50-20-071-C-701-004-B.
Transponder Cooling Adjustment/Test: TASK
AMM-34-50-24-071-801 .
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-50-20
CONFIG C
Page 501
Sep 30/20
© 2020 Eclipse Aerospace, Inc.

Eclipse EA500 Specifications

General

Brand	Eclipse
Model	EA500
Category	Aircrafts
Language	English