Eclipse EA500 Maintenance Manual page 235

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
System Test
Dual Standard Transponder
System Test
Dual Diversity Transponder
System Test
EFFECTIVITY: NOTED
EA500 Aircraft Maintenance Manual — 06-117751
TRANSPONDER - ADJUSTMENT/TEST
for testing procedures.
Table 501. Test Matrix
Std. Transponder 1 Adjustment/Test:
AMM-34-50-20-071-C-701-001-A
AMM-34-50-20-071-C-701-001-B, and
Std. Transponder 2 Adjustment/Test:
AMM-34-50-20-071-C-701-002-A
AMM-34-50-20-071-C-701-002-B.
Transponder Cooling Adjustment/Test:
AMM-34-50-24-071-801
Diversity Transponder 1 Adjustment/Test:
AMM-34-50-20-071-C-701-003-A
AMM-34-50-20-071-C-701-003-B, and
Diversity Transponder 2 Adjustment/Test:
AMM-34-50-20-071-C-701-004-A
AMM-34-50-20-071-C-701-004-B.
Transponder Cooling Adjustment/Test:
AMM-34-50-24-071-801
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
Procedures
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34-50-20
CONFIG C
Page 501
Sep 30/20