5.
ADS-B System Test
SUBTASK AMM-34-50-21-071-701-002
A. In order to verify ADS-B OUT function is active, perform the following test using IFR 6000
or an equivalent test set.
NOTE: If IFR 6000 (or an equivalent transponder test set) does not include the ADS-B
test capability, at a minimum, verification that the DF17 extended squitter format
is being detected is sufficient. During Generic Mode S tests, DF17 format
availability is being checked in the following subtasks:
•
SUBTASK AMM-34-50-20-071-C-701-001-A
or SUBTASK AMM-34-50-20-071-C-701-001-B
•
SUBTASK AMM-34-50-20-071-C-701-002-A
or SUBTASK AMM-34-50-20-071-C-701-002-B
•
SUBTASK AMM-34-50-20-071-C-701-003-A
or SUBTASK AMM-34-50-20-071-C-701-003-B
•
SUBTASK AMM-34-50-20-071-C-701-004-A
or SUBTASK AMM-34-50-20-071-C-701-004-B
NOTE: If no transponder test set with the ADS-B test capability is available, as an
additional or alternate method of verifying proper operation and performance of
the installed ADS-B OUT function, the FAA Public ADS-B Performance Report
(PAPR) may be requested after a Return to Service (RTS) flight. This report
request may be made online on the FAA web site at the ADS-B related area.
NOTE: To check if IFR 6000 has the ADS-B test, press SETUP to display SETUP-
GENERAL page. Press INFO and verify that ADSB is listed in the OPTIONS
area.
If using IFR 6000 with the ADSB test option, to make sure that the ADS-B OUT function
is active, perform the following procedure:
(1) ADS-B Test Setup
(a) After the Transponder Test Set (IFR 6000) performs Self Test, push SETUP
button on the test set to bring up the SETUP-XPDR page. If necessary, continue
pressing SETUP button until SETUP XPDR screen is displayed.
(b) Press ADS-B SETUP Soft Key to display the SETUP-ADSB Setup Screen. Use
NEXT PARAM and PREV PARAM Soft Keys to select each parameter.
Configure the setup parameters as shown in the following example:
POS DECODE: GLOBAL
LAT: 35 02 13.80 N
LON: 106 37 1.80 W
BARO PRES ALT: 5450 ft.
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: ALL POST MB 500-31-016
34-50-21
Page 504
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
