EMIT CAT = LIGHT
(k) Select BDS 6,1 A/C STATUS ST1 and check the following data:
AA = matches aircraft ICAO code displayed on the MFD Settings Page
MODE A (4096) CODE = Entered Squawk Code from the PFD
EMERG/PRIOR CODE = 0 - NO EMERGENCY
(l) Select BDS 6,5 A/C STATUS SUR and check the following data:
AA = matches aircraft ICAO code displayed on the MFD Settings Page
VERSION = 2 - DO-260B
1090 = 0
ANT OFF = RT 0 m, 6 m (for the Garmin GPS 400W equipped aircraft, ANT OFF
= RT 0 m, 4 m)
SIL
≥
3
LN/WD = 1 - <15m; <23m.
(m) On IFR 6000, press STOP TEST.
14. ADS-B FAIL Indicator Functional Test
SUBTASK AMM-34-50-20-071-C-701-008
* * * ALL POST MB 500-34-030
NOTE: This procedure is required only upon ADS-B FAIL Indicator replacement or
removal and installation.
A. ADS-B FAIL Indicator Functional Test
NOTE: After initial system installation, the initial acquisition of GPS position can take up
to 20 minutes. Subsequent acquisitions should take no more than 150 seconds.
This test must be done prior to GPS position acquisition and extinguishing of the
ADS-B FAIL indicator.
(1) Power up the aircraft.
(2) Make sure that the ADS-B FAIL indicator is illuminated in white color. Refer to
.
(3) Check that the brightness of the indicator can be adjusted with the Master Dim switch
on the Center Switch Panel (CSP).
(4) Make sure the ADS-B FAIL indicator extinguishes within 150 seconds or less after
power up.
15. Job Close-Up
SUBTASK AMM-34-50-20-071-C-921-002
* * * 0001-0104, 0113-0115, 0120, 0123-0124 POST SB 500-99-002; 0105-0112, 0116-0119,
0121-0122, 0125-0265 POST SB 500-99-005; AND 0266-0267; ALL POST MB 500-31-016,
MB 500-31-018. and MB 500-34-030
A. Set WOW Box switches to W-on-W (on-ground)
B. Reset the collared ECB’s. Refer to AMM-20-00-03-051-801 – Prepare Anti-Ice Systems
For Maintenance.
EA500 Aircraft Maintenance Manual — 06-117751
Temporary Revision No. 34-21
EFFECTIVITY: NOTED
34-50-20
CONFIG C
Page 539
Sep 30/20
© 2020 Eclipse Aerospace, Inc.
