Eclipse EA500 Maintenance Manual page 103

(not selectable), select OFF and return to this field to select EFIS / Airdata after
other fields on the page have been configured.
NOTE: Note 1 in
Indication and Electrical Provisions Package option), enter: "Off"; for aircraft
NOT configured for (Standby Indication and Electrical Provisions Package
option) or right GPS 400W, enter: "EFIS / Airdata". Example shows left GPS
400W on aircraft not configured for European operations.
(5) In this same manner, set IN 2 / SPEED to Low, IN 2 / DATA to Off, OUT / SPEED to
High, and OUT / DATA to GAMA 429 Grph w/ Int.
(6) Set SDI to Common and VNAV to Enable Labels.
(7) The MAIN ARINC 429 CONFIG screen settings should now match the settings in
Fig. 202.
(8) Press the small right knob to dismiss the cursor. The small right knob may now be
rotated to select other configuration screens.
D. Configure RS-232 Interfaces.
(1) Determine whether the aircraft has the Stormscope option installed. This will be
indicated by the LIGHTNING STRIKE DETECTION option being displayed on the
MFD or PFD INSTALLED EQUIPMENT list. The INSTALLED EQUIPMENT list may
be accessed on the MFD or PFD via the SETUP tab, selecting SETTINGS, then
selecting INSTALLED EQUIPMENT.
(2) On the GPS 400W, rotate small right knob to select MAIN RS232 CONFIG page.
(3) Press the small right knob to turn on the cursor.
(4) Using the large right knob to select fields as necessary, the small right knob to make
selections, and ENT to confirm selections, set up the RS-232 configuration as shown
in Fig. 203.
(a) Use the following settings for CHNL 2 INPUT:
1 "Off" for left GPS 400W on aircraft NOT configured for the (Standby
Indication and Electrical Provisions Package option).
2 "Shadin-adc" ("In" only; "out" is "off") for left GPS 400W on aircraft configured
for the (Standby Indication and Electrical Provisions Package option). Refer
to Fig. 221
3 "Off" for right GPS 400W regardless of configuration.
(b) If ADS-B OUT is installed, use the following settings for CHNL 2 OUTPUT:
CHNL 2/OUTPUT = ADS-B OUT+
NOTE: For this configuration selection to be available, GPS software must be at
least at the following level:
SW P/N 006-B1144-23 Main SW v5.03
SW P/N 006-B0803-20 GPS WAAS SW v5.0.
NOTE: If applicable, make sure that the GPS software is in same configuration
as it was when the removal task was completed. If necessary, update
GPS software to the required level.
EFFECTIVITY: 0001-0262, POST SB 500-99-005; AND
0266-0267; ALL POST MB 500-31-018
EA500 Aircraft Maintenance Manual — 06-117751
Fig. 202. For left GPS 400W, on aircraft configured for (Standby
for example of modification.
© 2020 Eclipse Aerospace, Inc.
Temporary Revision No. 34-21
34-50-10
CONFIG A
Page 205
Sep 30/20