EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 130-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
Figure 9-27: Non-Aspen Equipment Configuration Notes
GNS-430/530(W) & GPS-400/500(W)
MAIN ARINC 429 CONFIG Page
IN 1
LOW
Honeywell EFIS (when using pins 48/49)
or EFIS or EFIS/ADC*
IN 2
As required
OUT
LOW
(2)
GAMA 429 Graphics w/INT
SDI
See Note 1
VNAV
ENABLE LABELS (W models only)
VOR/LOC/GS ARINC 429 CONFIG Page
SPEED
LOW
(2)
RX
LOW
(2)
TX
SDI
COMMON
* Note
– Some GPS units require the EFIS config. ACU2
installs can use the EFIS/ADC config.
Garmin SL-30
The SL-30 can be connected to the EFD1000 in one of two
ways. The Resolver configuration is preferred.
Resolver: The composite output from the SL-30 to the PFD
will become invalid whenever VOR monitor mode or
localizer back course is selected on the SL-30. The
navigation source will show as failed on the PFD if either of
these two modes is entered and the SL-30 is the selected
navigation source. If connected, the backup NAV indicator
will continue to function if either of these two modes is
selected.
Converter: VOR monitor mode or localizer back course
mode are disabled from selection on the SL-30. A backup
NAV indicator (GI-106) cannot be connected without a KN-
72 between the SL-30 and indicator due to the fact that the
OBS resolver inputs become invalid with this configuration.
CNX-80/ GNS-480
(software 2.0 and below)
This configuration is not authorized. The GNS-480 should be
upgraded to software version 2.3 (see below)
GPS 155XL
429 IN
= SELECTED COURSE
429 OUT
= KING EFS 40/50
KLN-94
MAINTENANCE PAGE 7: *STANDARD RS-232 or
*ENHANCED RS-232
*See Table 5-3 for details
CNX-80/ GNS-480 (software 2.3)
GND MAINT - ARINC 429 SETUP
CH_IN SEL
SPEED SDI
2 EFIS
LOW See Note 1
CH_OUT SEL
SPEED SDI
1 *GAMA 429 GFX Int LOW
(2)
See Note 1
2 VOR/ILS
LOW
(2)
SYS1 or SYS2
*GAMA 429 GFX Int
– this configuration has Flight Plan
information.
GND MAINT
– MISCELLANEOUS SETUP
CDI SELECT:
USE
With this configuration the EFD1000 will read the GNS480 CDI
logic state on the A429 bus and toggle between GPS and VLOC on
the PFD when pressing the GNS480 CDI button.
EFD1000 will use GPS/
NAV ID’s A and B
NOTE 1
– GPS SDI Setting
EFD1000 SW is v2.1 or below:
Set the SDI to COMMON on all single and dual 430/530 and
SYS1 or SYS2 for all single and dual GNS480.
EFD1000 SW is 2.2 and above:
Single GNS/GTN set to COMMON, Single 480 set to SYS1 or
SYS2.
Dual GNS/GTN - Set to LNAV1(SYS1) for GPS1 and
LNAV2(SYS2) for GPS2.
GTX-330 (When used as a Data
Concentrator)
The ARINC channel that is connected to the EFD1000 (i.e.
receiving the ARINC labels from the EFD1000) must be set
to “AHRS” on the GTX-330.
Transponder or GPS using RS232 ADC
Output
GTX-330
– configure for ADC W/ALT if using the EFD1000
as the encoding source. Configure for ADC NO ALT if
EFD1000 is not to supply encoding source but is used for
OAT/TAS and other labels.
GNS430/530
– configure for Shadin-adc or Shadin.
GTN6xx/7xx
– configure for Airdata Format 1 or Altitude
Format 3 as desired.
KLN90B
- no config required
KLN89B/94
– Set RS232 Air Data = Y in Maintenance
Pages.
GTN650/750 and GTN625/635/725
ARINC 429 CONFIG Page
IN 1
LOW
EFIS Format 3 or EFIS Format 2 if ACU2
installed and using EFD1000 Air Data.
IN 2
As required
OUT
LOW
(2)
GAMA Format 3
SDI
See Note 1
VOR/LOC/GS ARINC 429 CONFIG Page
SPEED
LOW
(2)
RX
LOW
(2)
TX
SDI
COMMON
LOW(2)
The GPS/VOR buss speeds are typically set to low but if the ACU2 is used or it is
required to use HS A429 for other devices these settings may need to be set t o HI
(Note if set to HI then the appropriate settings in the EFD1000 must be set to HIGH)
