EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 107-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
Figure 9-7: GNAV with ACU (Autopilot)
Figure 9-8: Reserved
Figure 9-9: Reserved
Over Braid or
Double Shield
Over Braid or
Double Shield
EFD1000
16
429 GPS RX1A
429 GPS RX1B
17
1
2
P1
P3
4
5
ACU/ACU2
P3
18
19
26
27
14
1
15
2
VLOC/ACU RX2A
VLOC/ACU RX2B
PFD 429 TX1A
PFD 429 TX1B
429 RX1B
429 RX1A
429 TX1B
429 TX1A
A
U
T
O
P
I
L
O
T
429 RX2A
429 TX2A
429 TX2B
429 RX2B
1
ID#1
Description
B
ID#2
NONE
GNS430
With Autopilot
2
Use pins 48 & 49 or 50 & 51 not both.
3
1
*GNS530, GNS480 and GTN650/750 use
same config as GNS430
1
Over shield or over braid required on this wire
bundle to comply with HIRF & Lightning. Extend
within back shell. Ground at both ends.
4
Configuration Matrix
(see Section 10)
6
Pins 4 & 24 may be swapped with pins 5 & 25 if
configured accordingly.
Requires GNS-480 SW v2.3. See Figure 9-27 for GNS-
480 configuration.
5
See Figure 9-27 for GNAV configuration.
Refer to manufacturers’ documentation to verify the
integration data and for information regarding
checkout procedures. This drawing, as it pertains
to the non-Aspen equipment, is for reference only.
Autopilot
See Figure:
9-16 to 9-20 for Autopilot
Px001
Px006
46
GNS430/W
GNS530/W
47
24
23
48(50)
49(51)
_
_
_
_
_
_
CNX-80
GNS-480
P5
4
24
5
25
8
28
24
P1001
P1004
23
10
29
48
67
GTN6xx/7xx
_
_
_
_
_
_
25
57
4
2
GNAV
2
See Fig 9-28A for optional
air data interface
If 429 IN 1 is in use see manufacturers installation
instructions and wire to another unused 429 IN Port.
7
5
6
4
