Aspen Avionics EFD1000 E5 - Figure 9-11: RS-232 GPS with ACU (Analog Nav And;Or Autopilot)

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 109-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
Figure 9-11: RS-232 GPS with ACU (Analog Nav and/or Autopilot)
Over Braid or
Double Shield
Over Braid or
Double Shield
EFD1000
GPS/VLOC RX2A
GPS/VLOC RX2B
ACU/ACU2
P3
18
19
26
27
14
1
15
2
PFD 429 TX1A
PFD 429 TX1B
Autopilot - optional
429 RX1B
429 RX1A
429 TX1B
429 TX1A
G
P
S
I
N
P
U
T
A
U
T
O
P
I
L
O
T
RS-232/Analog GPS #1
See Figure:
9.12 for KLN89/B & KLN94
9.13 for KLN-90/A/B
9.14 for GX-50/60 & GX-55/65
RS-232 Flight Plan
To
EFD1000
Pin 9
Analog VLOC #1
Optional
Back-Up
Nav
Indicator
V
L
O
C
#
1
See Figure 9.24, 9.25, 9.26 for Back-Up
NAV recommendations.
2
1
2
3
1
ID#1
Description
G
H
ID#2
NONE
NONE
GPS1, No NAV1
GPS1,NAV1
See Figure 9.15 for:
KX-155(A) &165(A)
KN-53
KX-170A/170B/175/175B
SL-30
1
Over shield or over braid required on this wire
bundle to comply with HIRF & Lightning. Extend
within back shell. Ground at both ends.
3
Configuration Matrix
(see Section 10)
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.
See Figure:
9.16 to 9.20 for Autopilot