Aspen Avionics EFD1000 - Page 96

EFD1000 Installation Manual
DOCUMENT # A-01-126-00 PAGE 96-225 Revision H
© Copyright 2009 Aspen Avionics Inc.
Over Braid or
Double Shield
Over Braid or
Double Shield
EFD1000
16
429 GPS RX1A
P4001 P4006 P5006P5001
46 46
24
429 GPS RX1B
17
47
24
47
23
Figure 9.8 Pro Digital & Analog Mix with and w/o Autopilot Interface
GNS430(W)(AW)
GNS530(W)(AW)
23
P3
4
5
48(50)
49(51)
48(50)
49(51)
ACU
P3
18
19
26
27 14
1
15
2
ACU RX4A
ACU RX4B
PFD 429 TX1A
PFD 429 TX1B
Autopilot-optional
See Figure:
9.16 for Bendix King
9.17 for S-TEC
9.18 for Century
9.19 for Cessna ARC
9.20 – 9.23A Flight Director
_
_
_
_
_
_
_
_
_
_
_
_
429 RX1B
429 RX1A
429 TX1B
429 TX1A
G
P
S
#
2
I
N
P
U
T
22
23
V
L
O
C
#
2
I
N
P
U
T
A
U
T
O
P
I
L
O
T
Analog VLOC #2 - optional
RS-232/Analog GPS #2 - optional
See Figure:
9.12 for KLN89/B & KLN94
9.13 for KLN-90/A/B
9.14 for GX-50/60 & GX-55/65
429 VLOC RX2A
429 VLOC RX2B
GNAV #1
RS-232 Flight Plan
To
EFD1000
Pin 8
429 TX2A
429 TX2B
1
Optional
Back-Up
Nav
Indicator
See Figure 9.24, 9.25, 9.26 for
Back-Up NAV recommendations.
2
3
ID#1
Description
A
A
A
ID#2
D
F
H
GNS430, No GPS2,
NAV2
GNS430, GPS2,
No NAV2
GNS430, GPS2,
NAV2
4
See Figure 9.15 for:
KX-155(A) &165(A)
KN-53
KX-170A/170B/175/175B
SL-30
Use pins 48 & 49 or 50 & 51 not both.
2
*GNS530 uses same config as GNS430
3
1
1
1
Over shield or over braid required on this
wire bundle to comply with HIRF &
Lightning. Extend within back shell if
possible. Ground at both ends.
5
3
Configuration Matrix
(see Section 10)
CNX-80
GNS-480
P5
4
24
5
25
8
28
4
4
See Figure 9.27 for GNS430/530
configuration.
6
Pins 4 & 24 may be swapped with pins
5 & 25 if configured accordingly below.
See Figure 9.27 for GNS-480 configuration.
D
F
H
Q
Q
Q
GNS480, No GPS2,
NAV2
GNS480, GPS2,
No NAV2
GNS480, GPS2,
NAV2
5
2
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.