Aspen Avionics EFD1000 E5 - Figure 9-28 A: Digital Heading;Adc Outputs

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 131-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
Figure 9-28A: Digital Heading/ADC Outputs
Over Braid or
Double Shield
EFD1000
14
13
15
RS232 TX3
RS232 TX2
RS232 TX1
26
A429 TX1A
A429 TX1B
27
3
GNS430
GNS530
GTX330
Other Transponder
or GPS capable of
RS232 Format Z
P3301 PX001
24
57*
KLN89B
KLN94
KLN90B
Other GPS capable of
RS232 Format C
P901 PXX1
36
1
Pin
ARINC 429 Hi or Lo Speed
Heading and Air Data
2
A429 RXA
A429 RXB
3
See Section 8 of this manual for complete list of RS232
and A429 labels supported.
This note is not used
1
Configure Output for:
ADC TYPE 1 = Format Z (Garmin)
ADC TYPE 2 = Format C (King)
If ACU is installed parallel this EFD output with ACU and
other device requiring A429 Heading and/or Air Data.
2
4
A429 TX2A
A429 TX2B
5
P3
to optional GPS
(see Fig 9-7)
ACU
ARINC 429 Heading & ADC
RS-232 Heading & ADC
4
4
ACU transmits low speed 429 only.
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.
5
Pin
ARINC 429 Lo Speed
Heading only
A429 RXA
A429 RXB
ARINC 429 Heading
4
A429 TX2A
A429 TX2B
5
P3
to optional GPS
(see Fig 9-7)
ACU2
Pin
ARINC 429 Hi & Lo Speed
Heading and ADC
A429 RXA
A429 RXB
ARINC 429 Heading & ADC
25*
P1001
GTN
6xx/7xx
* other unused RS232 inputs may work
27*
GDL
84/88
P881
GTX
345
P3251
30*
GTX 345 requires sw 2.05 or later
5
6
3
3
3