Aspen Avionics EFD1000 E5 - 9.2 Optional Interfaces - ACU and ACU2

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 103-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
Figure #
Description
9-13
KLN-90/A/B Interface
9-14
Apollo GX-50/55/60/65 Interface
9-15
Analog NAV/VLOC Interface
9-15A
Analog Narco and ARC Navigation Radio Interface
9-16
Bendix/King KAP and KFC 100/140/150/200/250 Autopilot Interface
9-17
S-TEC autopilot interface
9-18
Century autopilot interface
9-18A
Century 21/31/41/2000
9-18B
Century IIB/III 1C388/M & 1C388C/MC
9-18C
Century IIB/II 1C388-2/-3
9-18D
Century IV
9-19
Cessna ARC 300B/400B/800B
9-19A
Cessna 300/400/800 IFCS
9-19B
Cessna Navomatic 400/400A
9-19C
Cessna Navomatic 300A
9-19D
Cessna Navomatic 300
9-20
Bendix FCS-810
9-24
Back-Up NAV Indicator (internal converter)
9-25
Back-Up NAV Indicator (OBS Resolver)
9-26
Back-Up NAV/GPS Indicator (OBS Resolver)
9-27
Non-Aspen Equipment Configuration Notes
Appendix E
EA100 Autopilot Attitude Source, Bendix King and Century – See Appendix E
Table 9-1: E5 Wiring Diagrams
9.2 Optional Interfaces – ACU and ACU2
Figure #
Description
ACU
ACU2
9-28A
Magnetic Heading – Low Speed ARINC 429
X
X
9-28A
Magnetic Heading – High Speed ARINC 429
X
9-28A
Air Data output (ARINC 429) – ACU installations must use RS-232 output from
EFD (Fig 9.28) for Air Data output.
X
9-28B
Magnetic Heading -ARINC 407 Synchro
X
Table 9-2: Optional ACU/ACU2 Interfaces