EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 205-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
13
RESERVED
14
GND
AIRCRAFT GROUND
15
POWER
INPUT
AIRCRAFT POWER 9-28VDC
Table E4: EA100 P1 Connector Pin Out
EA100 P2 Connector
PIN
NAME
INPUT/ OUTPUT
FUNCTION
1
AP EXCITE HI
INPUT
ATTITUDE REFERENCE HI
2
AP PITCH HI
OUTPUT
PITCH HI
3
AP ROLL HI
OUTPUT
ROLL HI
4 -15
RESERVED
16
AP EXCITE LO
INPUT
ATTITUDE REFERENCE LO
17
AP PITCH LO
OUTPUT
PITCH LO
18
AP ROLL LO
OUTPUT
ROLL LO
19
AUX EXCITE LO
INPUT
ATTITUDE REFERENCE LO
20
AUX PITCH LO
OUTPUT
PITCH LO
21
AUX ROLL LO
OUTPUT
ROLL LO
22-30
RESERVED
31
AUX EXCITE HI
INPUT
ATTITUDE REFERENCE HI (32Vp-p max)
32
AUX PITCH HI
OUTPUT
PITCH HI
33
AUX ROLL HI
OUTPUT
ROLL HI
34-38
RESERVED
39
A/P INTRLK COMM
INPUT
“COMM” CONTACT ON RELAY
40
A/P INTRLK RELAXED
OUTPUT
RELAXED STATE OF RELAY
41
A/P INTRLK ENERGIZED OUTPUT
ENERGIZED STATE OF RELAY
42
A/P AHRS VALID
OUTPUT
ENERGIZED STATE OF RELAY
43
A/P AHRS INVALID
OUTPUT
RELAXED STATE OF RELAY
44
A/P AHRS COMM
INPUT
“COMM” CONTACT ON RELAY
Table E5: EA100 P2 Connector Pin Out
AML STC SA10822SC approves use of the Pitch/Roll attitude outputs for the autopilots identified in this
installation data. Other applications were not evaluated under this STC. Other uses of the TSO EA100
equipment must have separate approval for installation in an aircraft. Refer to the TSO Installation
Instructions (Aspen document 900-00018-001).
E5.7 Wiring Diagrams
A.
Wire Figure E8 in all installations.
B.
Select Figure E9 – E22 depending on autopilot type and wire as shown.
C.
Century autopilots only, build transformer box TR1 or TR2 as shown in Figure E7 or E7A and per
instructions in Section E5.5.
44
15
31
1
16
30
