Figure B-15 Autopilot/Flight Director Interconnect - Collins - Garmin GI 275 Installation Manual

GI 275
(Pilot s Primary ADI
or Pilot s HSI)
P2752
LATERAL +LEFT OUT 48
LATERAL +RIGHT OUT 10
s
VERTICAL +UP OUT 9
VERTICAL +DN OUT 68
s
LATERAL +FLAG OUT 63
LATERAL -FLAG OUT 66
s
VERTICAL +FLAG OUT 24
VERTICAL -FLAG OUT 5
s
A/P HEADING ERROR HI 13
A/P HEADING ERROR LO 52
s
A/P COURSE ERROR HI 32
A/P COURSE ERROR LO 71
s
ILS/GPS APPROACH
1
(~DISCRETE OUT 7 LO)
26 VAC REF HI 65
26 VAC REF LO 7
8 FD ENABLE HI
18
FD ROLL RIGHT 38
FD ROLL LEFT 77
8
s
FD PITCH DOWN 58
FD PITCH UP 19
s
ADI
COLLINS
(on copilot s side)
FD-112 C/V
1 2
P2
Z
OFF MODE +
U
ROLL CMD +RIGHT
T
ROLL CMD +LEFT
F
PITCH CMD +UP
k
PITCH CMD +DOWN

Figure B-15 Autopilot/Flight Director Interconnect - Collins

190-02246-10
Rev. 11
s
AIRCRAFT 26 VAC 400 HZ AC
7
REFERENCE VOLTAGE
(OPTIONAL)
Sheet 1 of 2
161H-1
J1
42
38
11
30
34
37
41
3 4
+28 VDC
N/C
P/N 1N4007 OR
EQUIVALENT
OUT OF VIEW+
RELAY
28
52
GI 275 Part 23 AML STC Installation Manual
AUTOPILOT
AP-106/107 COMPUTER
913K-1/1A
J1 J2
- - LAT DEV +LT
- - LAT DEV +RT
7 - - GS DEV +UP
- - GS DEV +DN
- 23 NAV LL FLAG +
5
- 20 NAV LL FLAG -
- 1 - GS HL FLAG +
- 2 - GS HL FLAG -
- 24 - HDG ERROR HI
- 25 - HDG ERROR LO
22 - CRS DATUM HI
21 - CRS DATUM LO
2 27 - LOC FREQ GND
6
- - - 26 VAC 400 HZ REF I
- 29 - 26 VAC 400 HZ REF II
- 26 - 26 VAC IN LO
- - 33 OUT OF VIEW+
- - 28 ROLL STEER +RT
- - SIG COM (K-1)
20 - SIG COM (K-1)
- 8 - PITCH STEER +DN
Page B-43