Figure B-17 Autopilot/Flight Director Interconnect - Honeywell (Bendix/King - Garmin GI 275 Installation Manual

GI 275
(Pilot s Primary ADI
or Pilot s HSI) P2752
LATERAL +FLAG OUT 63 N/C
LATERAL -FLAG OUT 66 N/C
LATERAL +LEFT OUT 48
LATERAL +RIGHT OUT 10
s
VERTICAL +UP OUT 9
VERTICAL +DN OUT 68
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
VERTICAL +FLAG OUT 24
VERTICAL -FLAG OUT 5
s
GPS SELECT
40
(~DISCRETE OUT 8 LO)
ILS/GPS APPROACH
1
(~DISCRETE OUT 7 LO)
HDG/CRS DATUM VALID
72
(~DISCRETE OUT 4 LO)
PITCH AC OUT HI 6
PITCH AC OUT LO 64
s
ROLL AC OUT HI 26
20 ROLL AC OUT LO 45
s
10VAC REF IN HI 27
10VAC REF IN LO 46
s
20
TO
AUTOPILOT
C/B
9
NO 23
GYRO VALID
NC 42 N/C
RELAY
COM 3
TO
20
AUTOPILOT
C/B
9
NO 23
GYRO VALID
NC 42 N/C
RELAY
COM 3
YAW RATE HI 15
20
YAW RATE LO 73
s
20
11
BARO CORRECTION HI 35
BARO CORRECTION LO 54
s
FD ENABLE HI 18
FD ROLL RIGHT 38
FD ROLL LEFT 77
20
s
FD PITCH UP 19
FD PITCH DOWN 58
s
FLIGHT DIRECTOR FOR KFC 150 ONLY
KI 256 ADI
(copilot s side)
KI 256
1 2
P2561
CMD BAR RETRACT P
ROLL CMD BAR IN M
PITCH CMD BAR IN L
CMD BAR REF N

Figure B-17 Autopilot/Flight Director Interconnect - Honeywell (Bendix/King)

190-02246-10
Rev. 11
A/P DISC RELAY
5
(EXISTING)
NO NC NO NC
A/P DISC SW
C C
(EXISTING)
TO GI 275 C/B
18
TO A/P (TRIM)
WARNING
5
A/P DISC / SONALERT
TRIM INTR
(EXISTING)
TO GI 275 C/B
18
REPLACES KRG 331
REPLACES KEA 130A
13
Sheet 1 of 10
KAP 100
KC 190 KC 191/192
P1901 P1902 P19X1 P19X2
U - U
17 - 17
- -
- -
X - X
- 20
20
W - W
19 - 19
- -
- -
- -
B - B
1 -
Y - Y
21 - 21
- C
Z -
- 1
6
TO A/P (TRIM)
WARNING
SONALERT
AP DISC
RELAY
(EXTERNAL)
DISENG
- B
12
ENG
8
OR
DISENG
- B
12
ENG
8
AP DISC
RELAY
(EXTERNAL)
- -
- -
- -
10
- - 15
N/C - -
- -
- -
- - 16
- - C
- - E
- -
GI 275 Part 23 AML STC Installation Manual
3
AUTOPILOT
KAP 150 / KFC 150
KAS
KC 296
297B
P2961 P2962 P297B1
- - - - LAT DEV +LT
- - - - LAT DEV +RT
- V - - - GS DEV +UP
- 19 - - - GS DEV +DOWN
- - - - HDG DATUM HI
-
- - - HDG DATUM LO
- - - - CRS DATUM HI
- - - - CRS DATUM LO
- 21 - - - GS DEV FLAG +
- Y - - - GS DEV FLAG -
- - - - - GPS SELECT (GND=GPS)
- - - - ILS ENERGIZE (A/P IN)
1 - - - - COMPASS VALID
- - - PITCH ATTITUDE HI
-
- - - - ROLL ATTITUDE HI
- C - - - VG EXCITATION
Z - - - - VG REF
- 1 - - - PWR REF
- B - - - AP DISC
- B - - - AP DISC
- - 2 - - YAW RATE (HIGH)
- - C - - YAW RATE (LOW)
- - - 7 - YAW ANNUNCIATE
- - - - YD ANNUNCIATE
- - - - 4 BARO EXCITATION
- - - - 7 BARO SET (IN)
- - - - 3 BARO/XPDR REF
- - - - CMD BAR RETRACT
- - - - ROLL CMD BAR OUT
- - - - PITCH CMD BAR OUT
- A - - - CMD BAR REF
Page B-46