Garmin GI 275 Installation Manual page 396

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
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
LATERAL +FLAG OUT 63
LATERAL -FLAG OUT 66
s
VERTICAL +FLAG OUT 24
VERTICAL -FLAG OUT 5
s
ILS/GPS APPROACH
1
(~DISCRETE OUT 7 LO)
HDG/CRS DATUM VALID
72
(~DISCRETE OUT 4 LO)
¼ WATT
A/P BACKCOURSE
14
(~DISCRETE OUT 5 LO)
TO GI 275
C/B
18
FD ENABLE IN HI 18
FD ROLL RIGHT 38
FD ROLL LEFT 77
20
s
FD PITCH UP 19
FD PITCH DOWN 58
s
ADI
(copilot s side)
KCI 310
1 2
P1
CMD BAR RETRACT R
ROLL CMD BAR IN T
PITCH CMD BAR IN P
CMD BAR REF W
Figure B-17 Autopilot/Flight Director Interconnect - Honeywell (Bendix/King)
190-02246-10
Rev. 11
4" ADI Replacement – Basic
(cont d on Attitude page)
TO GI 275 CIRCUIT
BREAKER 18
2 M,
26 VAC 400 REF
(SEE ATTITUDE PAGE)
BACKCOURSE
RELAY
TO
KAC 325 TP-43
NC NC
4
AND
KDC 380 J1-R
NO NO
AP TEST
ONLY REQUIRED
WHEN KCI 310 IS NOT
CONNECTED
TO AUTOPILOT
CIRCUIT BREAKER
14
FUSE, 5A
OR LESS
100 K , ¼ WATT
Sheet 6 of 10
KFC 250 (4" INSTRUMENTS)
KCP 299
KA141 KC290
w/ 065-5015-XX
Adapter Card
P2991 P2992 P141
- C -
- A -
M - -
K - -
- H -
- M -
- W -
- S -
- - -
- - -
C - -
D - -
AA - -
c - -
- - -
- - -
H - -
- - -
- - -
15 16
- p _
- EE -
- BB -
F - 3
17
GI 275 Part 23 AML STC Installation Manual
BENDIX KING
AUTOPILOT
KFC 300
KCP 320
J2901 J1 J2TP J2BP
- 2 - - LAT DEV +LT
- 1 - - LAT DEV +RT
- 3 - - GS DEV +UP
- 4 - - GS DEV +DOWN
- 12 - - HDG DATUM HI
- 13 - - HDG DATUM LO
- 14 - - CRS DATUM HI
- 15 - - CRS DATUM LO
- - 30 - LAT DEV FLAG +
- - 31 - LAT DEV FLAG -
- - 24 - GS DEV FLAG +
- - 25 - GS DEV FLAG -
- - 29 - ILS ENERGIZE (A/P IN)
- - - - COMPASS VALID
- 17 - - COURSE DATUM COS-
- 16 - - COURSE DATUM COS+
- 19 - - 26 VAC 400 HZ REF HI
- - - 5 26 VAC 400 HZ REF LO
- - 40 - PRE-FLT TEST SWITCH
- CMD BAR RETRACT
9 - -
- 30 - - ROLL CMD BAR OUT
- 29 - - PITCH CMD BAR OUT
A - - 10 CMD BAR REF
Page B-51