Garmin GI 275 Installation Manual page 386

GI 275
(Pilot s Primary ADI only)
13
P2752
PITCH AC OUT HI 6
PITCH AC OUT LO 64
s
ROLL AC OUT HI 26
ROLL AC OUT LO 45
s
26 VAC REF HI 65
26 VAC REF LO 7
s
10 VAC REF HI 27
10 VAC REF LO 46
s
11
GYRO VALID NO 23
22 AW G
COM 3
RELAY
190-02246-10
Rev. 11
CA-1050A
Com puter
PK42 PK43 PK44
- 16
- GND
- 3
- -
- -
- -
- -
12
- -
- -
18 -
- -
22 AW G
ACTUATOR
INTERLOCK
CIRCUIT
Figure B-14 Autopilot/Flight Director Interconnect - Cessna
-0001 -0002, -0102
C-1050A AC-1050A CA-1050A C-1050A AC-1050A
Control Unit Air Data Com puter Control Unit Air Data
PK40 PK39 PK42 PK43 PK44 PK40 PK39
- - - - - - 11 -
- - - - - - GND -
- 13 - - 16 - 12 -
- 11 - - 3 - - -
- GND - - GND - - -
- - - - - - - -
- - - - - - - -
- - 24 - - - - 24
- - 25 - - - - 25
- - - 18 - - - -
37 - - - - 37 - -
Sheet 4 of 5
-0004 -0005, -0105
CA-1050A C-1050A AC-1050A CA-1050A
Com puter Control Unit Air Data Com puter
PK42 PK43 PK44 PK40 PK39 PK42 PK43 PK44
- 16 - - - - - -
- GND - - - - - -
- 3 - 13 - - 16 -
- - - 11 - - 3 -
- - - GND - - GND -
- - - - 23 - - -
- - - - 25 - - -
- - - - - - - -
- - - - - - - -
18 - - - - 18 - -
- - 37 - - - - 37
GI 275 Part 23 AML STC Installation Manual
1000 IFCS
C -1050A AC-1050A
Control Unit Air Data
PK40 PK39
11 - PITCH IN
GND -
12 - PITCH/ROLL TEST**
- - ROLL IN
- -
- 23 26 V, 400 Hz
- 25
26 V, 400 Hz RTN
- - 10 V, 400 Hz
- - 10 V, 400 Hz RTN
- -
ENGAGE INTLK
- -
GYRO VALID
Page B-41