Figure B-14 Autopilot/Flight Director Interconnect - Cessna - Garmin GI 275 Installation Manual

Part 23 aml stc
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GI 275
(Pilot s Primary ADI
or Pilot s HSI)
P2752
LATERAL +LEFT OUT
48
LATERAL +RIGHT OUT
10
s
LATERAL +FLAG OUT
63
N/C
LATERAL -FLAG OUT
66
N/C
VERTICAL +UP OUT
9
VERTICAL +DN OUT
68
s
VERTICAL +FLAG OUT
24
N/C
VERTICAL -FLAG OUT
5
N/C
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)
FD ENABLE HI
18
FD ROLL RIGHT
38
FD ROLL LEFT
77
13
s
FD PITCH UP
19
FD PITCH DOWN
58
s
ADI
4
CESSNA
(on copilot s side)
G-1050A
G-550A
P1
CMD BAR N VIEW
24
CMD BAR +RT
26
CMD BAR +LT/REFERENCE
27
CMD BAR +UP
28
CMD BAR +DN
29
GI 275
P2752
PITCH AC OUT HI
6
PITCH AC OUT LO
64
s
ROLL AC OUT HI 26
ROLL AC OUT LO
45
s
10 VAC REF HI
27
10 VAC REF LO
46
s
NO
23
GYRO
VALID RELAY
COM
3

Figure B-14 Autopilot/Flight Director Interconnect - Cessna

190-02246-10
Rev. 11
J1
8
9
26
10
-
8
ATTITUDE
TEST SWITCH
C
NC
NO
13
9
N/C
10
Sheet 2 of 5
300B/400B/800B IFCS
S-550A
CA550A/FD
J1
J2
J3
J1
-
-
5
-
-
-
22
-
-
-
16
-
-
-
4
-
-
-
1
-
-
-
6
-
-
-
15
-
-
-
14
-
12
-
-
-
13
-
-
-
-
-
21
-
-
-
24
-
-
-
-
15
6
-
-
-
-
-
-
-
-
-
10
-
-
-
19
-
-
5
19
-
-
-
-
11
-
-
-
1
-
-
-
22
-
-
-
1
-
-
300B/400B/800B IFCS
S-550A
CA550A/FD
CA550A/FD
J1
J2
J3
J1
J2
J1/P4
-
-
-
-
15
-
-
-
-
7
-
7
-
-
-
-
4
-
-
-
-
33
-
33
-
-
-
-
19
19
-
3
-
-
-
-
-
-
-
-
32
-
GI 275 Part 23 AML STC Installation Manual
MODE CONTROLER
400B
CA550A/FD
J2
J1/P4
J2/P5
-
-
5
VOR/LOC SIGNAL (+LT)
-
-
2
VOR/LOC SIGNAL (+RT)
-
-
-
NAV #2 VOR/LOC (+LT)
-
-
-
NAV #2 VOR/LOC (+RT)
-
18
-
G/S SIGNAL (+UP)
-
17
-
G/S SIGNAL (+DN)
-
-
-
NAV #2 G/S SIG (+UP)
-
-
-
NAV #2 G/S SIG (+DN)
-
24
-
DC HDG GYRO IN
-
-
-
#2 DC HDG GYRO IN
-
-
17
DC COURSE DATUM IN
-
-
-
#2 DC COURSE SIG IN
-
15
-
AC COURSE DATUM
20
-
20
AC HDG GYRO IN
-
-
9
VOR/LOC RELAY RTN*
-
-
-
NAV #1 LOC GND
-
-
-
NAV #2 LOC GND
-
-
-
FD COMPUTER ON
-
-
-
ADI ROLL BAR
-
-
-
SIGNAL COM/ROLL +LT
-
-
-
ADI PITCH BAR
-
-
-
ADI PITCH + DN
CESSNA
AUTOPILOT
400B AF
C-530A
J2/P5
J1
J2
-
L
-
PITCH IN
-
-
-
PITCH/ROLL TEST
4
-
-
ROLL IN
-
-
-
400 HZ REF
-
-
-
400 HZ RETURN
-
-
A
A/P DISABLE IN
32
-
-
400 Hz EXT OSC
Page B-39
2
7

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