Garmin GI 275 Installation Manual page 404

NOTES
FLIGHT DIRECTOR LOGIC OUTPUT FROM THE 55/55X (P2-4) MUST NOT BE CONNECTED TO ST-645
REMOTE ANNUNCIATOR (P1-20). IF THE ST-645 WAS PREVIOUSLY INSTALLED, THE WIRE CONNECTING
1
THE 55/55X COMPUTER P2-4 TO ANNUNCIATOR P1-20 MUST BE REMOVED OR CAPPED AND STOWED.
TO SUPPORT THE FLIGHT DIRECTOR INTERFACE WITH THE GI 275, THE PILOT-ACCESSIBLE PARALLAX
2
POT CONNECTIONS MUST BE REMOVED.
THE FLIGHT DIRECTOR CANNOT BE DISPLAYED ON AN ADI ON THE CO-PILOT'S SIDE BECAUSE THERE IS
NO WAY TO ADJUST THE FLIGHT DIRECTOR OFFSET FOR THIS ADI AFTER THE PARALLAX POT IS
3
REMOVED.
IF THE GI 275 IS REPLACING A DIRECTIONAL GYRO, ENSURE THE "DG GROUND STRAP" JUMPER IS
4
REMOVED.
IF THE GI 275 IS BEING INSTALLED IN AN AIRCRAFT THAT HAD NO HEADING SYSTEM, ENSURE THAT THE
5
"NO HEADING SYSTEM" JUMPER IS REMOVED.
THE ST-670 (P/N 01180 FOR THE KI-256) IS REQUIRED TO SUPPORT THE FLIGHT DIRECTOR DISPLAY FROM
6
THE S-TEC 60-2 AND 65 AUTOPILOTS.
CONNECTIONS MUST BE MADE TO THE PILOT'S PRIMARY ADI ONLY.
7
Figure B-18 Autopilot/Flight Director Interconnect - S-TEC
190-02246-10
Rev. 11
Sheet 4 of 4
GI 275 Part 23 AML STC Installation Manual
Page B-59