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190-01007-A3 GTN 6XX/7XX AML STC Installation Manual
Rev. 4 Page E-77
GTN 6XX/7XX
P1001
50
69
MAIN LATERAL +FLAG OUT
MAIN LATERAL -FLAG OUT
49
68
MAIN LATERAL +LEFT OUT
MAIN LATERAL +RIGHT OUT
51
70
12
31
MAIN VERTICAL +UP OUT
MAIN VERTICAL +DOWN OUT
56
ILS/GPS APPROACH*
CESSNA
800B
CA550A/
FD
J1/P5
400B
CA550A/
FD
300B
CA550A/
FD
MAIN VERTICAL +FLAG OUT
MAIN VERTICAL -FLAG OUT
LATERAL +FLAG
LATERAL -FLAG
LATERAL +LEFT
LATERAL +RIGHT
VERTICAL +FLAG
VERTICAL -FLAG
VERTICAL +UP
VERTICAL +DOWN
NAV FLAG +
NAV FLAG -
G/S FLAG+
G/S FLAG-
G/S +UP
G/S +DOWN
L/R +LT
L/R +RT
LOC SWITCH
AUTOPILOT
s
s
s
s
J1/P4 J2/P5
-
-
-
-
-
-
18
17
-
-
-
5
2
-
-
-
-
9
-
-
-
-
-
-
18
17
-
-
-
5
2
-
-
-
-
9
-
-
-
-
-
-
18
17
-
-
-
5
2
-
-
-
-
9
J1/P4 J2/P5 J1/P4 J2/P5
300IFCS
CA530FD
400IFCS
CA530FD
800IFCS
CA530FD
J1/P5 J1/P5
-
-
A
B
-
-
C
D
-
-
A
B
-
-
C
D
-
-
A
B
-
-
C
D
To Main CDI
4 4 4
5 5 5
s
6
s
s
s
6
6
6
1. ALL WIRES 24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED.
2. GROUND DESIGNATIONS: SHIELD BLOCK GROUND AIRFRAME GROUND
3. AT GTN 6XX/7XX, CONNECT SHIELD GROUNDS TO THE CONNECTOR BACKSHELL -- THE SHIELD TERMINATION LEADS MUST BE LESS
THAN 3.0". CONNECT OTHER END OF THE SHIELD PER THE REMOTE EQUIPMENT INSTALLATION REQUIREMENTS. IF NO SHIELD
TERMINATION REQUIREMENT EXISTS FOR THE REMOTE EQUIPMENT, TERMINATE SHIELDS AS SHORT AS POSSIBLE, NOT TO EXCEED
3.0". SEE SECTION 2.4.11.4.
4. THE ILS/GPS APPROACH DISCRETE OUTPUT MUST ALSO BE CONNECTED TO THE BACK COURSE RELAY – REFER TO
MANUFACTURER’S DOCUMENTATION FOR ADDITIONAL DETAILS.
5. REFER TO MANUFACTURER’S DOCUMENTATION FOR CORRECT CONNECTION OF THE VOR/LOC RELAY USING AN ACTIVE LOW INPUT.
6. THE SPLICE MUST BE PERFORMED AT THE CONNECTOR END OF THE WIRE. SPLICE AS SHOWN:
s
NOTES:
PXX
s
s
LRU
7
7. FOR IFR-CERTIFIED COMPOSITE AIRCRAFT ONLY (EACH AIRCRAFT IN APPENDIX G THAT REQUIRES OVERBRAID OVER THE GPS/
WAAS CABLE): ANY LRU (I.E. CDI, AUTOPILOT) THAT CONNECTS TO THE GTN’S P1001 MAIN CDI/VDI OUTPUTS MUST BE MOUNTED TO
THE INSTRUMENT PANEL OR COCKPIT CENTER CONSOLE WITH ELECTRICAL BONDING EQUAL TO OR LESS THAN 20 MILLIOHMS
BETWEEN THE EQUIPMENT AND THE INSTRUMENT PANEL.
Figure E-33. GTN 6XX/7XX – Cessna Autopilot Interconnect
373


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