FreeFlight 2101 I/O Approach Plus Installation And Checkout Manual page 35

PINOUT BY PIN NUMBER
PIN TYPE
J2-1 SYNCHRO IN
J2-2 SYNCHRO IN
J2-3 SYNCHRO IN
J2-4 SYNCHRO IN
J2-5 SYNCHRO IN
J2-6 SYNCHRO IN
J2-7 26 VAC GROUND
J2-8 26 VAC IN
J2-9 ARINC 419/429 IN
J2-10 SYNCHRO, ARINC 565 IN
J2-11 DISCRETE IN
J2-12 SYNCHRO, ARINC 565 IN
J2-13 DISCRETE IN
J2-14 SYNCHRO, ARINC 565 IN
J2-15 ARINC 419/429 IN
J2-16 ARINC 419/429 OUT
J2-17 26 VAC GROUND
J2-18 26 VAC IN
J2-19 DISCRETE IN
J2-20 SYNCHRO IN
J2-21 26 VAC IN
J2-22 SYNCHRO IN
J2-23 ARINC 419/429 OUT
J2-24 SYNCHRO IN
J2-25 26 VAC GROUND
J2-26 DISCRETE OUT
J2-27 DISCRETE OUT
J2-28 DISCRETE OUT
J2-29 DISCRETE OUT
J2-30 OUT
J2-31 DISCRETE OUT*
J2-32 ARINC 561/568 OUT
J2-33 GROUND
J2-34 GROUND
J2-35 SYNCHRO OUT
J2-36 SYNCHRO OUT
J2-37 SYNCHRO OUT
J2-38 SYNCHRO OUT
J2-39 GROUND
J2-40 SYNCHRO OUT
J2-41 GROUND
J2-42 SYNCHRO OUT
J2-43 GROUND
J2-44 26 VAC IN
J2-45 26 VAC IN
J2-46 OUT
J2-47 ARINC 561/568 OUT
J2-48 DISCRETE OUT
J2-49 ARINC 561/568 OUT
* Reserved for future use.
Revision E
May 31, 2006
SIGNAL
ALTITUDE FINE (Z)
ALTITUDE COURSE (X)
ALTITUDE FINE (Y)
ALTITUDE COURSE (Y)
ALTITUDE FINE (X)
ALTITUDE COURSE (Z)
ALTITUDE REF (C)
ALTITUDE REF (H)
RX1A
TAS (X), SIGNAL
ALTITUDE VALID (+28 VDC)
TAS (Y), ARINC 565 REFERENCE
TAS VALID (+28 VDC)
TAS (Z), ARINC 565 COMMON
RX1B
TX1A
TAS/SYNCHRO/ARINC 565 REF (C)
TAS/SYNCHRO/ARINC 565 REF (H)
HEADING VALID (+28 VDC)
HEADING (X)
HEADING REFERENCE (H)
HEADING (Y)
TX1B
HEADING (Z)
HEADING REFERENCE (C)
APPROACH ANNUNCIATOR
APPROACH ENABLE
LEG CHANGE
HSI SYNCHRO VALID (+28 VDC)
RESERVED
GLIDESLOPE VALID (+28 VDC)*
6W DATA (H)
GROUND
GROUND
SYNCHRO 1 (Y)
SYNCHRO 1 (X)
SYNCHRO 2 (Y)
SYNCHRO 2 (X)
6W (C), AP DEV +RT/-LT (C)
SYNCHRO 3 (X)
SYNCHRO 1(Z), 2(Z), 3 (Z) and AP (C)
SYNCHRO 3 (Y)
HSI REF (C), AP REF (C)
HSI REF (H)
AP REF (H)
ROLL STEERING (H)
6W CLOCK (H)
ROLL STEERING VALID (+28 VDC)
6W SYNC (H)
Figure 2-2 FreeFlight 2101 I/O Approach Plus J2 Pin-out
FreeFlight 2101 I/O Approach Plus GPS Navigation System
NOTE
GND TO AIRCRAFT PER ARINC 407
GND TO AIRCRAFT PER ARINC 407
SEE TABLES 3-2 AND 3-3
SEE TABLES 3-2 AND 3-3
SEE APPENDIX C PARAGRAPH C.2.8
SEE APPENDIX C PARAGRAPH C.2.8
GND TO AIRCRAFT PER ARINC 407
ACTIVE GND
ACTIVE GND
ACTIVE GND
RESERVED FOR FUTURE USE
USE J1-26 FOR VALID IF REQUIRED
393 mV/DEGREE
USE J1-26 FOR VALID IF REQUIRED
USE J1-26 FOR VALID IF REQUIRED
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