Page 2-7
Revision E
May 31, 2006
FreeFlight 2101 I/O Approach Plus GPS Navigation System
PINOUT BY PIN NUMBER
PIN
TYPE
SIGNAL
NOTE
J2-1
SYNCHRO IN
ALTITUDE FINE (Z)
GND TO AIRCRAFT PER ARINC 407
J2-2
SYNCHRO IN
ALTITUDE COURSE (X)
J2-3
SYNCHRO IN
ALTITUDE FINE (Y)
J2-4
SYNCHRO IN
ALTITUDE COURSE (Y)
J2-5
SYNCHRO IN
ALTITUDE FINE (X)
J2-6
SYNCHRO IN
ALTITUDE COURSE (Z)
GND TO AIRCRAFT PER ARINC 407
J2-7
26 VAC GROUND
ALTITUDE REF (C)
J2-8
26 VAC IN
ALTITUDE REF (H)
J2-9
ARINC 419/429 IN
RX1A
SEE TABLES 3-2 AND 3-3
J2-10
SYNCHRO, ARINC 565 IN
TAS (X), SIGNAL
J2-11
DISCRETE IN
ALTITUDE VALID (+28 VDC)
J2-12
SYNCHRO, ARINC 565 IN
TAS (Y), ARINC 565 REFERENCE
J2-13
DISCRETE IN
TAS VALID (+28 VDC)
J2-14
SYNCHRO, ARINC 565 IN
TAS (Z), ARINC 565 COMMON
J2-15
ARINC 419/429 IN
RX1B
SEE TABLES 3-2 AND 3-3
J2-16
ARINC 419/429 OUT
TX1A
SEE APPENDIX C PARAGRAPH C.2.8
J2-17
26 VAC GROUND
TAS/SYNCHRO/ARINC 565 REF (C)
J2-18
26 VAC IN
TAS/SYNCHRO/ARINC 565 REF (H)
J2-19
DISCRETE IN
HEADING VALID (+28 VDC)
J2-20
SYNCHRO IN
HEADING (X)
J2-21
26 VAC IN
HEADING REFERENCE (H)
J2-22
SYNCHRO IN
HEADING (Y)
J2-23
ARINC 419/429 OUT
TX1B
SEE APPENDIX C PARAGRAPH C.2.8
J2-24
SYNCHRO IN
HEADING (Z)
GND TO AIRCRAFT PER ARINC 407
J2-25
26 VAC GROUND
HEADING REFERENCE (C)
J2-26
DISCRETE OUT
APPROACH ANNUNCIATOR
ACTIVE GND
J2-27
DISCRETE OUT
APPROACH ENABLE
ACTIVE GND
J2-28
DISCRETE OUT
LEG CHANGE
ACTIVE GND
J2-29
DISCRETE OUT
HSI SYNCHRO VALID (+28 VDC)
J2-30
OUT
RESERVED
J2-31
DISCRETE OUT*
GLIDESLOPE VALID (+28 VDC)*
RESERVED FOR FUTURE USE
J2-32
ARINC 561/568 OUT
6W DATA (H)
USE J1-26 FOR VALID IF REQUIRED
J2-33
GROUND
GROUND
J2-34
GROUND
GROUND
J2-35
SYNCHRO OUT
SYNCHRO 1 (Y)
J2-36
SYNCHRO OUT
SYNCHRO 1 (X)
J2-37
SYNCHRO OUT
SYNCHRO 2 (Y)
J2-38
SYNCHRO OUT
SYNCHRO 2 (X)
J2-39
GROUND
6W (C), AP DEV +RT/-LT (C)
J2-40
SYNCHRO OUT
SYNCHRO 3 (X)
J2-41
GROUND
SYNCHRO 1(Z), 2(Z), 3 (Z) and AP (C)
J2-42
SYNCHRO OUT
SYNCHRO 3 (Y)
J2-43
GROUND
HSI REF (C), AP REF (C)
J2-44
26 VAC IN
HSI REF (H)
J2-45
26 VAC IN
AP REF (H)
J2-46
OUT
ROLL STEERING (H)
393 mV/DEGREE
J2-47
ARINC 561/568 OUT
6W CLOCK (H)
USE J1-26 FOR VALID IF REQUIRED
J2-48
DISCRETE OUT
ROLL STEERING VALID (+28 VDC)
J2-49
ARINC 561/568 OUT
6W SYNC (H)
USE J1-26 FOR VALID IF REQUIRED
*
Reserved for future use.
Figure 2-2 FreeFlight 2101 I/O Approach Plus J2 Pin-out
Содержание 2101 I/O PLUS
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Страница 11: ...FreeFlight 2101 I O Approach Plus GPS Navigation System SECTION I GENERAL INFORMATION ...
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Страница 25: ...FreeFlight 2101 I O Approach Plus GPS Navigation System SECTION II INSTALLATION ...
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Страница 53: ...FreeFlight 2101 I O Approach Plus GPS Navigation System SECTION III CHECKOUT ...
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Страница 83: ...FreeFlight 2101 I O Approach Plus GPS Navigation System APPENDIX B SERIAL INTERFACE SPECIFICATION ...
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Страница 103: ...FreeFlight 2101 I O Approach Plus GPS Navigation System APPENDIX C EXTERNAL INPUTS AND OUTPUTS ...
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Страница 141: ...FreeFlight 2101 I O Approach Plus GPS Navigation System APPENDIX E LOCAL GEODETIC REFERENCE DATUMS ...
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Страница 148: ...3700 Interstate 35 S Waco TX 76706 3756 USA 1 254 662 0000 ...
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Страница 150: ...3700 Interstate 35 S Waco TX 76706 3756 USA 1 254 662 0000 ...
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