Honeywell SPZ-8000 - Inertial Reference Unit Input;Output Information

Honeywell
MAINTENANCE
MANUAL
GULFSTREAMIV
Pin
Name
Remarks
JIB-G7(H) ARINC 429
\
JIB-G8(L) Output No. 1
JIB-E5(H) ARINC 429
JIB-E6(L) Output No. 2
JIB-K12(H) ARINC 429
,
JIB-K13(L) Output No. 3
JIB-F14(H) ARINC 429
JIB-F15(L) Output No. 4
JIB-G14(H) ARINC 429
JIB-G15(L) Output No. 5
JIB-H14(H) ARINC 429
JIB-H15(L) Output
!Jo. 6
>
JIB-A8(H) FMS
No. 1 ARINC 429’
JIB-A9(L) Initialization
Input
JIB-C5(H) FMS
tie. 2 ARINC 429
JIB-C6(L) Initialization
Input
JIB-A13(H) ISDUARINC 429
JIB-A14(L) Initialization
Input
JIB-K5(H) ADCNO. 1 ARINC
JIB-K6(L) 429/575 Input
J1B-J1O(H) ADCNO. 2 ARINC
JIB-J1l(L) 429/575 Input
1
JIB-J6 ARINC 575/429
ADC select
JIB-F1
Mode Discrete No. 1
JIB-F2 Mode Discrete No. 2
}
Refer to Table 2-4 for the data that is
transmitted on these identical buses.
Bit rate =
100 kbits/sec.
The IRU reads the following data from
these three ports:
label 041- set latitude
label 042- set longitude
label 043- set heading
Labels 041 and 042 are read for Nav
initialization. Label 043 is read
to set heading in attitude mode.
The following data is read from these
two ports:
label 203- pressure altitude
label 204- bare-corrected altitude
label 210- true airspeed
label 212- altitude rate
Gnd (short to JIB-A1) = ARINC 429
Open =ARINC 575 (419)
~ Alicm ~ ~
Fl: open
grid. gnd
open
F2: open
open gnd
gnd
Inertial Reference Unit
Input/Output Information
Table”2-2 (cent)
22-14-00
Page 105
Aug 15/91
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