M833811-00
Shadin Avionics
INSTALLATION MANUAL
AIS-380 FUEL FLOW ADAPTER
Rev: C
P/N 833811-00
Page: 7 of 20
Shadin Avionics
6831 Oxford Street
St. Louis Park, MN 55426
USA
Table 1 below defines the ARINC labels which are received at the input of the AIS-380 and the labels that are
transmitted out.
Table 1 – ARINC Data Transmission
ARINC 429 Input
ARINC 429 Output
ARINC 429 Output Bell 412 EPI
ARINC 429
Channel 1
102, 203, 201, 205, 206,
207, 210, 211, 212, 213,
234, 235, 236, 237, 312,
314, 350, 353
102, 203, 201, 205, 206, 207,
210, 211, 212, 213, 234, 235,
236, 237, 312, 314, 350, 353,
244, 347
102, 203, 201, 205, 206, 207,
210, 211, 212, 213, 234, 235,
236, 237, 312, 314, 350, 353,
351, 352
ARINC 429
Channel 2
320
320,
244, 347
320,
351, 352
Labels 244 and 347 are the labels generated by the AIS-380 and are shown in bold at the output of
Channel 1. Labels 351 and 352 shown in bold are specific to the Bell 412 EPI installation.
All of the data listed in the ARINC 429 Output column in Table 1 above is sent out on SERIAL 2 in RS-232
format.
1.6
ACCURACY
Fuel Flow conversion based on ± 10Hz of max input of 2 KHz typical accuracy is 0.1% of full scale with max
of 0.5% of full scale.
