Shadin Avionics AIS-380, Installation Manual

Page 1: ...0 FUEL FLOW ADAPTER P N 833811 00 INSTALLATION MANUAL MANUAL P N M833811 00 REV C Shadin Avionics 6831 Oxford Street St Louis Park MN 55426 USA Sales 800 328 0584 Customer Service 800 388 2849 www shadin com ...

Page 2: ... Oxford Street St Louis Park MN 55426 USA REVISION LOG REV DATE APP D ERN CHANGE 5 9 2013 RJW Baseline Release A 6 14 2013 1306 004 Sections for accuracy and incomplete system description added B 11 24 2014 1411 002 Added DC Fuel Flow Installation Application C 01 15 2019 1901 001 Updated Sections 1 2 and 1 5 Table 1 Figure 4 ...

Page 3: ...v C P N 833811 00 Page 3 of 20 Shadin Avionics 6831 Oxford Street St Louis Park MN 55426 USA Table of Contents REVISION LOG 2 1 OVERVIEW 4 2 INSTALLATION 11 3 CONFIGURATION TOOL 12 4 ENVIRONMENTAL QUALIFICATION FORM EQF 19 5 INSTALLATION DRAWINGS AND INSTALL KIT PARTS LIST 20 ...

Page 4: ...ng The AIS Fuel Flow combines this data and re transmits it on an ARINC 429 or RS 232 serial output bus The ARINC 429 speed K Factor single twin engine selection fuel density and serial output formats are configurable using the PC based configuration tool referenced later in this installation manual There is an additional RS 422 receive port for a custom application designed specifically for the B...

Page 5: ...t speed is matched when configured e g ARINC channel 1 input channel set for high speed results in ARINC channel 1 output set for high speed Fuel Flow labels 244 Total Fuel Flow and 347 Left and Right independent Fuel Flow based on SDI are generated and output at an 8 Hz rate when configured for normal fuel flow format on both ARINC 429 outputs Specific features for the Bell 412 EPI Installation F...

Page 6: ...etween failures MTBF is calculated following MIL HDBK 217 guidance as a starting point when available field or vendor data is used in place of MIL HDBK 217 predictions The AIS 380 prediction is for an environment of airborne inhabited cargo At 20 C the prediction is 36 367 hours and at 40 C it is 22 607 hours 1 4 INPUTS The AIS 380 accepts the following inputs Two Discrete Fuel Flow pulse frequenc...

Page 7: ...37 312 314 350 353 102 203 201 205 206 207 210 211 212 213 234 235 236 237 312 314 350 353 244 347 102 203 201 205 206 207 210 211 212 213 234 235 236 237 312 314 350 353 351 352 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...

Page 8: ... RTN 14 28 13 42 37 Fuel Flow Interface 1 17 2 1 16 28 VDC ARINC 429 Input 1 ADC Source optional Heading Source optional ARINC 429 Input 2 ARINC 429 Output 1 Fuel Flow Interface 2 Serial RS 232 I O Port 1 Serial 1 Maintenance RX pos RX neg 35 36 ARINC 429 Output 2 TX 20 Serial RS 232 Output 2 Nav Receiver optional 28 RTN ARINC Receiver 2 28 V POWER Serial RS 422 Receiver 4 TX 2 A TX 2 B 26 11 AIS ...

Page 9: ...In Right FF In Right FF GND Left FF In Left FF In Left FF GND Left Fuel Flow Indicator 8 15 13 6 4 5 7 12 14 2 1 3 10 9 11 Right Fuel Flow Indicator 28VDC 24 39 DC to Frequency Converter PN 630502 AIS Fuel Flow PN 833811 00 28VDC Power GND Left Freq FF Input Right Freq FF Input ARINC 429 Input 1 ARINC 429 Input 2 Maintenance Port RS 232 1 RS 232 2 2 17 1 16 40 41 27 12 34 19 20 21 28VDC GTN 750 Ai...

Page 10: ... Figure 4 Bell 412 EPI Installation Provisional wiring and interconnections to the ADIU can be found in Bell STC SR09600RC 1 7 INSTALLATION NOTES Aircraft power 28 VDC can be connected to both pins 2 and 17 for redundancy as shown above Alternatively the unit can be powered only through pin 2 or only through pin 17 The same applies to the return lines Pins 1 and 16 can both routed to the aircraft ...

Page 11: ...es for Airborne Equipment The AIS 380 is compatible with any fuel transducer whose output is a pulse frequency in the range of 0 to 13VDC and within 2Hz to 2KHz Installation Drawing D833811 00 included in Appendix A of this manual provides connector J1 pin out information for proper wiring The AIS 380 provides data conversion for display The installer must substantiate the interoperability when sh...

Page 12: ...K833811 Configuration Kit for 833811 1 MB hard disk space Desktop or Laptop PC with serial port or USB adapter if no serial port is available Intel Pentium Processor 1 6 GHz minimum 500 MB RAM minimum Contact Shadin Tech Support to obtain CK833811 Web www shadin com E mail service shadin com Phone 952 927 6500 or 800 388 2849 The software and the cable required for this tool are included in the ki...

Page 13: ...IGURATION TOOL SOFTWARE INSTALLATION 1 Copy 463803 msi and setup exe to a local folder on the PC 2 Run setup exe The following dialog box will appear 3 Follow the Setup Wizard instructions 4 After installation confirm the following message is displayed AIS 380 Fuel Flow Configuration has been successfully installed 5 Close the AIS 380 Fuel Flow Configuration Wizard dialog box ...

Page 14: ...ield Configuration Cable 2 Apply 28 VDC to the power leads of the Configuration cable which is connected to the AIS 380 3 On the PC navigate to the location of the 833811 Fuel Flow Configuration Tool icon which points to the newly installed program 463803 exe Double click the icon to start up the program The following dialog box will appear 4 Select the appropriate COM Serial Port which is connect...

Page 15: ...20 Shadin Avionics 6831 Oxford Street St Louis Park MN 55426 USA 5 Wait for the Software Version number to appear and the status indicator located next to the software version number to turn from yellow to green If the indicator remains yellow check the serial port cable connections and re run the program ...

Page 16: ...der Fuel Flow Parameters select Enabled 8 Select Use 422 Port Parameters if this is an AIS 380 Bell 412 EPI Helicopter installation per Figure 4 For all other installations leave this box unchecked 9 Select the appropriate Engine Type from the drop down list Single Engine or Twin Engine 10 Enter a Fuel Flow K Factor number between 4000 and 100000 for each applicable engine The K Factor can normall...

Page 17: ...sed on the equipment that will be connected to SERIAL 2 in the planned aircraft installation The serial output formats available are given in Table 2 below Table 2 Serial Output Formats SHADIN_Z SHADIN_G BENDIX_D_GPH BENDIX_D_PPH BENDIX_D_LPH CHELTON GENERIC_FF_GPH GENERIC_FF_LPH GENERIC_FF_PPH 13 Press the Program button Wait for the status indicator to turn from yellow to green The AIS 380 confi...

Page 18: ...P N 833811 00 Page 18 of 20 Shadin Avionics 6831 Oxford Street St Louis Park MN 55426 USA See the example below for a configuration with all fields completed 14 Turn power OFF to the AIS 380 and disconnect the configuration cable The AIS 380 is now ready for aircraft installation ...

Page 19: ...Tested to Category R B B1 U2 F F1 Explosion 9 0 Identified as Category X Not tested Waterproofness 10 0 Identified as Category X Not tested Fluids Susceptibility 11 0 Identified as Category X Not tested Sand and Dust 12 0 Identified as Category X Not tested Fungus 13 0 Identified as Category X Not tested Salt Spray 14 0 Identified as Category X Not tested Magnetic Effect 15 0 Tested to Category Z ...

Page 20: ...0 FUEL FLOW ADAPTER Rev C P N 833811 00 Page 20 of 20 Shadin Avionics 6831 Oxford Street St Louis Park MN 55426 USA 5 INSTALLATION DRAWINGS AND INSTALL KIT PARTS LIST Appendix A INSTALLATION DRAWING D833811 00 Appendix B INSTALL KIT PARTS LIST K833811 00 ...

Page 21: ......

Page 22: ......

Page 23: ...IPTION MFG MFG DESIGNATION COMMENTS Shadin Avionics Proprietary Information ALL RIGHTS RESERVED 5 232012 1 CONN HD D Sub 44 Pin Female Crimp w FC8022D2 Contacts POS ODD44S1000X 10 232507 1 CONN Backshell 25P D Sub Zinc Die Cast APH 17E 1657 25 15 239004 1 TOOL INSERT EXTRACT M81969 1 04 NWK 59K0052 20 753217 1 Thermal Label 4 x 1 ULI S 8601 25 PK1001 2 BAG 2 5 x 3 4 MIL Zip Lock 30 PK1007 1 BAG 6 ...