SHADIN AVIONICS
www.shadin.com
Customer Service: (952) 836-2269
[email protected]
AIS-380 FUEL FLOW ADAPTER
P/N: 833811-01
INSTALLATION MANUAL
MANUAL P/N: M833811-01
REV C
Sales: (952) 927-6500
Страница 1: ...VIONICS www shadin com Customer Service 952 836 2269 service shadin com AIS 380 FUEL FLOW ADAPTER P N 833811 01 INSTALLATION MANUAL MANUAL P N M833811 01 REV C SHADIN AVIONICS Sales 952 927 6500 www shadin com ...
Страница 2: ...shadin com REVISION LOG Rev Date ERN DESCRIPTION 22 JAN 2016 1509 004 Baseline Release A 16 OCT 2018 1810 004 Corrected typo bit 29 on page 8 B 15 JAN 2019 1901 001 Updated table 1 and deleted Bell 412 EPI Installation C 23 JAN 2020 2001 009 Added bonding section section 5 clarification and updated company address digitally signed by ShadinCM zk 2020 01 24 11 36 45 06 00 ...
Страница 3: ...2 6 REGULATORY CERTIFICATION 9 2 7 RELIABILITY 9 2 8 ACCURACY 9 3 INSTALLATION 10 3 1 LIMITATIONS 10 3 2 INCOMPLETE SYSTEM 10 3 2 1 PERFORMANCE STANDARDS 10 3 3 MOUNTING 10 3 4 ELECTRICAL CONNECTION 10 3 4 1 TYPICAL INSTALLATION WIRING 11 3 4 2 DC TO FREQUENCY INSTALLATION EXAMPLE 12 3 4 3 GARMIN RECEIVER INSTALLATION EXAMPLE 14 3 4 4 SINE TO SQUARE WAVE CONVERTER INSTALLATION EXAMPLE 15 3 5 BONDI...
Страница 4: ...low Adapter Overview 5 Figure 2 Air Data Computer Heading ARINC 429 to RS 232 8 Figure 3 Standard Fuel Flow Configuration 11 Figure 4 DC Fuel Flow Installation with P N 630502 12 Figure 5 Garmin Receiver Installation 14 Figure 6 Sine to Square Wave Converter Installation 15 Figure 7 Field Configuration Cable 17 LIST OF TABLES Table 1 ARINC 429 Data I O 7 Table 2 DC Fuel Flow K Factors 13 Table 3 S...
Страница 5: ...ormats are configurable using the PC based configuration tool referenced later in this installation manual A basic overview is shown below in Figure 1 AIS 380 Fuel Flow Adapter P N 833811 ARINC 429 HS LS Receiver 1 ARINC 429 HS LS Receiver 2 ARINC 429 HS LS Transmitter 1 ARINC 429 HS LS Transmitter 2 SERIAL 1 RS 232 Maintenance SERIAL 2 RS 232 Air Data Fuel Flow Data Output SERIAL 4 RS 422 Fuel Fl...
Страница 6: ... Protection Not internally fused 2 3 FUNCTIONAL 2 3 1 INPUTS The AIS 380 accepts the following inputs Two Discrete Fuel Flow pulse frequency signals One RS 232 Serial Interface for Maintenance One RS 422 Serial Interface compatible to fuel flow parameters Two ARINC 429 High Speed or Low Speed signals with Air Data and Heading labels as shown in Table 1 below 2 3 2 OUTPUTS The AIS 380 provides the ...
Страница 7: ...engine and sending each engine s data in a round robin fashion SDI bits 10 9 0 1 Left 1 0 Right Transmit interval 125 msec for an effective transmit interval of 250 msec per engine The data format is as follows Bits 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 Label 347 SDI 0 0 DATA S SM Parity Data type BNR Equipment ID 029 Bit 29 0 Sign Significant bits ...
Страница 8: ...uel flow data to the GPS via the RS 232 port Channel 2 The RS 232 serial format is programmed using the Maintenance Interface The available formats are listed in Table 3 below in Section 5 1 2 RS 232 Ch 2 GPS Air Data Computer Mag Heading ARINC 429 In CH 2 ARINC 429 In CH 1 AIS 380 Fuel Flow Adapter Figure 2 Air Data Computer Heading ARINC 429 to RS 232 2 4 ENVIRONMENTAL Qualification testing was ...
Страница 9: ...O C44c INCOMPLETE SYSTEM 2 7 RELIABILITY MTBF Mean Time Between Failures Greater than 20 000 hours Mean time between failures MTBF is calculated following MIL HDBK 217F guidance as a starting point when available field or vendor data is used in place of MIL HDBK 217F predictions The AIS 380 prediction is for an environment of airborne inhabited cargo At 20 C the prediction is 36 367 hours and at 4...
Страница 10: ...d by RTCA DO 160F Environmental Conditions and Test Procedures 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 01 included in Appendix A of this manual provides connector J1 pin out information for proper wiring The AIS 380 provides data conversion for display ...
Страница 11: ...FT FF XDCR A B C RIGHT FF XDCR A B C Figure 3 Standard Fuel Flow Configuration Aircraft power 28 VDC can be connected to both pins 2 and 17 for redundancy as shown in Figure 3 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 28 V return or return can be connected to either pin 1 or pin...
Страница 12: ...9 37 Fuel Flow Interface 1 17 2 1 16 28 VDC ARINC 429 Input 1 ADC Source Heading Source ARINC 429 Input 2 ARINC 429 Output 1 Fuel Flow Interface 2 Serial RS 232 I O Port 1 Serial 1 Maintenance ARINC 429 Output 2 TX 20 Serial RS 232 Output 2 Nav Receiver 28 RTN ARINC Receiver 2 28 V POWER TX 2 A TX 2 B 26 11 AIS 380 Fuel Flow Adapter ARINC Receiver 1 DC to Frequency Converter P N 630502 L FF In R F...
Страница 13: ...ionics technical support at 952 836 2269 Table 2 DC Fuel Flow K Factors Indicator P N K factor ppg Offset Hz Beech King Air 90 380009 2 49 050 24 90 380009 5 49 050 24 101 384009 1 49 050 24 101 384153 1 3 19 647 0 PC900 6A0600 XXX 24 599 0 PC900 1A0750 XXX 19 679 0 PC900 1A0800 XXX 18 449 0 Beechjet 400A PC900 3B2000 PH 1 7 400 0 Piper Cheyenne 3265013 0601 29 470 0 3260513 1201 29 470 0 Cessna C...
Страница 14: ... Serial 1 Maintenance Serial RS 232 I O Port 2 Garmin GTN RS 232 In 4 RS 232 In 1 RS 232 In 3 RS 232 In 2 ARINC 429 Input CH 2 ARINC 429 Input CH 1 AIS 380 Fuel Flow Adapter RX 1 A RX 1 B RX 2 A RX 2 B 40 41 27 12 ADC Source Heading Source Fuel Flow Interface 1 Fuel Flow Interface 2 SIGNAL SIGNAL 24 39 PWR RTN PWR RTN 14 28 13 42 LEFT FF XDCR A B C RIGHT FF XDCR A B C TX RX 34 19 Serial RS 232 I O...
Страница 15: ...uare Wave Converter Installation 3 5 BONDING The primary bonding is achieved through metal to metal contact of the mounting feet The two mounting feet 2 4 x 3 2 inches are unpainted chemical conversion coated per MIL DTL 5541F Type 1 Class 3 Additionally the top of the four mounting holes are unpainted to a diameter of roughly 0 45 inches The aircraft s mating surface should be free of paint or an...
Страница 16: ...s 2 42 000ft See remarks 2 15 000ft Temperature Variation 5 0 Tested to Category B Humidity 6 0 Tested to Category B Operational Shock and Crash Safety 7 0 Tested to Category B Vibration 8 0 Tested to Category R B B1 U2 F F1 Explosion 9 0 Qual by Similarity to Category E See remarks 3 Waterproofness 10 0 Identified as Category X Not tested Fluids Susceptibility 11 0 Identified as Category X Not te...
Страница 17: ... Windows 7 8 10 CK833811 01 Configuration Kit for 833811 01 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 01 Web www shadin com E mail service shadin com Phone 952 927 6500 The software and the cable required for this tool are included...
Страница 18: ...f 30 SHADIN AVIONICS www shadin com Customer Service 952 836 2269 service shadin com 5 1 1 CONFIGURATION TOOL SOFTWARE INSTALLATION 1 Copy 463803 01 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 Click Next ...
Страница 19: ...ADIN AVIONICS www shadin com Customer Service 952 836 2269 service shadin com 5 Choose install location and user access to tool Default settings are shown in the picture above and click on Next 6 A Confirm Installation window will appear as shown below click Next 7 A progress bar will appear as seen below ...
Страница 20: ...1 Page 20 of 30 SHADIN AVIONICS www shadin com Customer Service 952 836 2269 service shadin com 8 After installation confirm the following message is displayed 833811 01 Fuel Flow Configuration has been successfully installed 9 Close the 833811 01 Fuel Flow Configuration Wizard dialog box ...
Страница 21: ...the Field 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 01 Fuel Flow Configuration Tool icon which points to the newly installed program 463803 01 exe Double click the icon to start up the program The following dialog box will appear 4 Select the appropriate COM Serial Port which...
Страница 22: ...VIONICS www shadin com Customer Service 952 836 2269 service shadin com 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 ...
Страница 23: ... to 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 200 and 100000 pulses per gallon for each applicable engine The K Factor can normally be found on the fuel flow transducer Note the K Factor programmed should be in pulses per gallon whereas the K Factor listed on the transducer is typically in the ab...
Страница 24: ...rmat based on the equipment that will be connected to SERIAL 2 in the planned aircraft installation The serial output formats available are given in Table 3 below Table 3 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 38...
Страница 25: ...01 Page 25 of 30 SHADIN AVIONICS www shadin com Customer Service 952 836 2269 service shadin com 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 ...
Страница 26: ...trol SC1 INSTALLATION MANUAL Revision C M833811 01 Page 26 of 30 SHADIN AVIONICS www shadin com Customer Service 952 836 2269 service shadin com 6 APPENDIX A INSTALLATION DRAWING Installation drawing D833811 01 is provided on the next page ...
Страница 27: ... INPUT OUTPUT 1 SINGLE N A 27 ARINC 429 RX2 A ARINC 429 INPUT 2 LINE A STP PIN 12 6 DISCRETE IO 3 DISCRETE INPUT OUTPUT 3 SINGLE N A 28 FF PWR RTN 1 FUEL FLOW POWER RETURN 1 STT PIN 14 24 7 SER 3 RX SERIAL 3 RECEIVE POSITIVE STP PIN 8 29 DISCRETE OUT 5 DISCRETE OUTPUT 5 SINGLE N A 8 SER 3 RX NEG SERIAL 3 RECEIVE NEGATIVE STP PIN 7 30 DISPLAY GND EXTERNAL DISPLAY SUPPLY RETURN SINGLE PIN 3 4 44 9 S...
Страница 28: ... F N REV 0Z5P5 B SIZE CAGE CODE D833811 01 P N SHEET 2 OF 2 SCALE N A SHADIN AVIONICS PROPRIETARY INFORMATION ALL RIGHTS RESERVED SEE DETAIL A 1 46 1 57 4 00 4 24 5 62 0 70 PICTORIAL VIEW PIN 1 PIN 44 DETAIL A ENLARGED 6 90 6 25 2 00 3 20 0 70 1 80 3 40 2 4X 0 190 ...
Страница 29: ... SC1 INSTALLATION MANUAL Revision C M833811 01 Page 29 of 30 SHADIN AVIONICS www shadin com Customer Service 952 836 2269 service shadin com 7 APPENDIX B INSTALL KIT PARTS LIST The install kit parts list K833811 00 is provided on the next page ...
Страница 30: ...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 ...
