Advanced Panel System – Advanced Control Module Installation Manual

ACM-ECB Specifications ___________________________________________________________ 24 ACM Mounting .................................................................................................................................... 24 Component Weights ............................................................................................................................ 24 ACM-ECB Configuration Switch Settings______________________________________________ 25 DSUB Pin Crimper Tools __________________________________________________________ 29 Recommended Aircraft Power Wire Size _____________________________________________ 29 Quick Panel Post Installation Check _________________________________________________ 30 AF-6600 / AF-5000 EFIS Software Configuration (Must be done before first engine start and flight)31 Advanced-SV Network Configuration .................................................................................................... 32 Updating Network Components ................................................................................................................................... 32 Skyview HDX EFIS Software Configuration (Must be done before first engine start and flight) __ 48 ACM-EFIS RS-232 Serial Port Mapping AF-5000 ________________________________________ 57 ACM-EFIS RS-232 Serial Port Mapping Skyview ________________________________________ 58 IFR Panel ACM Fuse Sizes _________________________________________________________ 60 VFR Panel Fuse Sizes _____________________________________________________________ 61 AF-6600 / AF-5000 Panel Configuration Checklist ______________________________________ 62 IFD-540/440 Configuration when connected to AF-6600 / AF-5000 ________________________ 73 IFD-540/440 Configuration when connected to Dynon HDX or Skyview _____________________ 76 Version 8.0 Advanced ACM Panel Manual 4 GTN-650xi/750xi Configuration for AF-6600 / AF-5000 Only _____________________________ 78 GTN-650xi/750xi Configuration for Dynon HDX / Skyview _______________________________ 79 Garmin GPS-175 Configuration _____________________________________________________ 80 AF-6600 / AF-5000 EFIS......................................................................................................................... 80 Skyview EFIS ........................................................................................................................................ 80 Garmin G5 EFIS Configuration ______________________________________________________ 81 Instrument Panel System Tests _____________________________________________________ 82 RADIO and Audio Panel Tests ............................................................................................................... 82 Trim Servo Tests................................................................................................................................... 82 Panel Dimming..................................................................................................................................... 82 Aircraft Lights ...................................................................................................................................... 83 Auto Pilot Tests .................................................................................................................................... 83 ELT Tests .............................................................................................................................................. 83 D6 EFIS Tests ........................................................................................................................................ 83 Pitot Tube Tests ................................................................................................................................... 83 +12V Power Plug .................................................................................................................................. 83 Remote Component Mounting _____________________________________________________ 84 RV-7 Slider Panel .................................................................................................................................. 84 57840 Aircraft Front Harness ______________________________________________________ 85 57844 Aircraft Front Harness with PPS _______________________________________________ 86 57850 AIRCRAFT REAR HARNESS ___________________________________________________ 87 57854 AIRCRAFT REAR HARNESS AeroLED Lights ................................................................................... 88 AVEO Engineering ZIP TIP Wiring ___________________________________________________ 89 EFIS Inputs _____________________________________________________________________ 90 SV-GPS-250 GPS / SV-GPS-2020 / AFS P/N: 73102 GPS Wiring ____________________________ 91 ADAHRS SV-ADAHRS 200/201 Wiring ________________________________________________ 92 Advanced SV Network Wiring ............................................................................................................... 93 71320 SV-EMS-220 Wiring ________________________________________________________ 94 53914 SV EMS Engine Sensor Harness Diagram ..................................................................................... 95 53847 SV EMS EGT-CHT Harness Diagram ............................................................................................. 98 ACM FUSE Power Chart ___________________________________________________________ 99 ACM-ECB Electronic Circuit Breakers _______________________________________________ 100 57475 AP Servo Harness _________________________________________________________ 101 57860 Control Stick Harness with Micro Molex _______________________________________ 102 57861 Control Stick Harness Generic _______________________________________________ 103 Version 8.0 Advanced ACM Panel Manual 5 57870 Trim and Flap Servo Harness ________________________________________________ 104 57302 D10 Backup Harness with CO and TCW Battery _________________________________ 105 Aircraft Antennas _______________________________________________________________ 106 FLARM TRX-1500 Interface _______________________________________________________ 108 FLARM AT-1 Wiring _____________________________________________________________ 110 RV-14 Panel Install ______________________________________________________________ 111 RV-14 Remote Component Mounting ................................................................................................. 111 Avidyne IFD-540 Tray Mounting ......................................................................................................... 111 RV-14 EMS-220 Module Install............................................................................................................ 111 RV-14 SV-ADSB-470/472 ADS-B Module Install ................................................................................... 111 Advanced Control Module (ACM) ....................................................................................................... 115 RV-14 ADAHRS Mounting and Wiring.................................................................................................. 116 RV-14 Aircraft Front Wiring (P/N: 57842) ............................................................................................ 117 57841 RV-14 Front Harness ................................................................................................................ 118 RV-14 Airframe Harnesses (P/N: 57852) .............................................................................................. 119 57843 RV-14 Canopy Harness ............................................................................................................. 121 57851 RV-14 Aircraft Rear / Trim Harness 57476 RV-14 Servo Harness ................................................. 122 RV-14 Pitch Servo Wiring .................................................................................................................... 124 57880 RV-14 ADAHRS Fuselage Harness .............................................................................................. 125 RV-14 Right Wing Roll Servo and Trim Servo Wiring ........................................................................... 126 RV-14 Heated Pitot Tube .................................................................................................................... 127 RV-14 Optional TruTrak Autopilot Wiring ............................................................................................ 128 RV-14 Van’s Tailcone Left Wiring ........................................................................................................ 130 RV-14 Pitch Trim Wire Routing Table .................................................................................................. 131 RV-14 AFS P/N: 57481 Rear Servo Harness ......................................................................................... 132 RV-14 EMS-220 Harness Install (P/N: 53914) ...................................................................................... 133 RV-14 AFS SV-Network Wiring (P/N: 57853-AFS) ................................................................................. 134 RV-14 HDX SV-Network Wiring (P/N: 57853-HDX) ............................................................................... 135 RV-14 Control Stick Wiring (P/N: 57860) ............................................................................................. 136 RV-14 Input Wiring and Configuration (AF-5000) ................................................................................. 137 RV-14 Antenna Locations ................................................................................................................... 140 Glasair Sportsman Panel Install ___________________________________________________ 141 Sportsman Remote Component Mounting .......................................................................................... 144 P/N: 70080 ACM-ECB Mounting ................................................................................................................................. 144 Firewall Harness Routing ............................................................................................................................................ 144 P/N: 68201 Sportsman Right Side Avionics Mounting Plate Assembly ...................................................................... 145 SV-ADAHRS-200/201 .................................................................................................................................................. 148 Version 8.0 Advanced ACM Panel Manual 6 ADAHRS SV-NETWORK Wiring .................................................................................................................................... 148 Sportsman Switch Wiring ................................................................................................................... 149 Sportsman ACM-ECB Power Diagram .................................................................................................. 150 RV-10 Aerosport Panel Install _____________________________________________________ 167 RV-10 Component Mounting .............................................................................................................. 168 RV-10 Aerosport Power Diagram ....................................................................................................... 169 RV-10 SV-NET Wiring .......................................................................................................................... 170 Aerosport Duel LED Switch Wiring ...................................................................................................... 171 RV-10 Antenna Locations ................................................................................................................... 173 ACM Flap Control – AF-5000 ______________________________________________________ 174 SV Autopilot Setup ______________________________________________________________ 175 System Wiring Table ____________________________________________________________ 176 Electronic Ignitions ______________________________________________________________ 178 EMAG Air ........................................................................................................................................... 178 Lightspeed.......................................................................................................................................... 178 SureFly – Lycoming EIS ........................................................................................................................ 179 P/N: 57840-LS Dual Lightspeed with TCW Example Wiring ................................................................... 180 P/N: 57840-SF Dual SureFly with TCW Example Wiring ........................................................................ 181 P/N: Dual Lightspeed with Backup Battery Example Wiring ................................................................. 182 P/N: 53403 EMAG Wiring ................................................................................................................... 185 Harness Schematics _____________________________________________________________ 186 P/N: 57100 AF-5000 to ACM Harness .................................................................................................. 187 P/N: 57200 Skyview to ACM Harness .................................................................................................. 188 P/N: 57260 ACM AF-5000 TCW Backup Battery Harness ...................................................................... 189 P/N: 57265 ACM Skyview Backup Battery Harness P/N: 57450 ACM to AP-PANEL HARNESS ................. 190 P/N: 57500 ACM to SV-XPNDR, SV-GPS, SV-ADSB Harness ................................................................... 192 P/N: 57535 GTN650 to ACM Harness .................................................................................................. 193 P/N: 57651 PMA-450 EX/PDA-360 Audio Panel Harness ...................................................................... 194 P/N: 57540 IFD-440/540 GPS Navigator Harness ................................................................................. 195 Trouble Shooting ADS-b Data on an Avidyne IFD ....................................................................................................... 196 P/N: 57315 Garmin G5 Harness .......................................................................................................... 198 P/N: 57700 SV-COM to ACM Harness .................................................................................................. 199 P/N: 57726 GTR-200 to ACM Audio Panel Harness .............................................................................. 200 P/N: 57727 GTR-200 Radio Only to ACM Harness ................................................................................ 201 P/N: 57536 Garmin GPS-175 Harness .................................................................................................. 202 P/N: 57537 Garmin GNC-355 Harness ................................................................................................. 203 Version 8.0 Advanced ACM Panel Manual 7 P/N: 57690 ACM to Dynon T25/T8 (Trig) Com Radio with COM Panel .................................................. 204 P/N: 57692 ACM COM 2 to Dynon T25/T8 (Trig) Remote Com Radio .................................................... 205 P/N: 57693 ACM COM 1 to Dynon T25/T8 (Trig) Remote Com Radio .................................................... 206 P/N: 57305 Back AF-5600, G5, CO, Ethernet Harness .......................................................................... 207 P/N: 74263-ACM Aithre Shield EX 3.0 S Wiring (RS-232 Serial) ............................................................. 208 P/N: 11080-ACM Aithre Altus Oxygen Wiring (RS-232 Serial) ............................................................... 208 B & C Alternators ............................................................................................................................... 210 P/N: 57847 Aircraft Front Harness Dual Alternators ............................................................................ 211 Upgrading from an ACM-FUSE to ACM-ECB – AF-5000 _________________________________ 212 Changing a SV-COM Radio _______________________________________________________ 213 AF-5000 EFIS Messages __________________________________________________________ 214 ACM Switch Wiring Troubleshooting _______________________________________________ 220 Registration Information _________________________________________________________ 224 Version 8.0 Advanced ACM Panel Manual 8 MANUAL REVISION HISTORY REVISION DATE DESCRIPTION 1.0 12/31/2014 Original Release 2.0 4/9/2015 Updates 2.4 11/5/2015 IFD540 Configuration, Crimpers 2.5 12/23/2015 Updates 2.7 10/11/2016 SV EMS 3.0 12/16/2016 RV-14 Data, ACM Torque 4.0 9/1/2017 ACM-ECB 4.4 1/2/2018 Updated RV-14 Canopy and Harness Drawings 4.5 2/21/2018 Updated test procedure and CHT setup 4.6 2/23/2018 Updated IFR/VFR Testing 4.7 3/8/2018 Added Serial Port to plug chart 4.8 3/12/2018 Updated Install Checklist and Flap Testing 5.0 3/23/2018 Updated for ACM-ECB 5.1 4/6/2018 Added ACM-ECB Switch Settings 5.2 7/3/2018 Added Harness Drawing Section 5.3 2/1/2018 Added Panel Switch Operation Section 6.0 2/8/2018 Added ACM-ECB and Switch Operation, Harness Drawings 6.1 2/18/2018 Updated RV-14 schematics, Added Sportsman Drawings , 6.2 9/25/2018 Updated Sportsman and Front Harness Drawings 6.5 3/14/20 Sportsman Wiring 7.0 3/30/22 Updated IFD Settings, Electronic Ignitions 7.2 1/2/2023 Added G5 Backup Settings 7.3 2/9/2023 Changed GTN and IFD ARINC OUT to High Speed 7.4 2/15/2023 Added IFD ADS-B Troubleshooting 7.5 6/12/2023 Added Schematics 7.6 9/2/2023 Changed Rear Harness drawings for Remote Radio 8.0 11/3/2023 IFD and GTN COM Radio Tuning, updated switch settings Version 8.0 Advanced ACM Panel Manual 9 Overview The Advanced Quick Panel system is based on our Advanced Control Module “ACM”. The ACM is available in two different versions, fused or electronic circuit breaker. The fused version uses lighted ATO style fuses for circuit protection. The electronic circuit breaker “ECB” version has internal circuit current monitoring and will shut off a circuit if the current is too high. With the ACM-ECB you can monitor the current of each circuit and reset any tripped circuits from the EFIS. The ACM is the main power distribution center for the aircrafts electrical system. The avionics, headsets, aircraft lights, autopilot servos, trim servos, flap motor, control sticks and panel switches all get connected to the ACM. Using the ACM with its plug and play features vastly simplifies an aircraft’s wiring and troubleshooting. The ACM also makes future upgrades extremely easy. Want to add an IFR Navigator in the future? No problem, just plug it into the ACM NAV-COM and GPS NAVIGATOR plugs. The complicated and time consuming (Audio Panel, GPS RS-232 data, NAV ARINC data and GPS ARINC) wiring is already done. The ACM must never be used to power anything critical to Engine operation, including: Electronic Ignition, Electronic Fuel Injection or high pressure main electric fuel pumps. ACM module with Electronic Circuit Breakers ACM module with Fuses ACM Features • 27 dedicated channels of circuit protection including: PFD, MFD, BACKUP EFIS, TRANSPONDER- ADSB, COM 1, NAV 1, COM 2, NAV 2, GPS NAVIGATOR, AUDIO PANEL, CABIN LIGHTS, DEFROST, ALTERNATOR, AUX POWER, STARTER, BOOST PUMP, PITOT HEAT, LEFT LANDING LIGHT, RIGHT LANDING LIGHT, NAV LIGHTS, STROBE LIGHTS, TRIM MOTORS, AP SERVOS, FLAP MOTOR. ACM-ECB ONLY: BACKUP ALTERNATOR, LIGHTS, SPARE POWER CIRCUIT, CABIN LIGHT SWITCH • Built in SV-ARINC module • Multi Step Flap Positioning System • Wig-Wag Lighting Circuit (airspeed controlled) • Panel Dimmer • Trim Controller (must have SV-AP-PANEL) • SV Network Hub (4 Port + AP Servos) • Panel Switch Interface with support for switch lights • Control Stick Interface • Alternator Field overvoltage protection, shuts off the alternator field at 16 volts Version 8.0 Advanced ACM Panel Manual 10 Advanced Panel Customer Order Form ACM Panel Switch Operation The ACM can be used with either our standard switch modules using a 25 pin ribbon cable or custom switches wired to the ACM PANEL SWITCHES DSUB-25 pin connector. The operation of the panel switches should be the same for either a Skyview or AF-5000 equipped panel. CAUTION: Do not fly the aircraft until you review and completely understand the proper use of each panel switch. MASTER Turns on the Aircraft Master relay providing power to the ACM Main Power Input Red Post, this will turn on the EFIS PFD. This switch does not connect to an ACM Input. ALT Signal to ACM to turn on the Alternator Field Power. You should never turn ON the ALT switch with the MASTER switch OFF AVIONICS Signal to ACM to turn on the Avionics Bus in the ACM (EFIS MFD, Com1, Com2, Nav1, Nav2, Transponder, ADSB, Audio Panel) AUTOPILOT Signal to ACM to turn on the Autopilot Servo power. This switch must be ON before the Master Switch is turned on. We recommend that this switch be left in the ON position and only turned off if you need to turn OFF power to the Autopilot Servos. BOOST PUMP Signal to ACM to turn on the Electric Boost Pump STROBE / Signal to ACM to turn on the STOBE and NAV Lights NAV Signal to ACM to turn on the NAV Lights only, No Strobe. This is normally used when flying in the clouds. LAND LT / Signal to ACM to turn on the Left and Right Landing Lights PULSE Signal to ACM to alternate the Left and Right Landing Lights “wig-wag mode” when above the configured airspeed. The pulse airspeed is set in the SET > CAL > 21. Electrical Configuration menu. PITOT Signal to ACM to turn on the Pitot Heat DEFROST Signal to ACM to turn on the Defrost fans FLAPS Optional panel switch to run the flaps up and down. Many installations will only have a flap switch on the control stick. Version 8.0 Advanced ACM Panel Manual 11 ACM-ECB Electronic Circuit Breaker Operation The ACM-ECB is a solid-state system that replaces traditional buss bars, thermal circuit breakers, fuses and mechanical relays. The electronic circuit breaker is a solid-state circuit that monitors and reports the current for each circuit to an attached EFIS. If the current in the circuit exceeds the trip setting the ACM-ECB will turn off the circuit and report it on the EFIS screen. The tripped ECB can then be reset from the EFIS > ELECTRICAL menu. The current tripped state is preserved over a Master Relay power cycle for all channels other than the PFD EFIS circuit. All the circuits can be monitored from the EFIS Electrical page giving you far more information than a traditional circuit breaker or fuse. CAUTION: Do not fly the aircraft until you review and completely understand the proper use of the EFIS Electrical Circuit Breaker Page. The red line indicates the trip level of the ACM- ECB Channel Version 8.0 Advanced ACM Panel Manual 12 AF-6600 / AF-5000 Electrical Circuit Breaker Page You access the Circuit Breaker electrical page by pressing the [CHECK] button followed by the [ELEC] button. Total ACM-ECB Current AMPs being used ACM-ECB Input Voltage ACM-ECB Status Landing Light Mode A Green Bar indicates the circuit is turned ON. The current Circuit Amperage being used is displayed to the right of the circuit name. A Red Bar indicates the circuit is Tripped and turned OFF. The bottom of the page displays the circuit information for the highlighted circuit: • Circuit Name • Rating in AMPS • Controlling Switch • Status Highlighted Circuit Control Buttons [ SET ] Lets you change the circuit breaker size [ ON ] Turn ON the Circuit, Ignores the switch position [ OFF ] Trip the Circuit, must be RESET before you can turn it back ON [ RESET ] Reset the Circuit Breaker Version 8.0 Advanced ACM Panel Manual 13 The FLAPS circuit also has buttons that enable you to move the flaps UP and DOWN independent of the control stick or panel FLAP switch. You should verify proper flap direction from this page before programming the flap positions. If the flaps are backwards you can reverse the polarity from the EFIS CAL Flap Menu. If the panel or stick flap control buttons are backwards you will need to swap the button wiring. [ DOWN ] Move Flaps down [ UP ] Move Flaps up Version 8.0 Advanced ACM Panel Manual 14 Dynon Skyview Electrical Page Total ACM-ECB Current AMPs being used ACM-ECB Input Voltage A Green Bar indicates the circuit is turned ON. The current Circuit Amperage being used is displayed to the right of the circuit name. A Yellow Bar indicates the circuit is Tripped and turned OFF. To Reset the Tripped circuit, use the right knob cursor to select and then press the knob. Version 8.0 Advanced ACM Panel Manual 15 In Flight Emergencies Tripped Circuit Breaker Advanced Flight Systems does not recommend RESET-ing a circuit breaker in flight. If a circuit breaker trips you should trouble shoot the overcurrent problem after landing. Electrical Smoke Turn OFF the ALT and Master switches (Red Switches), Turn OFF all the remaining panel switches. The PFD and MFD EFIS along with the attached Dynon GPS should continue to operate from the backup battery. When the electrical smoke stops you can if necessary, turn ON the MASTER Switch followed by individual critical circuits from the EFIS Electrical Page. If you detect smoke after turning on a circuit, you should immediately turn it back OFF Failed Switch On an AF-6600/AF-5000 EFIS you can turn on individual circuits from the EFIS Electrical Page, Skyview does not have this capability Version 8.0 Advanced ACM Panel Manual 16 ACM Aircraft Wiring Overview Version 8.0 Advanced ACM Panel Manual 17 Advanced Skyview Network Planning Most of the AFS - Dynon components communicate using our proprietary SV-Network. The SV-Network provides a primary and backup +8 Volt power source and a primary (A) and backup (B) two wire network for the remote devices. The SV-Network is designed to use 9 pin DSUB connectors and a special 9 conductor cable. The AFS-Dynon components all use a 9 Pin DSUB connector with male pins. The SV-NET harnesses all use a 9 pin DSUB connector with female pins. The SV-Network is designed to be a parallel network that does not require any special terminations. As long as all components are connected together in a single network they should communicate. Some of the Dynon components have two SV-Network connectors so you can continue the network connection to the next device. You can use multiple Dynon 5 port hubs connected if you need more ports. SV-NET CABLE • The following devices should be connected to the SV-Network using the standard SV-NET cables: AF- 6600, AF-5000 , SV-ADAHRS-200, SV-ADAHRS-221, SV-AP-PANEL, SV-KNOB-PANEL, ACM-ECB, SV-COM-RADIO, SV-ARINC-429 • The SV-EMS-220 or SV-EMS-221 require a special SV-NET cable when using an AF-6600 or AF-5000 with a jumper on the SV-EMS end of the cable to power the fuel flow transducer. NOTE: When using a Dynon HDX or Skyview EFIS you must use a standard SV-NET cable without the EMS Jumper wire. Version 8.0 Advanced ACM Panel Manual 18 ACM Panel Switch Wiring & Logic Version 8.0 Advanced ACM Panel Manual 19 AFS STANDARD SWITCH WIRING COLORS & ACM PIN Item Color ACM Switch Panel Pin Alternate Use PWM Dimmer Red 6,14 Ground Black 1,5,18,25 Taxi Light Orange Grey 19 Tank Transfer Left Boost Pump Brown 7 Nav Light Green 20 Strobe Light Purple Gray 8 Landing Light Blue White 21 Pulse Light Blue Green 9 Landing Light-Single Switch Pitot Heat Orange White 22 Defrost Fan Orange Green 10 Tank Transfer Right Flaps Up Yellow 11 Flaps Down Yellow White 23 Autopilot Blue 2 Avionics Purple 3 Alternator 1 Orange 15 Alternator 2 White 4 Cabin Lights Gray 24 Version 8.0 Advanced ACM Panel Manual 20 ACM Toggle Switch Wiring Version 8.0 Advanced ACM Panel Manual 21 ACM Power Diagram & Logic Version 8.0 Advanced ACM Panel Manual 22 Getting Started The following is a general recommendation on the steps required to install the Advanced Quick Panel: • Disconnect the Aircraft Battery • Remove the old panel from the aircraft (if upgrading). Label each wire as you disconnect them from the old panel switches and components. • Mark all remote component locations and drill mounting holes using the information from the Remote Component Mounting section of this manual or supplied layout drawings. • Cut any required clearance holes in the sub-panel. • Remove EFIS screens from the new Panel for sub panel access. You will need to press the release buttons on the side of the USB data connector to get the cable to release • Test fit new panel and trim panel ribs for clearance if required. • Configure the ACM-ECB Jumpers on the back of the unit • Mount the ACM Module. • Connect the #8 main power wire from the battery master relay to the red power lug on the ACM. The main power wire should have a ¼” (0.250”) ring terminal with a molded plastic cover. Torque to 30 in-lbs • Connect the #10 airframe ground wire from the airframe ground to the black power lug on the ACM. The ACM main ground wire should have a #10 ring terminal with a molded plastic cover. Torque to 24 in-lbs • Connect your existing aircraft Landing Lights, Nav Lights, Strobe Lights, Pitot Heat, and ELT to the supplied P/N: 57850 Aircraft Rear Harness ACM connector. You must limit the power on each D-Sub pin to less than 5 amps by using multiple pins at the connector. The recommended procedure is to use 20ga wire for each pin and then use a Solder Sleeve to connect the multiple wires to the larger gage wire going to the device. Version 8.0 Advanced ACM Panel Manual 23 • Connect your existing aircraft Fuel Pump, Alternator, and Starter Switch to the supplied P/N: 57840 Aircraft Front Harness ACM connector. • Connect your existing aircraft Control Stick switches to the supplied P/N: 57860 Aircraft Control Stick ACM connector. • Connect your existing aircraft flap and trim motor wiring to the supplied P/N: 57870 Flap and Trim motor ACM connector. • Mount the SV-200 and SV-201 ADAHRS units in the aircraft using the instructions from the AF-5000 manual. • Mount the OAT sensor to the bottom of the wing. Wire the OAT sensor to the ADAHRS • Plump Pitot,Static and AOA to the mounted ADAHRS • Wire the ADAHRS to the spare SV Network DSUB-9 connector on the ACM module • Wire the Autopilot servos to the ACM AP Servo connector • Mount the remote components to the sub panel. • Mount the AF-GPS module and connect to the ACM Transponder-GPS-ADSB harness • Connect aircraft Antennas to the remote radios (Transponder, Com, ADS-B in, …) • Install the Engine Sensors • Connect the Engine Sensors to the EMS and CHT/EGT Harness. The Engine Harnesses should route to the Left PFD EFIS display in the panel. BE sure to leave service loop of cable to make installing the EFIS PFD easier. • Mount the Panel using the supplied mounting screws. • Connect the aircraft Master relay to the screw terminals on the back of the Master Switch PCB board. • Verify that you have protection diodes installed in your master and starter relay. • Wire Aircraft Magneto P-Leads to the Key Switch. • Carefully connect and route all the supplied panel harnesses to the ACM module. • Double check that all ACM harnesses are connected to the correct DSUB connector. • Install the EFIS PFD connecting the EFIS Main Connector, EFIS AUX connector, Ethernet, and USB data port wire. • Install the EFIS MFD and connectors • Connect the Aircraft Battery, verify that it is charged • Turn on the Autopilot Panel Power Switch (should always be on before EFIS power up) • Turn on the Panel Master Switch and verify that the EFIS PFD powers up • Turn on the Panel Avionics Switch and verify that the EFIS MFD and Radios power up. Version 8.0 Advanced ACM Panel Manual 24 ACM-ECB Specifications The ACM should be mounted on the sub panel behind the instrument panel. The Fused and Electronic Circuit Breaker versions are the same size and mounting. The ACM module should be mounted to the sub panel using four 10-32 screws and nut plates. ACM Mounting Do not over-torque the power terminal nuts, they are soft copper and will break if over-torqued. Red Main Power Terminal Nut Torque: 28 in-lbs Black Main Ground Terminal Nut Torque: 19 in-lbs Component Weights ACM-ECB Module 2 Lbs 3 oz Master Switch Module 5 oz Lower Switch Module 7 oz Version 8.0 Advanced ACM Panel Manual 25 ACM-ECB Configuration Switch Settings The Electronic Circuit Breaker version of the ACM has configuration switches on the back of the unit must be set for proper RS-232 serial port operation. The switch settings control how the EFIS PFD and MFD serial ports are routed to the attached devices. On a dual (PFD/MFD) EFIS screen AF-5000 system you will have a total of 10 serial ports to control attached devices. On a Skyview system both the PFD and MFD serial ports must be tied together so you end up with only 5 serial ports. Dual AF-5000/6600 Settings Single AFS EFIS Settings Skyview Settings Version 8.0 Advanced ACM Panel Manual 26 Dual EFIS AF-5000 Settings SW1 >> CLOSED (ON) Grey is Switch Position ACM RX< PFD 0 TX MFD 0 TX >BACKUP EFIS RX ACM TX> PFD 0 RX MFD 0 RX <BACKUP EFIS TX Spare spare NOT SUPPORTED ARINC SP2 TX GPS NAV RX >GPS Nav Fuel Flow PFD FUEL FLOW> PFD 4 TX GPS NAV RX >GPS Nav Fuel Flow PFD 4 TX MFD 4 TX >DYNON GPS RX PFD AVTN data< PFD 4 RX GPS NAV TX <GPS Nav AVTN DATA PFD 4 RX MFD 4 RX <Dynon GPS TX SW2 >> CLOSED (ON) Grey is Switch Position EFIS AUDIO L AUDIO PANEL ACM TX> PFD 1 TX MFD 1 TX >ELT/COM2 TUNE RX PFD 1 RX MFD 1 RX < COM2 TUNE TX SPARE SPARE XPNDR RX< PFD 2 TX MFD 2 TX >CO DETECT RX XPNDR TX> PFD 2 RX MFD 2 RX <CO DETECT TX IFD RADIO TUNE RX PFD 3 TX MFD 3 TX >ADSB RX IFD RADIO TUNE TX PFD 3 RX MFD 3 RX <ADSB TX Version 8.0 Advanced ACM Panel Manual 27 Single EFIS AF-5000 Settings SW1 >> CLOSED (ON) Grey is Switch Position ACM RX< PFD 0 TX MFD 0 TX >BACKUP EFIS RX ACM TX> PFD 0 RX MFD 0 RX <BACKUP EFIS TX Spare spare NOT SUPPORTED ARINC SP2 TX GPS NAV RX >GPS Nav Fuel Flow PFD FUEL FLOW> PFD 4 TX GPS NAV RX >GPS Nav Fuel Flow PFD 4 TX MFD 4 TX >DYNON GPS RX PFD AVTN data< PFD 4 RX GPS NAV TX <GPS Nav AVTN DATA PFD 4 RX MFD 4 RX <Dynon GPS TX SW2 >> CLOSED (ON) EFIS AUDIO L AUDIO PANEL AUDIO P TX> PFD 1 TX MFD 1 TX >ELT/COM2 TUNE RX AUDIO P RX< PFD 1 RX MFD 1 RX < COM2 TUNE TX SPARE SPARE XPNDR RX< PFD 2 TX MFD 2 TX >CO DETECT RX XPNDR TX> PFD 2 RX MFD 2 RX <CO DETECT TX IFD RADIO TUNE RX PFD 3 TX MFD 3 TX >ADSB RX IFD RADIO TUNE TX PFD 3 RX MFD 3 RX <ADSB TX Version 8.0 Advanced ACM Panel Manual 28 SKYVIEW EFIS Settings SW1 >> CLOSED (ON) Grey is Switch Position ACM RX< PFD 0 TX MFD 0 TX >BACKUP EFIS RX ACM TX> PFD 0 RX MFD 0 RX <BACKUP EFIS TX Spare spare NOT SUPPORTED ARINC SP2 TX GPS NAV RX >GPS Nav Fuel Flow PFD FUEL FLOW> PFD 4 TX GPS NAV RX >GPS Nav Fuel Flow PFD 4 TX MFD 4 TX >DYNON GPS RX PFD AVTN data< PFD 4 RX GPS NAV TX <GPS Nav AVTN DATA PFD 4 RX MFD 4 RX <Dynon GPS TX SW2 >> CLOSED EFIS AUDIO L AUDIO PANEL AUDIO P TX> PFD 1 TX MFD 1 TX >ELT/COM2 TUNE RX AUDIO P RX< PFD 1 RX MFD 1 RX < COM2 TUNE TX SPARE SPARE XPNDR RX< PFD 2 TX MFD 2 TX >CO DETECT RX XPNDR TX> PFD 2 RX MFD 2 RX <CO DETECT TX IFD RADIO TUNE RX PFD 3 TX MFD 3 TX >ADSB RX IFD RADIO TUNE TX PFD 3 RX MFD 3 RX <ADSB TX Version 8.0 Advanced ACM Panel Manual 29 DSUB Pin Crimper Tools Daniels Mil Spec Crimper AFM8 Part Number: M22520/2-01 AFM8 Positioner for Standard D-Sub Connectors DMC Part Number: K13-1 Less expensive crimpers are available from a number of sources. Crimper, D-Sub, Closed Barrel Contacts, 4-Way Indent AWG 26-20 Recommended Aircraft Power Wire Size Circuit Amperage Use wire size (AWG) 5A 20 10A 18 15A 14 RS-232/ARINC Data signals 22 Version 8.0 Advanced ACM Panel Manual 30 Quick Panel Post Installation Check CAUTION: Do not fly the aircraft until the following check list has been completed. Never Power the system with an automotive battery charger and the aircraft battery disconnected. Before Power is applied for the First Time o Verify ACM-ECB Configuration Switch Settings o Aircraft ground is properly connected to the ACM Module BLACK Terminal Verify relay protection diodes are installed on all large aircraft relays (Master, Starter, Avionics...etc) o Pitot/Static and AOA plumbing is secured to the correct ports on the ADAHRS o All Component Harnesses have been properly connected to the correct ports on the ACM module. o Verify the Ethernet cable is connected to all EFIS screens Applying Power for the First Time o The BLACK Autopilot switch controls power to the autopilot servos. The Autopilot switch should be ON before powering up the EFIS screens. o The RED Master Switch controls power to the Pilot PFD EFIS screen. o The BLACK Avionics switch controls power to the MFD EFIS and all radios Version 8.0 Advanced ACM Panel Manual 31 AF-6600 / AF-5000 EFIS Software Configuration (Must be done before first engine start and flight) Make sure you have the Ethernet cable connected between EFIS screens. All the AFS EFIS configuration and setup is done from the Instrument Calibration menu. From the normal EFIS run menu you press [SET] -> [CAL] and Hold for 2 seconds to enter the Instrument Calibration mode. A list of menu pages and instruments will appear. Use the lower right knob to scroll through the list. There are multiple pages of instruments. To select an item press the lower knob in while the cursor is on the desired menu item. To exit the Instrument Calibration menu or a subpage press the [BACK] button to return to the previous page. Select Advanced SV Network from the Instrument Calibration Menu on the Pilot side PFD EFIS Version 8.0 Advanced ACM Panel Manual 32 Advanced-SV Network Configuration The first thing you should do after powering up the system for the first time is SCAN for all the components that are connected to the Dynon Advanced SV Network. Press SCAN You will need to do a new SCAN anytime a different or new component is connected to the SV Network. Updating Network Components After you SCAN for components you should get a list of all the Dynon components that are connected to the SV Network. If any of the components have old software you will need to press the UPDT button to update the software on all network devices. Once the new software is loaded on the network devices you will be instructed to power down the system. Once all the EFIS screens are shut down you can turn on power to the systems and verify that all Items are ready (red text gone) and the Chanel A and B lanes are green. If you have a red A or B lane you need to check the network wiring. Need to press UPDT All Components Ready Version 8.0 Advanced ACM Panel Manual 33 • Verify that both EFIS screens are getting ADAHRS and Engine Data. Remote Transponder Remote Audio Panel Airspeed should show - - - The only red X should be over the Autopilot Menu If you have an Avidyne IFD it should power up on the warning test page and the EFIS should show a half left CDI and Waypoint ID of AVIDN Manifold Pressure should display • Aircraft Info Menu settings ➢ Weight & Balance – Select Aircraft Model ➢ Engine Type – Select Engine ➢ Tail Number – Enter Aircraft Tail Number ➢ Mode S Code – For N Number registered aircraft the EFIS will calculate, you will need to enter the Mode S code for non N number aircraft. Version 8.0 Advanced ACM Panel Manual 34 • Configure and Test the Flaps Flap Buttons a. Verify that the flaps run in the correct direction using the Flaps Up and Down Buttons on the CHECK > ELECTRICAL Page. If they are backwards swap the motor leads or use the Reverse Polarity setting in the CAL > FLAPS menu. b. Verify that the flaps run in the correct direction using the panel mounted flap switch or Stick Grip buttons. If they are backwards you MUST Swap the wires to the flap switch or buttons. c. Verify that the Flap position value changes in the CAL > Flaps menu when you move the flaps. d. Program the Flap positions in the CAL > Flaps menu e. Verify the flaps stop at the correct locations. If the flaps don’t stop at the correct locations recheck the flap direction using the CHECK > ELEC > FLAPS on screen buttons. • Calibrate Trim Positions ➢ FULL UP ➢ CENTER ➢ FULL DOWN • Perform Auto Trim Test Version 8.0 Advanced ACM Panel Manual 35 • Calibrate Autopilot servos ➢ With the EFIS screens shut down center the Aileron and Elevator control surfaces. ➢ Make sure the panel mounted AUTO PILOT power switch is in the ON position. ➢ Turn on the aircraft Master Switch and Avionics Switch. ➢ Select SET > CAL > 11. Autopilot STEP 1 of 7 ➢ Select 4. Servo Calibration and verify that the SERVO POSITION values change when you move the controls. ➢ Press START STEP 2 of 7 ➢ Press the Autopilot Disconnect Switch (CWS) Normally a button on the stick. STEP 3 of 7 ➢ Move the control stick to the full pitch down and full left position. ➢ Press NEXT Version 8.0 Advanced ACM Panel Manual 36 STEP 4 of 7 ➢ Move the control stick to the full pitch down and full right position ➢ Press NEXT STEP 5 of 7 ➢ Move the control stick to the full pitch up and full right position ➢ Press NEXT STEP 6 of 7 ➢ Move the control stick to the full pitch up and full left position • Press NEXT Version 8.0 Advanced ACM Panel Manual 37 If you have a Capstan or RV-10 Pitch Servo you will get a WARNING about servo traveling more than 120 degrees. ➢ Press YES if you have an RV-10 or Capstan Servo ➢ Press NO if you only have Servo with an arm. If the Pitch and Roll Servos calibrated correctly you should get a SUCCESS message. ➢ Press SAVE to save the Servo Calibration Version 8.0 Advanced ACM Panel Manual 38 • Autopilot Servo Test Procedure ➢ Make sure the control stick is free to move in the full range of motion. ➢ Select 5. Servo Test ➢ Press START ➢ The Autopilot will move the controls 80% of travel in all directions and should complete the test with a SUCCESS message. ➢ Press DONE Version 8.0 Advanced ACM Panel Manual 39 • Configure Airspeed Settings ➢ Vne Source ➢ V Speeds ➢ Performance Settings • Verify that the Engine parameters are correct on both EFIS screens. Configure the engine sensor types and range markings for your engine. (CHT – J type, EGT K-type, Oil Pressure, Fuel Pressure, …._ ➢ The RPM Gauge needs to be configured so it will display the correct RPM: Pulses Per 2 Revolutions: The system needs to know how many pulses the RPM input will see in two propeller rotations. The following data should help select the correct number to use. Standard RPM sensor with Slick Mag 4 Cylinders: Pulses = 2 Standard RPM sensor with Slick Mag 6 Cylinders: Pulses = 3 Electronic Ignition 4 Cylinders: Pulses = 4 Electronic Ignition 6 Cylinders: Pulses = 6 The EFIS lets you select a different Pulses Per 2 Revolutions for each ignition. Version 8.0 Advanced ACM Panel Manual 40 • Verify that all transponder settings are correct in both EFIS screens, including aircraft N Number ➢ Transponder Type SV-XPNDR-26x ➢ VFR Code North America 1200 ➢ Tail Number Aircraft N Number in the USA ➢ Mode S Code Automatically set for N Number registered aircraft ➢ Length (Meters) Aircraft Length for ADS-b ➢ Width (Meters) Aircraft Width for ADS-b ➢ Max Cruise (KTS) Max ADS-B cruise speed range ➢ ALT/GND Switch Controls ground / flight mode - set to AIRDATA ➢ TIS Service Controls Transponder TIS Traffic - set to ON ➢ ADS-B In Type Set to 1090ES & UAT for Dynon 472 ➢ Input Type Transponder ADS-B GPS source The only ADS-B approved options are: -Dynon GPS-2020 AF-GPS-2020 -Avidyne IFD (410,440, 540, 550) AVIDYNE (AVI) -Garmin(GTN650, GTN750, GPS175) GARMIN ADSB+ ➢ Lateral Offset (Meters) Antenna Lateral Offset ➢ Linear Offset (Meters) Antenna Linear Offset Version 8.0 Advanced ACM Panel Manual 41 • Calibrate and verify the Fuel Tank sensors. ➢ Select Instrument ON or OFF All the unused fuel tank gauges should be configured to OFF ➢ Select Audio Alarms ON ➢ Select Tank Units (Gallons or Liters) ➢ Set Tank Size ➢ Set Yellow Low value ➢ Set Red Low value ➢ Select tank sending unit type (Float or Capacitance) ➢ Verify correct SV-EMS pin is selected. ➢ Calibrate Fuel Tank using the instructions on the following pages. Version 8.0 Advanced ACM Panel Manual 42 The AF-6600 / AF-5000 EFIS stores two sets of calibration numbers for each tank. It uses the ground calibration numbers when the Airspeed is less than 30kts. The flight calibration numbers are used when the airspeed is greater than 30kts. This feature enables the fuel gauges to read correct on the ground for a tail-wheel equipped airplane. If the aircraft does not have a tail-wheel set the ground and flight data to the same calibration number. It is important to understand that fuel level measurements are subject to the physical limitations of the sensor. Depending on your fuel tank and sensor geometry, there may be some immeasurable fuel at one or both ends of the fuel level sensors’ range. The end result is that you may experience fuel readings at “full” that are numerically less than the physical capacity of the tanks, and in this case you may also see no apparent change in fuel level readings when the sensor is maxed out on the full side. Similarly, on the empty side, you may see a zero quantity indication before the tank is truly empty if the sensor has reached the bottom of its travel or measuring capability when the tank still in fact has fuel in it. Most fuel tank sensors are mounted in the root of the wing. If your wing has dihedral, it is common for the fuel tank sensor to stop reading the fuel level at around 2/3 of a tank. Version 8.0 Advanced ACM Panel Manual 43 Steps To Calibrate a Fuel Tank: 1. Select Instrument Calibration mode on the Pilot PFD EFIS, verify that all EFIS screens are powered on in the aircraft. Use the lower knob to scroll to Tank 1 (Left Main), Tank 2 (Right Main), Tank 3 Left Aux, or Tank 4 Right Aux. 2. Verify the Tank is Empty. 3. Enter the max size of the Tank in the Tank Size field. 4. Set the Audio On/Off Setting. If this is set to ON, an Audio warning will sound if the fuel level is below the Red Low At setting. 5. Set the Instrument On/Off Setting. If this is set to ON the tank will be displayed. 6. Enter the number of calibration points; it must have at least two points. Four points could be used (zero, ¼, ½, ¾, Full) or one point for every 2 gallons. Every calibration point must be different from the previous value until the tank sensor cannot detect a change in the fuel level. Tank sensor values must never reverse direction. 7. Use the lower knob to scroll down to the tank calibration data. The calibration data is displayed in columns, one for ground and one for flight. Use the lower knob to switch between ground and flight data columns. The current ADVAL (digital value of the transducer) reading for the tank is displayed at the top of the table. Version 8.0 Advanced ACM Panel Manual 44 8. Starting at 0 Gallons press the [COPY] button or use the knob to record the current ADVAL to the correct fuel amount and attitude (ground or flight). 9. Add fuel (at increments decided on) and then record the new ADVAL by pressing [COPY] 10. Fill and record a reading for each attitude (ground and flight). If it is a tail wheel aircraft, the best way to do this is to record the ground data then lift the tail and record the flight data after the fuel reading has settled. Repeat this for each increment until the tank is full. 11. Press the [SAVE] button to save the data to permanent memory and [BACK] to exit Tank Calibration. 12. After completing Tank 1, move on to Tank 2 and follow the same procedure. If Aux Tanks are present, follow this procedure for Tank 3 & 4. 13. IF THE AIRCRAFT DOES NOT HAVE AUX TANKS, TURN TANKS 3 & 4 OFF! CAUTION: Do not turn off power before pressing the save button and exiting the calibration menu. Calibration Tips: When lifting the tail you should set it on something, so the level you lift it to will be consistent. You should also wait until the reading stops changing before setting it. Fuel tank sensors are not accurate when the tank is near full. Once you notice the reading not changing much or not corresponding with the rest of the readings during calibration the last few entries in the fuel calibration data should be set to the same value. If the tanks do not consistently show full, lower the digital value for the tank full data. The fuel gauge will only show the digital fuel amount for the highest reading that the float changed with a plus sign indicating that the correct fuel amount is not known but is over the last reading. The analog gauge will show full for the last changing reading. It is normal for an 18-gallon tank to show 16+ when it is full. This indicates that the float stopped changing at 16 gallons and this is the highest fuel reading that can be detected by the float in the tank. Valid Tank calibration values. Values do not reverse direction and the sensor stopped detecting fuel changes at 25 gallons. Version 8.0 Advanced ACM Panel Manual 45 • Get a Pitot/Static and Transponder Test before the first flight. Background Dynon Avionics SV-ADAHRS-200/201 use airspeed in the calculation of attitude (or GPS ground speed when airspeed is unavailable). The internal rate sensors are monitored and calibrated in flight using feedback from the accelerometers and from airspeed to achieve a highly accurate attitude solution. When a pitot or static test is performed the sensors in the SV-ADAHRS-200/201 are being exposed to dynamics that are impossible to achieve in a real aircraft flight environment, namely, large airspeed changes without the accompanying accelerations and rotations. This false condition will cause a well-calibrated unit to incorrectly adjust its calibration. Furthermore, when a unit is in a test situation a change in applied pitot or static pressure will cause the attitude to pitch up or down. This is expected. The AF-6600/AF-5000 EFIS contains a special mode that allows you to perform required altimeter and/or airspeed checks without affecting the calibration of the attitude-sensing components. Pitot/Static Test Instructions This test must be used when performing pitot/static, transponder, or other tests that manipulate either the pitot or static pressures. You Before conducting any pitot/static testing, follow these guidelines: 1. The aircraft itself should be temperature stable. For example, if the aircraft is moved from outside in the sun to a hangar for testing, tests should not be started until the airplane has stabilized at the hangar temperature. 2. Transponders and ADS-B OUT systems operating under test conditions transmit specific information about the aircraft, including position and altitude data. These tests frequently involve a check of the aircraft’s altimetry system in which air pressure is induced into the pitot static system to simulate operation at various altitudes. In cases where transmission lines are not attached directly to test equipment, antenna shielding must be used to prevent propagation of test signals with potential to interfere with ATC operations or TCAS-equipped aircraft operating in the area. 3. Turn AF-5000 on and let it warm up until the altitude reading is stabilized. This period should be at least 5 minutes, but may take longer depending on environmental conditions. Connect your Pitot/Static Test Set to the aircrafts Pitot and Static ports. You will need to cover the two Dynon Pitot Tube drain holes on the bottom of the Pitot Tube. 4. To enter the Altitude Test mode select: SET > CAL > 12. Altitude Menu on the EFIS. Both the active and standby ADAHRS (if equipped) are shown to allow a single test to calibrated multiple ADAHRS. The altitude values shown in this mode are the same as you would encounter while in-flight with a Baro setting of 29.92 . They are not adjusted or otherwise altered from their normal readings and behaviors. 5. Set Airspeed to stable constant airspeed on your Pitot/Static Test Unit, we usually use 65 knots. 6. Set Altitude Climb rate to a value of +/- 2000 fpm on your Pitot/Static Test Unit. 7. Perform a standard leak check on the Pitot/Static system before testing the required altitudes. 8. Set each required Altitude on your Pitot/Static Test unit and verify the altitude is within acceptable limits on each ADAHRS. Version 8.0 Advanced ACM Panel Manual 46 ALTITUDE ADJUST: There is a single point altitude adjustment for each ADAHRS that can be used to adjust the barometric altimeter from the AHRS if it is not in tolerance. This adjustment affects both the displayed altitude and the altitude sent to other devices. Verifying Altitude You can check the altitude from the Altitude Calibration Menu: SET > CAL > 12. Altitude Menu The Configure Altitude Menu will display the non baro adjusted (29.92) altitude from each Adahrs in the aircraft. Manual ALT / GND mode switching Transponder checks require manual switching to ALT and GND mode. A Dynon Avionics SV-XPNDR-261/262 is normally configured to automatically switch between GND and ALT mode based on airspeed and other parameters. You can change the ALT/GND Switch to NONE so that you can turn on the Transponder ALT mode while on the ground. Note: Before changing AUTO ALT/GND, record which squat switch configuration is set; you will need this information to restore AUTO ALT/GND to this setting after transponder testing is complete. Version 8.0 Advanced ACM Panel Manual 47 Pitot/Static Test Chart Altitude - feet Pressure Tolerance ±(feet) ADAHRS 200 ADAHRS 201 Backup EFIS −1,000 31.018 20 0 29.921 20 500 29.385 20 1,000 28.856 20 1,500 28.335 25 2,000 27.821 30 3,000 26.817 30 4,000 25.842 35 6,000 23.978 40 8,000 22.225 60 10,000 20.577 80 12,000 19.029 90 14,000 17.577 100 16,000 16.216 110 18,000 14.942 120 20,000 13.75 130 22,000 12.636 140 25,000 11.104 155 Airspeed (kts) Tolerance ±(feet) ADAHRS 200 ADAHRS 201 Backup EFIS 20 25 40 50 75 100 125 150 175 Version 8.0 Advanced ACM Panel Manual 48 Skyview HDX EFIS Software Configuration (Must be done before first engine start and flight) • Verify that your HDX screens are running software version 15.4 or newer, update if needed. • Enter the EFIS instrument calibration menu by holding down the right two buttons on the PFD • Enter Aircraft Information: Tail Number, Total Fuel Capacity, … • Scan for Network devices by pressing the DETECT button in SKYVIEW NETWORK SETUP Version 8.0 Advanced ACM Panel Manual 49 • Configure ACM SETUP • Configure ACM-ECB Circuit Breaker Sizes in 1/10 amp for each circuit • Configure SV-EMS from the EMS Setup page to match your engine sensors. Version 8.0 Advanced ACM Panel Manual 50 • Configure Engine Information • Configure SV-EMS Sensor Input Mapping to match your engine sensor wiring *The Flaps, Aileron and Elevator Trim do not use the SV-EMS inputs Version 8.0 Advanced ACM Panel Manual 51 • Configure SV-EMS C25 Pins for CHT and EGT Probes • Configure Skyview SENSOR SETUP for each engine gauge Version 8.0 Advanced ACM Panel Manual 52 • Configure Skyview Serial Ports Serial Port 1 : Advanced CTRL Module Serial Port 2 : NMEA 9600 OUT for ELT Data Serial Port 3 : SV-XPNDR-261 Version 8.0 Advanced ACM Panel Manual 53 Serial Port 4 : SV-ADSB-472 Serial Port 5 : SV-GPS-250 or SV-GPS-2020 • Calibrate Trim Positions Version 8.0 Advanced ACM Panel Manual 54 • Configure and Test the Flaps – Set to POSITIONAL if you have a flap position sensor. a. Verify that the flaps run in the correct direction using the Flaps Up and Down Buttons on the ELECTRICAL Page. If they are backwards swap the motor leads or use the Reverse Polarity setting in setup menu. b. Verify that the flaps run in the correct direction using the panel mounted flap switch or Stick Grip buttons. If they are backwards you MUST Swap the wires to the flap switch or buttons. c. Verify that the Flap position value changes in the Setup > Flaps menu when you move the flaps. d. Program the Flap positions in the EMS > Flap Configuration Menu Version 8.0 Advanced ACM Panel Manual 55 e. Verify that the flaps stop at the correct locations. • Calibrate Autopilot servos • Test Autopilot servos • Calibrate and verify the Fuel Tank sensors. • Verify that both EFIS screens are getting ADAHRS and Engine Data • Get a Pitot/Static and Transponder Test before the first flight. Version 8.0 Advanced ACM Panel Manual 56 First Engine Start o With relay protection diodes installed, your EFIS screens can be turned on before the engine is started. o After the engine has started, verify oil pressure and temperature. If none is indicated SHUT DOWN, the engine. Verify all wiring and consult your local A&P, the engine manufacturer, and/or AFS technical support. o Verify all engine indications are correct per your engine manufacturers manual. Before First Flight o Verify you have the latest system software and mapping data (if applicable) - Visit the Dynon/AFS Website for latest software and map data o Weight & Balance page updated with your aircrafts data o Checklist pages updated with information from your aircraft manufacturer o Magnetometer ADAHRS Alignment completed o Pitot/Static check completed from an authorized FAA Repair Station. o Verify that both aircraft ignition system are properly wired and functioning o Verify that Aircraft fuel system (Flow Meter, Pressure Transducer) is properly plumbed and not leaking. o Perform a minimum fuel flow test and verify each tanks unusable fuel quantity. Verify that the RPM, Oil Pressure, Fuel Pressure, Fuel Flow, Manifold Pressure, Oil Temperature, CHT and EGT temperatures are correct and reasonable during a high-power run-up. Never take-off with high temperatures or abnormal readings. Version 8.0 Advanced ACM Panel Manual 57 ACM-EFIS RS-232 Serial Port Mapping AF-5000 Version 8.0 Advanced ACM Panel Manual 58 ACM-EFIS RS-232 Serial Port Mapping Skyview Version 8.0 Advanced ACM Panel Manual 59 Advanced IFR with IFD540 Serial Port EFIS PFD NOTES EFIS MFD NOTES 0 ACM-ECB GARMIN G5 ADAHRS DATA from G5 1 PDA360 Audio Panel ACK ELT/SL30 2 74109 AFS XPNDR *CO CO Detect Option 3 GTR/GNC-2xx IFD Tuning SV-ADSB-47X 4 AVTN/RNAV SV-GPS-250/2020 Advanced RV-10 3 Screen IFD540 Serial Port EFIS PFD NOTES EFIS MFD NOTES 0 ACM-ECB IFD-ADSB Send ADSB to IFD 1 PDA360 Audio Panel ACK ELT/SL30 2 74109 AFS XPNDR *CO CO Detector 3 GTR/GNC-2xx IFD Tuning SV-ADSB-47X AFS-ADSB 4 AVTN/RNAV SV-GPS-250 Skyview Serial Ports Serial Port EFIS PFD NOTES EFIS MFD NOTES 1 ACM-ECB ACM-ECB 2 NMEA 9600 NMEA 9600 ELT Signal 3 TRANSPONDER TRANSPONDER 4 ADS-B ADS-B 5 SV-GPS-250 *GPS-220 SV-GPS-250 *GPS-2020 Advanced IFR with GTN-650 Serial Port EFIS PFD NOTES EFIS MFD NOTES 0 ACM-ECB NMEA 9600 D6 GPS Signal 1 PDA360 Audio Panel ELT/SL30 2 74109 AFS XPNDR *CO CO Detect Option 3 NONE 74112 AFS-ADSB 4 AVTN/FADC1 SV-GPS-250 *GPS-2020 Version 8.0 Advanced ACM Panel Manual 60 IFR Panel ACM Fuse Sizes LABEL SIZE DESCRIPTION LEFT LT 10 Left Landing Light STROBE 7.5 Strobe Lights NAV LT 10 Nav Lights RIGHT LT 10 Right Landing Light PITOT H 10 Pitot Heat TRIM 2 Trim Motors FLAPS 5 Flap Motor ALT FLD 5 Alternator Field Power BOOST P 10 Boost Pump STARTER 7.5 Starter contactor AUX PWR 5 Auxiliary power plug (ACM-FUSE: Cabin Light, Fans, Aux Plug) AUTO P 5 Autopilot Servos NAV 2 Nav 2 Radio COM 2 5 Com 2 Radio XPONDER 3 Transponder and ADS-B Power AUDIO P 3 Remote Audio Panel Power BACKUP 3-5 Dynon D6 EFIS, ELT, CO Detector (5 AMP for AF-5000/HDX) NAV 1 7.5 Navigator NAV Power COM 1 10 Navigator Com Power MFD 5 Copilot EFIS Screen CHARGE 10 TCW Battery, Charge and Pass through power PFD 5 Pilot EFIS Screen Version 8.0 Advanced ACM Panel Manual 61 VFR Panel Fuse Sizes LABEL SIZE DESCRIPTION LEFT LT 10 Left Landing Light STROBE 7.5 Strobe Lights NAV LT 10 Nav Lights RIGHT LT 10 Right Landing Light PITOT H 10 Pitot Heat TRIM 2 Trim Motors FLAPS 5 Flap Motor ALT FLD 5 Alternator Field Power BOOST P 10 Boost Pump STARTER 7.5 Starter contactor AUX PWR 5 Auxiliary power plug (ACM-FUSE: Cabin Light, Fans, Aux Plug) AUTO P 5 Autopilot Servos NAV 2 3 Nav 2 Radio COM 2 5 Com 2 Radio XPONDER 3 Transponder and ADS-B Power AUDIO P 2 Intercom BACKUP 3 Backup EFIS NAV 1 3 Nav 1 Radio COM 1 5 Com 1 Radio MFD 5 Copilot EFIS Screen CHARGE 10 TCW Battery, Charge and Pass through power PFD 5 Pilot EFIS Screen Version 8.0 Advanced ACM Panel Manual 62 AF-6600 / AF-5000 Panel Configuration Checklist (Completed by AFS before panel shipment) N Number:______________ Customer:___________________________ Aircraft:_________________ Tank Size:________ INJ or Carb:______ Verify Fuse or Circuit Breaker Sizes 1. Verify ELT Panel Battery (green sticker with date) 2. Configure EFIS ADMIN Settings DUAL EFIS SCREEN IFR Panel Settings PFD IFD Radio Tuning Fuel Data to IFD/GTN MFD Version 8.0 Advanced ACM Panel Manual 63 SINGLE EFIS SCREEN IFR Panel Settings PFD Version 8.0 Advanced ACM Panel Manual 64 DUAL SCREEN VFR Settings PFD MFD . Serial Ports Functions Navigation Source Selection Version 8.0 Advanced ACM Panel Manual 65 3. SV Network Configuration. Press SCAN and verify that all attached SV-Network devices are detected. Press UPDT to load the current software in all devices. Channel A and B should be green for all devices. 4. Configure Aircraft Info 5. Verify that the Wi-Fi module is installed in MFD and configure Wi- Fi Settings on MFD Screen. Set the NETWORK ESSID to the aircraft N Number. 6. Configure PFD EFIS Inputs if RV-14 (Canopy, Pitot Heat, Stall Warning Tab) 7. Configure Test Audio to 75 and verify that EFIS audio warnings are playing in headset. 8. Configure Autopilot Settings 9. Configure Yaw Damper settings if present. 10. Verify Altitude Settings 11. Configure Airspeed Settings for aircraft 12. Configure AoA Settings for aircraft Version 8.0 Advanced ACM Panel Manual 66 Radios & Transponder Settings 17. Configure Audio Panel Settings on PFD and MFD to PDA360 18. Configure Transponder Settings on PFD and MFD -Tail Number -Length -Width -Max Cruise -ALT/GND Switch -ADS-B In Type -GPS Input Type 19. Configure Com Radio Setup on PFD and MFD Primary S/N (from SV-NET Scan) Radio Type SV-COM Squelch 70 Side Tone 25 Mic Gain 50 20. NAV Radio Configuration DISABLED Version 8.0 Advanced ACM Panel Manual 67 Electrical System Settings 21. Configure Electrical System for ACM-ECB The ACM-ECB configuration is what controls how the panel switches operate. 2. Audio Alarms Turns on ACM audio warnings 3. Strobe Switch Three Position Strobe/Nav or separate switches. 4. Switch Lights Controls Backlite always ON or turn on with NAV switch 5. Operation Mode Landing Lights with WIGWAG 6. Warm Up Time Time delay in seconds before landing lights start to flash 7. Cool Down Time Time delay in seconds after landing lights are turned OFF before they can be turned back ON. 8. On Above Airspeed Above this Airspeed (Knots ) the landing lights will flash when the Panel switch is in the PULSE mode. Below this airspeed they will remain ON. 22. Configure Primary Volts Settings for the EFIS Primary Volt Meter 23. Configure Backup Volts Settings for the EFIS Backup Volt Meter. When enabled the Backup Voltmeter splits the volt meter bar to display both voltages. 24. Configure Amperage (Shunt) 25. Configure Amperage (Hall-effect) EFIS Amp meter display settings from the optional shunt transducer. Version 8.0 Advanced ACM Panel Manual 68 Fuel System Settings 27. Verify Fuel Flow Settings Set Red High and Yellow high for Engine HP 28. Verify Fuel Computer settings 29. Configure Fuel Pressure Sensor and Ranges Carburated Injected Sensor 41015 (0-15PSI) Kavlico 41150 (0-150PSI) Kavlico150 Max 15 40 Red High 10 35 Yellow High 8 30 Yellow Low 3 15 Red Low 2 12 Min 0 0 Carb Setting Injected Settings 30. Configure Tank 1 31. Configure Tank 2 32. Set Tank 3 to Zero Gallons and OFF 33. Set Tank 4 to Zero Gallons and OFF Version 8.0 Advanced ACM Panel Manual 69 Engine Sensor Settings 34. Verify Manifold Sensor Configuration 35. Verify RPM set to 2 Pulses for 4 Cylinder and 3 Pulses for 6 Cylinder 36. Configure Oil Pressure 41101 (0-150) 101693-000 Kavlico 37. Configure Oil Temp 40405 VDO Version 8.0 Advanced ACM Panel Manual 70 38. Verify that EGT Sensor Type is K 39. Verify that CHT Sensor type is J 41. Configure HP Engine Type and Horse Power 42. Configure Carb Temp Carb = ON INJ = OFF Version 8.0 Advanced ACM Panel Manual 71 Flaps & Trim Settings 44. Configure Flap Position Operation Mode The Flaps can be configured for MOMENTARY or POSITION mode if you are using a RayAllen POS12 flap sensor. Position Calibration You can program 4 unique flap positions. Retract Mode Selects if the flap move all the way UP or Multi-Step to the programed positions. Motor Polarity Used to change motor direction for the CHECK > ELECTRICAL > FLAPS > UP / DOWN buttons. Do not use this setting to change flap direction from the stick buttons. If the ELECTRICAL Page buttons work in the correct direction and the stick buttons are backwards you must swap the push button wiring at the sticks. Endpoint Slop Timeout This setting is used to make sure the flaps move up and down all the way in position mode. The flap motor will continue to run for this settings seconds in the UP and DOWN positions. 45. Configure Elevator Trim to ACM Version 8.0 Advanced ACM Panel Manual 72 46. Configure Aileron Trim to ACM Version 8.0 Advanced ACM Panel Manual 73 IFD-540/440 Configuration when connected to AF-6600 / AF-5000 USB Slot To enter configuration mode you will need to power up the IFD with a USB memory stick. ARINC config with AF-6600 / AF-5000 Set Out 1 to HIGH Speed, Set In 1 to Low for AF-5000 / AF-6600 Version 8.0 Advanced ACM Panel Manual 74 Serial Port Config for AF-6600 / AF-5000 Only Shadin-fadc Enables fuel range rings on IFD Map, AF-5000 / AF-6600 Only. AFS EFIS Remote IFD COM Radio Tuning (Requires PFD and MFD EFIS in Panel) PFD Serial Port 3 must be wired to IFD and configured for IFD COM VOR / LOC / GS ARINC 429 Config for AF-6600 / AF-5000 ONLY Set RX to Low and TX to High Speed Version 8.0 Advanced ACM Panel Manual 75 OPTIONAL Serial Port Config for IFD ADS-B Weather and Traffic The PFD EFIS serial port #3 is wired through the ACM-ECB to the IFD serial port 3. You can choose to use this serial connection to enable the EFIS to tune the IFD COM radio or have the EFIS send ADS-b data to the IFD. If you choose to use the serial port connection for ADS-b data you should configure the IFD using the following settings. NOTE: The Dynon HDX does not support sending ADS-b data to the IFD Shadin-fadc Enables fuel range rings on IFD Map, AF-5000 / AF-6600 Only. Receive ADS-B data from AFS EFIS (Requires PFD and MFD EFIS in Panel) PFD Serial Port 3 must be wired to IFD and configured for ADS-B GDL90 Out Version 8.0 Advanced ACM Panel Manual 76 IFD-540/440 Configuration when connected to Dynon HDX or Skyview USB Slot To enter configuration mode you will need to power up the IFD with a USB memory stick. ARINC config with Dynon HDX or Skyview Set In 1 and Out 1 to High Speed Version 8.0 Advanced ACM Panel Manual 77 Serial Port Config for Dynon HDX and Skyview Sends Aviation Data to Dynon EFIS Sends Certified GPS position data to Transponder VOR / LOC / GS ARINC 429 Config for Dynon HDX and Skyview Set RX to High and TX to High Speed Version 8.0 Advanced ACM Panel Manual 78 GTN-650xi/750xi Configuration for AF-6600 / AF-5000 Only The PFD EFIS serial port #3 is wired through the ACM-ECB to the GTN serial port 3. If your panel has a PFD and MFD EFIS you can use this serial connection to enable the EFIS to tune the GTN COM radio. The AF-6600 / AF-5000 EFIS will send the required data to enable Smart Glide on the GTN. ARINC Settings RS-232 Serial Configuration Fuel Flow and Tank Level data to GTN Aviation data to EFIS Sends Certified GPS position data to Transponder Allows EFIS to Tune GTN COM Radio VOR/LOC/GS Settings GTN Smart Glide Settings Set Glide Ratio and Best Glide Speed for your aircraft Version 8.0 Advanced ACM Panel Manual 79 GTN-650xi/750xi Configuration for Dynon HDX / Skyview The Dynon HDX or Skyview EFIS does not support remote GTN COM Radio tuning or send the required data to enable the use of Smart Glide ARINC Settings RS-232 Serial Configuration Aviation data to EFIS Sends Certified GPS position data to Transponder VOR/LOC/GS Settings Version 8.0 Advanced ACM Panel Manual 80 Garmin GPS-175 Configuration The GPS-175 plugs into the ACM GPS NAVIGATOR connector using harness P/N: 57536 The GPS-175 needs to be configured (hold knob during power on) using the following settings: AF-6600 / AF-5000 EFIS Skyview EFIS You can verify that the interface is working from the GPS-175 start up Instrument Test page. The EFIS LCDI, VCDI, Flag, OBS and DTK should match the GPS-175 display settings with the waypoint GARMN. Version 8.0 Advanced ACM Panel Manual 81 Garmin G5 EFIS Configuration The Garmin G5 can be used as a backup ADAHRS for an AF-6600 or AF-5000 EFIS. The AFS EFIS will do AHRS cross checking using the systems SV-ADAHRS and G5. You can select the ADAHRS to use from the EFIS Options Menu by touching the aircraft symbol on the center of the screen. If an ADAHRS fails, the system should switch to the backup ADAHRS if you have selected AUTO. The color of the aircraft symbol changes based on the current ADAHRS in use. The G5 should be connected to the ACM Backup EFIS DSUB 9 Connector. The ACM Backup EFIS serial port connection is wired to the MFD EFIS using serial port #0. Garmin G5 - RS-232 Configuration Input Format None Output Format Text Baud Rate 115200 MFD EFIS Serial Port 0 Function setting - GARMIN G5 BACKUP Version 8.0 Advanced ACM Panel Manual 82 Instrument Panel System Tests • ADAHRS 1 and 2 working • Verify all buttons • Verify Knobs • Verify Joystick (AF-5600) • Test Dimmer • Verify Ethernet (EMS and Bugs work on both screens) • Test AP Panel FD Button • Verify Map Database is current and High Res Terrain from USB sticks • Verify ADAHRS cross check is working • Verify Bugs are turned ON (Heading, ALT, Speed) • Verify EFIS Backup Battery (Shutdown and Button 1 Power Up) RADIO and Audio Panel Tests • Pilot PTT – Radio TX is displayed on the AF-COM Panel and radio transmits. • Copilot PTT – Radio TX is displayed on the AF-COM Panel and radio transmits. • Radio receives from handheld • Intercom works between headsets, verify squelch and volume work. • Music input works • EFIS PFD sets and displays radio freq • EFIS MFD sets and displays radio freq. • Radio displays airport data from EFIS • EFIS audio works, test using EFIS timer • EFIS PFD and MFD screens can flip-flop radio Trim Servo Tests • Trim and Flap motors work from control sticks • Flap motor works from panel flap switch • Trim and Flap positions change on EFIS PFD and MFD. • Program and test flap positions Panel Dimming • Panel buttons dim with EFIS screens • AP Panel Module buttons dim with EFIS screens • Dynon Radio dims with EFIS screens Version 8.0 Advanced ACM Panel Manual 83 Aircraft Lights • Left Landing light turns on • Right Landing light turns on • Landing lights flash in Pulse Mode • Nav lights turn on • Strobe lights turn on Auto Pilot Tests • AF-SV Scan for Servos • Set Travel Limits • Motors turn ON and OFF ELT Tests • Test GPS Signal to ELT using scope on pin 4. D6 EFIS Tests • Compass Wiring? • D6 Receiving GPS data? Pitot Tube Tests • Pitot Status line +12V Power Plug • Verify Power Version 8.0 Advanced ACM Panel Manual 84 Remote Component Mounting RV-7 Slider Panel Version 8.0 Advanced ACM Panel Manual 85 57840 Aircraft Front Harness Use the supplied DSUB 15 Pin male connector assembly P/N: 50115MA and schematic to wire the aircraft front connector. Verify wire sizes from this drawing. Version 8.0 Advanced ACM Panel Manual 86 57844 Aircraft Front Harness with PPS Version 8.0 Advanced ACM Panel Manual 87 57850 AIRCRAFT REAR HARNESS Use the supplied DSUB 25 Pin male connector assembly P/N: 50125MA and schematic to wire the aircraft front connector. Verify wire sizes from this drawing. Version 8.0 Advanced ACM Panel Manual 88 57854 AIRCRAFT REAR HARNESS AeroLED Lights Version 8.0 Advanced ACM Panel Manual 89 AVEO Engineering ZIP TIP Wiring Version 8.0 Advanced ACM Panel Manual 90 EFIS Inputs The PFD and MFD EFIS screen digital inputs (1,2,3) are wired to the ACM Aircraft Rear Connector and configured in the EFIS calibration menu. The EFIS inputs are designed to activate when connected to ground. Version 8.0 Advanced ACM Panel Manual 91 SV-GPS-250 GPS / SV-GPS-2020 / AFS P/N: 73102 GPS Wiring After routing the AF-GPS wires through the fuselage install the supplied DSUB-9 Male connector and plug into the Female AF-GPS harness from the ACM Module. The SV-250-GPS and SV-GPS-2020 all have the same mounting and wiring. The 9 Pin connector on the GPS then plugs into the Transponder-GPS-ADSB harness that plugs into the ACM. Version 8.0 Advanced ACM Panel Manual 92 ADAHRS SV-ADAHRS 200/201 Wiring After mounting the ADAHRS in the rear fuselage you should connect it to the spare SV-NETWORK port on the ACM module. The ADAHRS uses the standard SV-NETWORK DSUB-9 Female cables and should be wired using the following: Version 8.0 Advanced ACM Panel Manual 93 Advanced SV Network Wiring Advanced-SV Network Female D9 Pin Advanced-SV Network Cable Wire Color Description 1 Green Network Data 1 A 2 Black Network Ground 1 3 White with Black Stripe Network Ground 2 4 White with Blue Stripe Network Data 2 B 5 Orange EMS Auxiliary Voltage 6 Blue Network Data 1 B 7 Red Network Power 1 8 White with Green stripe Network Data 2 A 9 White with Red stripe Network Power 2 Network Female D9 Pin Insertion View (Rear) 71320 SV-EMS-220 Wiring Version 8.0 Advanced ACM Panel Manual 95 53914 SV EMS Engine Sensor Harness Diagram Version 8.0 Advanced ACM Panel Manual 96 P/N: 53914-AFS Engine Sensor Harness Wires You can remove all unused wires from the Engine Sensor Harness using a pin removal tool Pin EMS 37-pin Harness Wire Color Sensor 1 Red Optional Aithre CO Detector 2 Yellow Optional Aithre Tank PSI Detector 3 4 Violet/Blue Carb Temp 5 Black Ground – Carb Temp 6 White/Yellow Oil pressure 7 White/Brown Oil temperature 8 Brown Fuel pressure 9 10 11 12 13 Black Ground 14 Yellow Fuel flow 15 Red +8V Fuel Flow & Amps Hall Transducer Power. (*Must have SV-EMS Network Pin 7 jumper to Pin 5) 16 17 Black Ground 18 White/Red +5V Aux Out 300ma 19 20 Orange/Brown Tank 1 – Float Sensor Only 21 Orange/Blue Tank 2 – Float Sensor Only 22 Violet/Yellow Tank 3 or Capacitance Tank 1 23 Violet/Green Tank 4 or Capacitance Tank 2 24 Orange/Green Ammeter shunt + 25 Orange/Violet Ammeter shunt - 26 Green/Red Manifold Pressure 27 28 29 30 31 32 White/Green Standard RPM LEFT 33 White/Blue Standard RPM Right 34 35 36 37 Version 8.0 Advanced ACM Panel Manual 97 P/N: 53914-HDX Engine Sensor Harness Wires You can remove all unused wires from the Engine Sensor Harness using a pin removal tool Pin EMS 37-pin Harness Wire Color Sensor 1 Red Skyview Voltmeter 1 2 Yellow 3 4 Violet/Blue Carb Temp 5 Black Ground – Carb Temp 6 White/Yellow Oil pressure 7 White/Brown Oil temperature 8 Brown Fuel pressure 9 Brown/Blue GP Input 5 – RV14 Pitot Warning 10 Brown/Yellow GP Input 6 – RV14 Canopy 11 Orange GP Input 7 – RV14 Stall Tab 12 13 Black Ground 14 Yellow Fuel flow 15 Red Fuel Flow & Amps Hall Transducer Power. 16 17 Black Ground 18 White/Red +5V Aux Out 300ma 19 20 Orange/Brown Tank 1 – Float Sensor Only 21 Orange/Blue Tank 2 – Float Sensor Only 22 Purple / Yellow Tank 3 23 Purple / Green Tank 4 24 Orange/Green Ammeter shunt + 25 Orange/Violet Ammeter shunt - 26 Green/Red Manifold Pressure 27 28 29 30 31 32 White/Green Standard RPM LEFT 33 White/Blue Standard RPM Right 34 35 36 37 Version 8.0 Advanced ACM Panel Manual 98 53847 SV EMS EGT-CHT Harness Diagram Version 8.0 Advanced ACM Panel Manual 99 ACM FUSE Power Chart Fuse Description Max Amps Connector (Pins) Control 1 Left wing landing light 10 AIRCRAFT REAR (13,25) CPU 2 Stobe Lights 10 AIRCRAFT REAR (11,23,24) CPU 3 Nav Lights 10 AIRCRAFT REAR (9,21,22) CPU 4 Right wing landing light 10 AIRCRAFT REAR (7,20) CPU 5 Pitot Heat 15 AIRCRAFT REAR (18,19) Switch 6 Trim Servos 5 AP PANEL (9) Vin-Power 7 Flap Motor 10 FLAP-TRIM CPU 8 Alternator Field 5 AIRCRAFT FRONT (8) Switch 9 Boost Pump 10 AIRCRAFT FRONT (7,15) Switch 10 Starter Contactor 10 AIRCRAFT FRONT (6,14) Vin-Power 11 AUX Power (Defrost, AUX Plug) 5+5 AIRCRAFT FRONT (12,13) Switch 12 Autopilot servos 10 AP SERVOS (1,5,13) Switch 13 Nav 2 Radio 10 NAV-COM 2 (12,13) AV2 Relay 14 Com 2 Radio 10 NAV-COM 2 (1,2,3) AV2 Relay 15 Transponder + ADS-B 5 XPONDER-GPS-ADSB (1,6) AV2 Relay 16 Audio Panel 5 AUDIO PANEL (1,2) AV2 Relay 17 Backup EFIS - CO Detector 5 BACKUP EFIS (1,5) AV2 Relay 18 NAV 1 Radio + GPS 10 NAV-COM 1 (12,13) GPS NAVIGATOR (1,2) AV1 Relay 19 Com 1 Radio 10 NAV-COM 1 (1,2,3) AV1 Relay 20 MFD EFIS 5 EFIS MFD (1,2) AV1 Relay 21 Backup Battery Charger 10 BACKUP BAT (2,3) AV1 Relay 22 PFD EFIS 5 EFIS PFD (1,2) Vin-Power Advanced Control Module Fuses Version 8.0 Advanced ACM Panel Manual 100 ACM-ECB Electronic Circuit Breakers The ACM-ECB module uses electronic circuit breakers that can be reset or shut off from the EFIS screen. Version 8.0 Advanced ACM Panel Manual 101 57475 AP Servo Harness Version 8.0 Advanced ACM Panel Manual 102 57860 Control Stick Harness with Micro Molex Version 8.0 Advanced ACM Panel Manual 103 57861 Control Stick Harness Generic Version 8.0 Advanced ACM Panel Manual 104 57870 Trim and Flap Servo Harness Version 8.0 Advanced ACM Panel Manual 105 57302 D10 Backup Harness with CO and TCW Battery Version 8.0 Advanced ACM Panel Manual 106 Aircraft Antennas Use RG400 Cable and Contact airframe manufacturer for recommended mounting locations. Antenna Installation AFS does not supply COM antennas, radio coaxial cable, or antenna BNC connectors. The antenna (including coaxial cable and connector) should be installed according to the manufacturer’s instructions. The following considerations should be taken into account when siting the antenna: • The antenna should be well removed from any projections, the engine(s) and propeller(s). It should also be well removed from landing gear doors, access doors or others openings which will break the ground plane for the antenna. • Separation of COM antenna(s) from transponder(s) and GPS receivers / antennas: 1 foot (12 inches). • Separation of COM antenna(s) from Automatic Direction Finder (ADF) or 121.5 MHz Emergency Locator Transmitter (ELT): 4 feet (48 inches) • Separation of COM antenna from another COM or NAV antenna: Recommended separation between COM antenna(s), NAV antenna(s), and ELT antennas is 6 feet (72 inches). Minimum required separation between antennas is 4 feet (48 inches). Ideally, install the primary COM antenna on the lower fuselage, and install the secondary / standby COM antenna on the upper fuselage. • The COM antenna(s) should not be installed in close proximity to AF-5000 displays, modules, or servos to avoid RF interference. • Where practical, plan the antenna location to keep the cable lengths as short as possible and avoid sharp bends in the cable to minimize the VSWR (voltage standing wave ratio). • Double-shielded coaxial cable is superior to single shield coax – more of the transmit power will be coupled to the antenna, and less received signal will be lost. • Electrical connection to the antenna should be protected to avoid loss of efficiency as a result of the presence of liquids or moisture. All antenna feeders shall be installed in such a way that a minimum of RF energy is radiated inside the aircraft. Antenna Ground Plane When a conventional aircraft monopole antenna is used it relies on a ground plane for correct behavior. For ideal performance the ground plane should be very large compared to the wavelength of the transmission, which is approx. 7.5 feet. In a metal skinned aircraft this is usually easy to accomplish, but is more difficult in a composite or fabric skinned aircraft. In these cases a metallic ground plane should be fabricated and fitted under the antenna. As the ground plane is made smaller, the actual dimensions of the ground plane become more critical, and small multiples of the wavelength should be avoided, as should circles. Rectangles or squares are much less likely to create a critical dimension that resonates with the transmissions. The thickness of the material used to construct the ground plane is not critical, providing it is sufficiently conductive. A variety of proprietary mesh and grid solutions are available. Heavyweight cooking foil meets the technical requirements, but obviously needs to be properly supported. Version 8.0 Advanced ACM Panel Manual 107 Antenna Cable When routing the cable, ensure that you: • Route the cable away from sources of heat. • Avoid routing antenna cables together. • Route the cable away from potential interference sources such as ignition wiring, 400Hz generators, fluorescent lighting and electric motors. • Allow a minimum separation of 300 mm (12 inches) from an ADF antenna cable. • Keep the cable run as short as possible. • Avoid routing the cable around tight bends. • Avoid kinking the cable even temporarily during installation. • Secure the cable so that it cannot interfere with other systems. Version 8.0 Advanced ACM Panel Manual 108 FLARM TRX-1500 Interface Version 8.0 Advanced ACM Panel Manual 109 FLARM TRX-1500 Configuration Use the TRX PC configuration software set the TRX-1500 to: Serial Port 3 Output format: GARMIN TIS Baud Rate: 9600 On the MFD EFIS screen: Calibration->Admin Settings. Set item, '6. Port 3' to 'ZAON TRFC' Version 8.0 Advanced ACM Panel Manual 110 FLARM AT-1 Wiring Version 8.0 Advanced ACM Panel Manual 111 RV-14 Panel Install RV-14 Remote Component Mounting The remote radio transceiver, backup battery and audio panel mount on new ribs mounted in the glove compartment area. The following modifications need to be done: • Remove glove compartment ring from the RV-14 sub panel P/N: F-01455B • Install new ribs to the RV-14 sub panel P/N:68102 and P/N:68103 • Install new center console cover plate with Alternator Circuit breaker and Alternator Shunt P/N: 68101 Avidyne IFD-540 Tray Mounting The IFD Tray mounts to the RV-14 airframe panel ribs. You will need to use the IFD tray as a template to mark the side hole locations on the airframe panel ribs. After marking the 8 hole locations, 4 on each side you will need to drill for 6-32 screws. Mount the tray to the airframe panel ribs using qty 8 6-32 x 3/8” counter sunk screws and nylon lock nuts. RV-14 EMS-220 Module Install Mount the EMS-220 to the left side panel mounting rib, see P/N: 25014 RV-14 remote component mounting drawing. RV-14 SV-ADSB-470/472 ADS-B Module Install Mount the ADSB receiver to the right side panel mounting rib, see P/N: 25014 RV-14 remote component mounting drawing. Version 8.0 Advanced ACM Panel Manual 112 Version 8.0 Advanced ACM Panel Manual 113 Version 8.0 Advanced ACM Panel Manual 114 Version 8.0 Advanced ACM Panel Manual 115 Advanced Control Module (ACM) The P/N: 70050 ACM or 70080 ACM-ECB module mounts on the sub panel behind the EFIS PFD. You will need to drill the sub-panel using the ACM module as a template. The ACM module should be connected using QTY:4 10-32 x .5” screw, washer and nylon lock nut. You will also need to drill the sub-panel for the ACM ground wire, make sure you remove the paint for a good electrical contact using a 10-32 x .5” screw, washer and nylon lock nut. • Connect the main power wire from the battery master relay to the red power lug on the ACM. The Van’s supplied main power wire should have a ¼” (0.250”) ring terminal with a molded plastic cover. • Connect the ground power wire from the airframe ground to the black power lug on the ACM. The ACM main ground wire should have a #10 ring terminal with a molded plastic cover. Do not over-torque the power terminal nuts, they are soft copper and will break if over- torqued. Red Main Power Terminal Max Nut Torque: 25 in-lbs Black Main Ground Terminal Max Nut Torque: 19 in-lbs Version 8.0 Advanced ACM Panel Manual 116 RV-14 ADAHRS Mounting and Wiring The RV-14 ADAHRS mounts in the left wing using the Van’s supplied slide in mounting bracket. The Van’s ADAHRS bracket has a built-in tab that will hold the ADAHRS into the slide in mounting bracket. The ADAHRS should slide into the bracket slots and not have any slop or looseness. If the ADAHRS is loose in the bracket you will need to shim the ADAHRS with UHMW tape. If you are using a dual ADAHRS system you should bolt the backup ADAHRS to the primary ADAHRS using the AFS supplied Dual ADAHRS mounting kit and instructions. When the ADARS is properly installed the PITOT/STATIC ports should point forward. The ADAHRS wires are supplied in the Van’s wing kit, you will need to insert the pre-wired female pins into the AFS supplied DSUB 9 female connector and connector Shell. Version 8.0 Advanced ACM Panel Manual 117 RV-14 Aircraft Front Wiring (P/N: 57842) Complete the aircraft front wiring using the following drawing and items. Version 8.0 Advanced ACM Panel Manual 118 57841 RV-14 Front Harness Version 8.0 Advanced ACM Panel Manual 119 RV-14 Airframe Harnesses (P/N: 57852) Install the AFS supplied RV-14 airframe harness Do not purchase or use Van’s RV-14 Airframe Harness P/N: 57852AFS for AF-5600 install or P/N: 57852HDX for a Skyview HDX install. Start in the middle of the fuselage and work toward the ACM connector end (Aircraft Rear, AP Servo, Flap Trim, ADAHRS SVN-Net) routing the harness using Van’s instructions Section 55-02 RV-14 Harness install. You will need to use the supplied Van’s airframe harness bushing kit P/N: Van’s 3346 Version 8.0 Advanced ACM Panel Manual 120 Version 8.0 Advanced ACM Panel Manual 121 57843 RV-14 Canopy Harness Version 8.0 Advanced ACM Panel Manual 122 57851 RV-14 Aircraft Rear / Trim Harness Version 8.0 Advanced ACM Panel Manual 123 57476 RV-14 Servo Harness Version 8.0 Advanced ACM Panel Manual 124 RV-14 Pitch Servo Wiring Version 8.0 Advanced ACM Panel Manual 125 57880 RV-14 ADAHRS Fuselage Harness Version 8.0 Advanced ACM Panel Manual 126 RV-14 Right Wing Roll Servo and Trim Servo Wiring Version 8.0 Advanced ACM Panel Manual 127 RV-14 Heated Pitot Tube The Dynon heated pitot tube is mounted in the left wing using the Dynon Pitot Mast P/N: 102813-000 • Mount the controller box to one of the wing ribs near the pitot tube mounting location. • Extend the Pitot Tube controller wires and connect to the Left Wing C400P Molex connector using the following: Pitot Controller Description Wire Size C400P Male Pin Red +12V Power #14 4 Black Ground #14 Locally grounded using ring terminal White Signal #22 3 The Pitot line and AOA line should be connected to the Dynon ADAHRS using the Dynon Pitot/Static Plumbing Kit P/N: 102628-000 Version 8.0 Advanced ACM Panel Manual 128 RV-14 Optional TruTrak Autopilot Wiring Version 8.0 Advanced ACM Panel Manual 129 Version 8.0 Advanced ACM Panel Manual 130 RV-14 Van’s Tailcone Left Wiring Version 8.0 Advanced ACM Panel Manual 131 RV-14 Pitch Trim Wire Routing Table RV-14 Pitch Trim Servo Wiring ACM Flap-Trim C411P C431J C431J C411P C409P C409J C429J C409P Trim Motor M1 10 2 2 11 11 4 4 4 4 White M2 3 10 10 12 12 5 5 5 5 White C410J C410P C409P C409J C429J C409P Trim Motor +5V 9 5 5 2 2 2 2 ORN/WHT POSN 1 4 4 3 3 3 3 GRN/WHT Ground 2 7 7 6 6 6 6 BLU/WHT Version 8.0 Advanced ACM Panel Manual 132 RV-14 AFS P/N: 57481 Rear Servo Harness Version 8.0 Advanced ACM Panel Manual 133 RV-14 EMS-220 Harness Install (P/N: 53914) If you are installing a Skyview EFIS you will need to wire the SV-EMS input pins (9,10,11) to the RV-14 airframe harness near the ACM connectors. An AF-5600 system uses the EFIS inputs for (Canopy, Stall Tab, and Pitot Heat warning). Version 8.0 Advanced ACM Panel Manual 134 RV-14 AFS SV-Network Wiring (P/N: 57853-AFS) Version 8.0 Advanced ACM Panel Manual 135 RV-14 HDX SV-Network Wiring (P/N: 57853-HDX) Version 8.0 Advanced ACM Panel Manual 136 RV-14 Control Stick Wiring (P/N: 57860) Version 8.0 Advanced ACM Panel Manual 137 RV-14 Input Wiring and Configuration (AF-5000) The RV-14 uses the EFIS PFD inputs to monitor the Canopy Latch, Pitot Heat and wing mounted stall tab. The inputs are wired to the ACM aircraft rear harness and can be tested in the EFIS PFD Configure Inputs page in calibration. Version 8.0 Advanced ACM Panel Manual 138 Version 8.0 Advanced ACM Panel Manual 139 RV-14 Input Wiring and Configuration (Skyview) The Skyview EFIS inputs cannot be used to monitor the Canopy, Pitot Heat or Stall Tab so you will need to connect the inputs from the RV-14 airframe harness to the SV-EMS harness. The RV-14 airframe harness should have three labeled wires to connect to the same color wires in the SV-EMS harness. Function Pin Color Input # RV-14 Connector Pin Canopy Latch 10 Brown/Yellow GP6 C414J 9 Stall Tab 11 Orange GP7 C403P 5 Pitot Warning 9 Brown/Blue GP5 LC400J 3 Using the Skyview Inputs Configuration menu you will need to configure the inputs Version 8.0 Advanced ACM Panel Manual 140 RV-14 Antenna Locations Version 8.0 Advanced ACM Panel Manual 141 Glasair Sportsman Panel Install AF-5600 IFR Panel Skyview HDX IFR Light Panel Version 8.0 Advanced ACM Panel Manual 142 Glasair Sportsman IFR Light Panel Version 8.0 Advanced ACM Panel Manual 143 Glasair Sportsman VFR Panel Version 8.0 Advanced ACM Panel Manual 144 Sportsman Remote Component Mounting P/N: 70080 ACM-ECB Mounting The ACM-ECB module should be mounted to the forward fuselage weldment with three cushioned Adel mounting clamps using the supplied ACM mounting plate. Locate the module so that the clamps connect to the weldment bars. Firewall Harness Routing Left side firewall penetration has the following wires: • Oil Pressure • Fuel Pressure • Oil Temp • Mag P-Leads • Battery Cable • Starter Cable • Cylinder 2,4 CHT- EGT Right side firewall penetration has the following wires: • Fuel Flow • Alternator B Lead • Alternator Field • Cylinder 1,3 CHT- EGT Version 8.0 Advanced ACM Panel Manual 145 P/N: 68201 Sportsman Right Side Avionics Mounting Plate Assembly The SV-EMS-220 module is mounted on the top of the mounting plate. The master and starter relays are mounted on the bottom of this plate. The master relay, starter relay, amperage shunt, manifold sensor and Skyview batteries are mounted on the bottom of the same plate on the right side of the fuselage. For an AF-5000 panel the TCW backup battery mounts on the bottom side of the plate. The TCW Battery mounting nuts are located so they don’t interfere with components on the other side of the plate. Version 8.0 Advanced ACM Panel Manual 146 P/N: 68202 Sportsman Left Side Avionics Mounting Plate Assembly The Transponder and ADS-B receiver should mount on the top of the left front plate. Version 8.0 Advanced ACM Panel Manual 147 The optional PS Engineering Remote Audio Panel mounts on the bottom of the plate with 1” spacers. Version 8.0 Advanced ACM Panel Manual 148 SV-ADAHRS-200/201 Th