Electronics International MVP-50T Installation Instructions Manual Download Page 35

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3.1 Attach the three EDC 37-pin Wire Harnesses to the EDC:

3.2 Connect the EDC Harness to the Temperature Probes:

3.3 Connect the EDC Harness to the Pressure Transducers:

3.4 Connect the EDC Harness to the Shunt:

3.5 Connect the EDC Harness to the Fuel Flow Transducer:

3.6 Connect the RFLM-4-x Harness to the EDC Connector and to the Resistive Fuel

Level Sensors:

3.7 Connect the EDC Harness to the Capacitive Fuel Level Probes:

3.8 Connect the EDC Harness to the P-300M Magnetic Fuel Level Senders:

3.9 Connect the EDC Harness (Volts Measurement Pin) to the Bus:

3.10 Connect the EDC Harness to the N1 and/or N2 Tach Generator:

3.11 Connect the EDC Harness to the VI-221's (Voltage Interface Units):

3.12 Connect the EDC Harness to Power and Ground:

3.13 Route the EDC RS422 Wires to the MVP Connector:

3.0 INSTALL THE EDC WIRE HARNESSES

AND ROUTE WIRES

Summary of Contents for MVP-50T

Page 1: ... installing or operating the instrument This manual contains warranty and other information that may affect your decision to install this product and or the safety of your aircraft Glass Panel Engine Monitor MVP 50T for Turboprops and Jets Installation Instructions 5 55 W x 5 15 H x 2 4 D Engine Data Converter EDC 33T To PWR GND ...

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Page 3: ...S PRODUCT This product may be returned for a refund Contact Electronics International Inc for details By installing this product the aircraft owner pilot and installer agree to hold Electronics International Inc harmless and in no way responsible for monetary compensation including punitive damages for any incident harm and or damage associated with this product If you do not agree to the above DO...

Page 4: ...r loose fittings connections clamps probes and inspect for leaks chafing obstructions heat damage and anything that may cause unsafe flight before the 1st run up after the 1st run up and after the first flight The MVP allows the pilot to enter checklists flight plans and general information through the USB port This data must be verified for its accuracy by the pilot before it is used Before allow...

Page 5: ...l below 1 8 You should always fly the aircraft in such a manner as to maintain at least the FAA minimum fuel requirements in the aircraft at all times Depending on the mounting location and type of fuel sensor used the MVP may not be able to accurately measure the last few gallons of fuel in the tanks 4 Improper Calibration If the MVP has not been properly calibrated it will not display accurate f...

Page 6: ...check measure the fuel levels in the tanks before every takeoff Crosscheck the measured fuel levels with the displayed levels on the MVP Also crosscheck these levels with the fuel requirements for the flight listed in your flight plan 4 In Flight Make the MVP part of your normal instrument scan Crosscheck the fuel levels displayed on the MVP with your flight plan at each leg of the flight or every...

Page 7: ...nal 16 2 11 Install the Shunt 16 2 12 Install the Fuel Flow Transducer 17 2 13 Install the P 300C Fuel Level Probes 18 2 14 Install the P 300M Magnetic Fuel Level Sender 18 2 15 Install the Resistive Fuel Level Module RFLM 4 X 19 2 16 Install the Voice Alarm Control Panel AV 17CP Optional 19 2 17 Install the Intensity Control Pot CP 1 Optional 19 2 18 Install the Master Warning red and Caution yel...

Page 8: ...MVP Harness to the Fuel Data Input on the GPS Optional 34 4 9 Connect the MVP Transmit Lockout Input pin to the Transmit Key Optional 35 4 10 Connect the MVP Harness to Power and Ground 35 4 11 Connect the MVP Harness to the CO Guardian CO Detector Optional 35 4 12 Connect to the MVP RTDO Port Optional 35 5 0 Mandatory System Setup and Checkout 37 5 1 Power On Checkout 39 5 2 Perform all Steps lis...

Page 9: ...ve Fuel Level Problem 58 7 10 Voltage Problem 58 7 11 Annunciator Problem 59 8 0 Technical Data 61 Specifications Functions and Features 63 Environmental Qualification Form DO 160 71 STC AML 74 A Appendix 77 A1 0 Appendix Connecting an EDC Input to a Custom Probe 79 A2 0 Appendix Connecting a Second EDC to the MVP 82 ix ...

Page 10: ... Agreement shall not apply to any product that has been repaired or altered by any person other than Electronics International Inc or that has been subjected to misuse accident incorrect wiring negligence improper or unprofessional assembly or improper installation by any person This warranty does not cover any reimbursement for any person s time for installation removal assembly or repair Electro...

Page 11: ...NTABILITY OR FITNESS FOR A PARTICULAR PURPOSE PURCHASER AGREES THAT IN NO EVENT SHALL MANUFACTURER BE LIABLE FOR SPECIAL INCIDENTAL OR CONSEQUENTIAL DAMAGES INCLUDING LOST PROFITS OR LOSS OF USE OR OTHER ECONOMIC LOSS EXCEPT AS EXPRESSLY PROVIDED HEREIN MANUFACTURER DISCLAIMS ALL OTHER LIABILITY TO PURCHASER OR ANY OTHER PERSON IN CONNECTION WITH THE USE OR PERFORMANCE OF MANUFACTURER S PRODUCTS I...

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Page 13: ... 1 MVP Display 1 1 2 EDC 33T 1 1 3 Probes Transducers and Modules 1 1 4 Wiring Extension Cables 1 2 Operational Overview 1 3 Installation Overview 1 4 Password Protection 1 4 1 Level 1 Password Maintenance 1 4 2 Level 2 Password OEM Experimental 1 ...

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Page 15: ...VP display via two wires RS422 If a second EDC is installed one of the data lines will be connected to a RS232 channel on the MVP The EDC measures 4 5 long by 3 5 wide by 2 2 high and is to be mounted on the cockpit side of the firewall or in an equipment bay The EDC reduces the wire bundle to the instrument panel by over 100 wires There are three 37 pin D sub connectors that interface the EDC to ...

Page 16: ...h Time Engine Hours Flight Time Pressure Altitude Flaps Trim etc 2 The function is then placed on the Main or System screen of the MVP System Configuration Screens 2 or 3 allows the placement location of the function to be selected for either the Main or System screen 3 The analog and or digital display of the function with redlines limits colors etc is depicted on the appropriate screen Redlines ...

Page 17: ...alibrating the unit 1 4 1 Level 1 Password Maintenance The Level 1 password is for the installer or maintenance personnel This password allows the installer to perform the following A Delete Log Files B Set up the Gear Warning C Adjust the Recovery Factor D Calibrate the Fuel Level for all fuel tanks E Adjust the aircraft s Weight and Balance data F Set the Fuel Weight Tach Time and Engine Hours G...

Page 18: ...tified unit the password is only released under a contract or agreement The password protects the MVP from unauthorized access to calibration data If calibration data is improperly changed it could lead to engine or aircraft damage and or personal injury Once the unit is installed and checked out this password should be changed on either the certified or non certified unit to a unique number and s...

Page 19: ...ator and Gear Warning 2 10 Install the CO Guardian CO Detector 2 11 Install the Shunt 2 12 Install the Fuel Flow Transducer 2 13 Install the P 300C Fuel Level Probes 2 14 Install the P 300M Magnetic Fuel Level Sender 2 15 Install the Resistive Fuel Level Module RFLM 4 X 2 16 Install the Voice Alarm Control Panel 2 17 Install the Intensity Control Pot CP 1 2 18 Install the Master Warning red and Ca...

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Page 21: ... at the bottom of the Model Label G Before starting the installation make sure the instrument will fit in the location you intend to install it without obstructing the operation of any controls CFR 23 1321 a states Each flight navigation and power plant instrument for use by any required pilot during takeoff initial climb final approach and landing must be located so that any pilot seated at the c...

Page 22: ...an existing aircraft panel This method requires creating a sub panel slightly larger than the MVP display The MVP display is mounted in the sub panel and the sub panel is mounted on the front of the existing aircraft panel This allows the installer to rough cut a hole in the aircraft panel to accommodate the MVP display The sub panel covers any imperfections in the cut hole Also the MVP display ma...

Page 23: ... probe depth does not interfere with the inner workings of the engine B OAT Probe Installation Mount the OAT Probe in an appropriate location on the aircraft using the hardware supplied The OAT Probe is sensitive to air temperature changes For this reason do not mount the OAT probe in the path of the cowl or engine exiting air i e on the belly of the aircraft Also if the probe is mounted in the co...

Page 24: ...n be adapted to any pressure line Use only a flexible hose and fittings suitable for aircraft use Route a flexible fuel pressure line from the primary torque pressure pick up point to the pressure transducer and tighten all fittings Do not use the case of the pressure transducer to tighten the pressure fittings Some fittings you may want to consider using are listed below B Oil Pressure Transducer...

Page 25: ...e tight The ports are 1 4 flare union Care should be taken not to put excess pressure on the flexible lines Make sure the flexible lines do not kink E Airspeed Transducer Installation Mount the PT 05Diff Pressure Transducer on the inside firewall or in the equipment bay under the aircraft instrument panel Use the holes in the bottom plate to mount the PT 05Diff Only two mounting holes are required...

Page 26: ...or 2 7 Install the Interface Circuit for Annunciators Any Temperature or Resistive Fuel Level channel on the EDC may be used to monitor the state of a switch relay or output from a device This output can be used to trigger a light annunciator on the MVP Annunciator lights such as Chip Detect Bypass De ice Pitot Heat Fire Fault Exceedance etc can be displayed on the Main or System screen on the MVP...

Page 27: ...it is shown below The Unsafe Indicator is REQUIRED with any landing gear options listed below and requires one EDC input Landing Gear Position There are three options for interfacing the EDC to the aircraft s gear system Option 1 Connect the EDC to the aircraft s Right Left and Nose Gear green down lights The state of each gear will be displayed independently on the MVP Select Gear Left RT and Nos...

Page 28: ...ed with the unit The CO Detector connects to RS232 Port 3 on the MVP 2 11 Install the Shunt An external shunt is a strip of metal usually mounted on a bakelite base This metal is made of special alloys to produce a very small precise signal when current passes through it It is not affected by temperature changes If your aircraft currently has an external shunt you can calibrate your MVP to that sh...

Page 29: ...f fuel through the transducer must follow the direction marked on the transducer E The flow transducer must be mounted so the wires exiting the transducer are pointing up or the cap with five bolts is pointing up or the output port is pointing up or any combination thereof F Before connecting any hoses thoroughly clean them and ensure they are free of any loose material High air pressure may be us...

Page 30: ...VP cannot correct for inconsistent or non repeatable signals from resistive fuel level senders Unfortunately many older resistive fuel level senders and in some cases newer resistive senders exhibit some of the following problems Variation in the wiper to element resistance CRV Stick slip problems with bearings and wiper to element contact Windup causing jumps in readings Weak wiper tension Loose ...

Page 31: ...ce behind the aircraft instrument panel B Using the AV 17CP Control Panel as a template mark the aircraft instrument panel and drill a 1 4 hole for the AV 17CP Switch C Mount the Switch from behind the aircraft instrument panel Be careful not to damage the screenprinting on the Control Panel The Switch must be mounted with the white orange wire up The lock washer should be mounted on the Switch an...

Page 32: ...ional The FAA PMA d FM SC and AC 1 are used to convert engine data from a FADEC unit to the MVP 50 To install the converter follow the instructions provided with the appropriate unit 2 21 Install the BC 5xx Optional The BC 5xx provides an interface between engine and aircraft devices and the MVP 50 The BC 5xx comes with schematics and installation instructions specific to the application Install t...

Page 33: ...tors pointing down on the inside firewall under the aircraft instrument panel or in an equipment bay The EDC SHOULD NOT be installed in a location where it can be pressure washed For a twin engine aircraft the EDC can be mounted on the opposite side of the firewall of the engine or in the cabin or equipment bay Use the holes in the bottom plate of the EDC to mount the unit Be sure you will have en...

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Page 35: ...nd to the Resistive Fuel Level Sensors 3 7 Connect the EDC Harness to the Capacitive Fuel Level Probes 3 8 Connect the EDC Harness to the P 300M Magnetic Fuel Level Senders 3 9 Connect the EDC Harness Volts Measurement Pin to the Bus 3 10 Connect the EDC Harness to the N1 and or N2 Tach Generator 3 11 Connect the EDC Harness to the VI 221 s Voltage Interface Units 3 12 Connect the EDC Harness to P...

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Page 37: ... slack in the cable exiting the probe to prevent damage to the probe over time 3 3 Connect the EDC Harness to the Pressure Transducers Route each of the pressure cables in the EDC harness to the appropriate pressure transducers Cut the wires to length install the appropriate connectors see the Working with Connectors section of this manual for more information and connect to the pressure transduce...

Page 38: ...cable in the EDC harness to the Fuel Flow Transducer Cut the wires to length install the appropriate connectors see the Working with Connectors section of this manual for more information and connect to the fuel flow transducer When connecting to the Fuel Flow Transducer leave some slack in the cable exiting the transducer to prevent future damage to the transducer If the flow transducer is hard m...

Page 39: ...iate capacitive fuel level wires for the number of tanks to be monitored in the EDC harnesses to the capacitive fuel level probes Cut the wires to length install the appropriate connectors see the Working with Connectors section of this manual for more information and connect to the capacitive fuel level probe Note The capacitive fuel level channels are shared with the resistive channels A single ...

Page 40: ...nd referenced Ohm the output pins to ground If the Ohm reading is less than 200 ohms the output signal is ground referenced 2 Connecting the EDC harness to a ground referenced Tach Generator Connect the wire from the appropriate EDC harness to one of the output pins on the N1 and or N2 Tach Generator You re Done 3 Connecting the EDC harness to an ungrounded Tach Generator Ground one of the output ...

Page 41: ...the MVP Connector Route the RS422 white green wire and the RS422 white wire to the MVP connector These wires will be connected to the MVP RS422 wires in a later step If a second EDC is installed see the appendix for connection information MVP RS422 pin 12 MVP RS422 pin 13 Pin 37 Red Wire Pin 19 Black Wire Pin 36 White Wire Pin 18 White Green Wire MVP RS422 Input To Aircraft Ground To the MVP EDC 5...

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Page 43: ...the Audio Panel 4 6 Connect the MVP Harness to the External Intensity Control Pot CP 1 4 7 Connect the MVP Harness to the Moving Map Data Out from the GPS 4 8 Connect the MVP Harness to the Fuel Data Input on the GPS 4 9 Connect the MVP Transmit Lockout Input Pin to the Transmit Key 4 10 Connect the MVP Harness to Power and Ground 4 11 Connect the MVP Harness to the CO Guardian CO Detector 4 12 Co...

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Page 45: ...ll the appropriate connectors see the Working with Connectors section of this manual for more information and connect to the AL 1R Route the MVP Master Caution Out wire White Yellow Pin 17 to the Master Caution Yellow Light AL 1Y White Yellow wire cut the wires to length install the appropriate connectors see the Working with Connectors section of this manual for more information and connect to th...

Page 46: ...ction of this manual for more information and connect to the CP 1 Install the ground and power wires to the CP 1 as shown in the paper work supplied with the control pot 4 7 Connect the MVP Harness to the Moving Map Data Out from the GPS Optional Route the MVP Moving Map Data In wire green wire in a 4 wire cable to the Moving Map Data Output Port on the GPS Cut the wire to length install the appro...

Page 47: ...d to any pin on the MVP other than pin 1 and 2 damage to the MVP and any connected hardware may occur Ensure power is provided on pin 1 and 2 of the MVP before attaching the connector 4 11 Connect the MVP Harness to the CO Guardian CO Detector Optional If a CO detector was installed connect the RS232 output from the Remote Mounted 353 201 experimental only or 452 201 011 certified CO Detector to P...

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Page 49: ...Perform all Steps listed in the MVP 50T Setup Checklist 5 3 Ground Run Checkout 5 4 First Flight Checkout 5 5 Read the Warranty Agreement and the Important Notice 5 6 POH AFM Supplement 5 0 MANDATORY SYSTEM SETUP AND CHECKOUT 37 ...

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Page 51: ...th this installation 5 3 Ground Run Checkout Before starting the engine test the N1 N2 and ITT functions for proper operation If an important function does not appear proper during any phase of the start abort the start Electronics International produces Field Test Devices that output signals to emulate ITT N1 N2 Oil Pressure Fuel Pressure Oil Temperature Fuel Flow shunts and Resistive and Capacit...

Page 52: ...rcraft for normal operation until all steps in this document have been performed and the aircraft is safe to fly 5 5 Read the Warranty Agreement and the Important Notice Require the pilot to read the Warranty Agreement and the Important Notice located in the front of the Operating Instructions before releasing the aircraft for flight 5 6 POH AFM Supplement The MVP 50T Primary Engine Monitor FAA Ap...

Page 53: ...r Lap Connector onto Copper or TC Wire 6 3 2 Installing a D sub Pin onto a TC or Tin Copper Wire MVP 50T 25 pin D sub Connector Wiring Diagram EDC Wiring Work Sheet Top Connector EDC Wiring Work Sheet Middle Connector EDC Wiring Work Sheet Middle Connector MVP 50 Aircraft Panel Cutout Template EDC Template 6 0 INSTALLATION DATA 41 ...

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Page 55: ...any other tool that was not designed to crimp terminal connectors It will NOT produce a long term reliable crimp and eventually you will have problems The real key to achieving a long term reliable crimp is to PREPARE the wire correctly produce a TIGHT crimp and TEST the crimp Another factor which we have covered for you is to use a quality connector made of material with long term spring tension ...

Page 56: ...the insulation Check that the pin is inserted into the crimpers properly Note the ears on the pin must be facing into the center of the crimp tool cavity to produce a good crimp If the pin rotates even a little during crimping the connection will be unreliable C Insert the wire into the pin Check that the insulation is in the strain relief crimp area but not in the bare wire crimp area Crimp the p...

Page 57: ...RK SHEET DB25 CONNECTOR MVP 50T AIRCRAFT ID SAMPLE DB 25 MVP 50T DB 37 RS422 13 RS422 RS422 12 RS422 GRN WHT AIRCRAFT SPECIFIC WORKSHEET WILL BE PROVIDED IN YOUR KIT FOR REFERENCE ONLY Unused Pressure inputs must be grounded DB 25 Back View Wire Side 25 14 13 1 DB 25 421 0331 00 PIN 421 0301 00 EDC 33T OEM or Experimental ONLY External Exit Button External Screens Button External Select Button Tra...

Page 58: ...h 3 Pressure Ch 4 Pressure Ch 5 Pressure Ch 6 17 Do Not Use 34 Do Not Use 21 GND 3 Signal In 2 Signal In 20 5V Pressure Ch 1 16 GND 14 Signal In 15 10V Fuel Flow DB 37 Back View Wire Side 20 37 1 19 EDC WORK SHEET TOP CONNECTOR EDC 33T AIRCRAFT ID SAMPLE AIRCRAFT SPECIFIC WORKSHEET WILL BE PROVIDED IN YOUR KIT EDC 33T DB 37 MVP 50T DB 25 13 RS422 12 RS422 GRN WHT FOR REFERENCE ONLY TOP CONNECTOR U...

Page 59: ...Extra GND 30 Extra GND 36 5V 18 GND 19 Signal In 37 Signal In Pressure Ch 7 DB 37 Back View Wire Side 20 37 1 19 EDC WORK SHEET MIDDLE CONNECTOR EDC 33T AIRCRAFT ID SAMPLE EDC 33T DB 37 MIDDLE CONNECTOR AIRCRAFT SPECIFIC WORKSHEET WILL BE PROVIDED IN YOUR KIT FOR REFERENCE ONLY Unused Pressure inputs must be grounded Extra Grounds maybe used for shields Unused Temp Channels may be used for annunci...

Page 60: ...2 Capacitive Input 33 5V 34 GND Fuel Level Ch 3 30 Signal In 12 Signal In 8 5V 11 GND Pressure Ch 8 31 Signal In 13 Signal In 10 5V 9 GND Pressure Ch 9 DB 37 Back View Wire Side 20 37 1 19 EDC WORK SHEET BOTTOM CONNECTOR EDC 33T AIRCRAFT ID SAMPLE EDC 33T DB 37 BOTTOM CONNECTOR AIRCRAFT SPECIFIC WORKSHEET WILL BE PROVIDED IN YOUR KIT FOR REFERENCE ONLY Unused Pressure inputs must be grounded Extra...

Page 61: ...Template for MVP Cutout 49 ...

Page 62: ...Template for EDC 50 ...

Page 63: ...mperature Problem on all Channels 7 4 Temperature Problem with one Function 7 5 N1 or N2 Problem 7 6 Fuel Flow Problem 7 7 Amp Problem 7 8 Resistive Fuel Level Problem 7 9 Capacitive Fuel Level Problem 7 10 Voltage Problem 7 11 Annunciator Problem 7 0 TROUBLESHOOTING 51 ...

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Page 65: ...d ground wires Ohm the ground wire to ground Look for a short B Symptom COM is displayed for the digital value for most functions The EDC is not communicating with the MVP 1 Problem One of the EDC external 5 volt power supplies on the Bottom Connector is shorted to ground a Action Remove the Bottom Connector If the COM error goes away look for a short on one of the 5 volt wires 2 Problem The Power...

Page 66: ...d wire 5 volts Black wire 0 volts Green wire 1 65 volts and White wire 1 65 volts Short the Green wire to the White wire and look for a zero pressure reading If you do not get a zero reading you may have an open wire Ohm the Black Green and White wires at the pressure transducer to ground The Black wire should be grounded the Green and White wires should not 7 3 Temperature Problem on all Channels...

Page 67: ...uld get a short 10 ohms Ohm one lead of the probe to ground You should get an open 100K ohms 7 5 N1 or N2 RPM Problem An N1 or N2 Tach Generator produces a sine wave at a frequency equal to the RPM of the engine The voltage level of the sine wave is very low at low RPM and can be above 20 volts at high RPM The signal is generated from a coil inside the unit Most Tach Generators have three coils an...

Page 68: ...Inaccurate jumpy or zero reading 1 Problem A wire is open shorted or mis wired a Action Measure the voltage on the transducer wires from the EDC at the Flow Transducer The Red lead 10 volts Black wire 0 volts White wire 5 volts with the White wire removed from the flow transducer Ohm the Black wire to ground The Black wire must be shorted to ground 10 ohms Rapidly tap the White transducer wire to ...

Page 69: ...data in the Fuel Tank Calibration screen Resistive floats are notoriously inaccurate and inconsistent A float will move up and down millions of time during its lifespan They can move even when the aircraft is parked The metal to metal contact of the wiper to the coil wears and corrodes The wiper force weakens The bearing surfaces wear It s not uncommon to find even new floats that work poorly The ...

Page 70: ...e called sensor counts based on the signal frequency The sensor counts can be viewed in the Fuel Tank Calibration screen The sensor counts are then converted to a fuel level based on the calibration data in the Fuel Tank Calibration screen A Symptom An Err is displayed for the digital value Also you may have an inaccurate jumpy or zero reading 1 Problem The IMC is mis wired a Action Measure the vo...

Page 71: ...edlines Limits and Color Setup screen Note The color white will be displayed as black or off You can also set the trip level at which the Annunciator changes color The trip level is displayed in sensor counts so you will need to get a sensor count reading with the Annunciator on and then off Set the trip level between the on and off value A Symptom The Annunciator is not changing colors 1 Problem ...

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Page 73: ...Specifications Functions and Features DO 160 Environmental Qualification Form STC and AML 8 0 TECHNICAL DATA 61 ...

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Page 75: ...eye and external control line EDC 33P and EDC 33T Weight 1 0 Lb Environmental Designed and Tested to TSO DO 160E See Environmental Qualification Form Software Designed and Documented to TSO DO 178B Level C Power Requirements 7 5 to 30 Volts 0 1 amps Typ Accuracy all Functions 1 Unless otherwise noted Input Configuration EDC 33P 1 Volt Channel 1 Amp Channel 1 Fuel Flow Channel 6 Pressure Channels 1...

Page 76: ...period Notes 10 Volts are provided from the EDC to energize the flow transducer An FFDM 1 MVP module may be used to accommodate fuel return from a pressure carburetor A FM Flow P module may be used to measure flow from a pulsed injector RPM Piston EDC 33P Two RPM channels are available May be configured for digital or mag pickup Also may be set up to operate from one or two inputs Selectable jumpe...

Page 77: ...nsor counts per Hz Accuracy 5 Ch 2 N1 Input Trigger 11V 0V Hysteresis Input Resistance 20K ohms Max RPM 6140 Hz Sensitivity 16 1 sensor counts per Hz Accuracy 5 EDC 33T W Both RPM Channels Input Trigger 054V 0V Hysteresis Input Resistance 1M ohm Max RPM 10 2K Hz Sensitivity 8 963 sensor counts per Hz Accuracy 5 Pressure Input 0 to 2 5 Volts Differential Input Resistance 20M Ohms Common Mode Range ...

Page 78: ...per channel Input Range 0 to 18 Volts single ended input Input Resistance 14 4K Ohms Sensitivity 07169mV per count when set for non ratiometric measurement Notes The Resistive Fuel Level inputs may be used to monitor other functions or annunciators When monitoring a resistive probe a RFLM 4 12 or 24 module will be required see EI price sheet Also measurements are made ratiometric to the bus voltag...

Page 79: ...AT function to be displayed Recovery Factor Recovery Factor is used to calculate Corrected OAT and True Airspeed TAS The Recovery Factor compensates for airspeed altitude OAT probe design and OAT probe placement The setting is between 0 and 1 99 with 1 0 being the average setting for most configurations The Recovery Factor is set to produce no change in the OAT between slow flight and fast cruise ...

Page 80: ...r Graph CHT Max Limit Line MVP 50T If the following conditions are met a CHT Red Max Limit Line will be drawn 1 The Cylinder field in the EGT CHT Bar Graph Limits and Color Setup screen must be set to ALL for the CHT function 2 The To value in the Display Operating Range field must be set to the same value as the Red Limit for the CHTs If these conditions are NOT met the CHT Max Limit Line will be...

Page 81: ...al input signals routed into a Temp or Resistive Fuel Level channel on the EDC An annunciator for landing lights nav lights boost pump door or canopy latch deicing warning indications chip detect door seals bleed air step status FADEC outputs ignition status faults ATR switch settings and many more status indications may be displayed on the MVP 50x Date Local Time and Zulu Time When the MVP is off...

Page 82: ...nel the function associated with that channel on the MVP will display A D for the value OVR If a channel on the EDC is over ranged 2 5 volts differential an OVR will be displayed for that function Err If a capacitance fuel probe is unplugged the fuel level will be displayed as Err REF If the reference for any function has a problem or a derived value used to calculate the function has a problem th...

Page 83: ... FFDM 1 MVP FM VA XX DPIM 1 FFDM 1 FFAM 1 FM FP XX FM Gyro CP 1 AL 1 x Specifications Document 0425052 can be found in the MVP 50 Installation Instructions Manufacturer Electronics International Inc 63296 Powell Butte Hwy Bend OR 97701 Test Requirements DO 160E Changes 1 2 and 3 Conditions Section Description of Tests Conducted Temperature and Altitude 4 Tested to Category D1 Operating Temp 200 C ...

Page 84: ...cies noted during any test Explosive Atmosphere 9 Category X No test performed Waterproofness 10 Category X No test performed Fluids Susceptibility 11 Category X No test performed Sand and Dust 12 Category X No test performed Fungus 13 Category X No test performed Salt Fog Test 14 Category X No test performed Magnetic Effect 15 Tested to Category Z Less than 3m Power Input 16 Tested to Category Z ...

Page 85: ...category H Radio Frequency Emission 21 Tested to Category M Suitable for transport aircraft Lightning Induced Transient Susceptibility 22 Tested to Category B2XXX Lightning Direct Effects 23 Category X No test performed Icing 24 Category X No test performed Electrostatic Discharge 25 Category A Fire Flammability 26 Tested to Category C Flammability 73 ...

Page 86: ...STC AML 74 ...

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Page 89: ...A1 0 Connecting an EDC Input to a Custom Probe A2 0 Connecting a Second EDC to the MVP A APPENDIX 77 ...

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Page 91: ... Type Differential Voltage a plus and minus input is provided A single ended input may be used Voltage Range 0 to 2 5 Volts Common Mode Voltage Range 0 to 4 Volts Resolution 9 537 uV per Count Maximum Counts Available 262 143 Input impedance 12 1K Ohms to ground each input Differential impedance 24 2K Ohms EDC Pressure Input Type Differential Voltage a plus and minus input is provided The input vo...

Page 92: ...re setting a series of calibration parameters that will be applied to the signal received from the Custom Probe There are two Software Probes that may be used for most Custom Functions Volts 0 2 5 Use this Software Probe when the output signal from the Custom Probe is a variable voltage from 0 to 2 5 volts or less and the signal voltage does NOT change with bus voltage Res 0 2 5V Use this Software...

Page 93: ... the selected Function The 4 Redlines Limits and Color Setup screen provides the necessary parameters Navigating to the 4 Redlines Limits and Color Setup screen Start with the Main Engine screen push the MENU button Select System Configuration Menu Select 4 Redlines Limits and Color Setup screen 81 ...

Page 94: ...ing Work Sheets found in the MVP Installation Instruction Manual The pin designations for the wiring harnesses on the secondary EDC are exactly the same as on the primary EDC Follow the MVP 50 installation instructions when connecting the wires from the secondary EDC wire harness to any transducers Tie wrap all wires so they do not obstruct the freedom of travel of any controls 4 Route the Power a...

Page 95: ... must be running software with an ID of 2 x x or greater to use the second EDC 7 Input Ambient Temp Calibration Data for the Second EDC Navigate to the 5 EDC Input Cal screen found in the System Configuration Screens Menu Change the Input line to Temp Comp 2 Scroll to the Reset values back to factory defaults line found at the bottom of the screen and select Yes Next Scroll to Offset and set its v...

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