Electronics-international MVP-50P Bedienungsanleitung

Glass Panel Engine MonitorGlass Panel Engine MonitorGlass Panel Engine MonitorGlass Panel Engine MonitorGlass Panel Engine Monitor(with In-Flight Data

1.01.01.01.01.0IntroductionIntroductionIntroductionIntroductionIntroduction1.1 Features:1.2 Overview of the MVP Screens:1.3 System Hardware:1.4 SE

1.1 Features:The MVP-50P is a state-of-the-art Glass Panel Engine Monitorwith in-flight data that provides most of the engine and systeminstruments f

Screen goes into a red or yellow operating range, the appropriateannunciator will blink, the appropriate external warning light willblink and an appro

The MVP hardware consists of the following three groups of components:A. Probes, Transducers and Extension Cables – These components are used to meas

1.5 Display Dimming:The MVP provides two methods of controlling the brightness of the TFT display. When the “Brightness Control” isset for “Auto Dim

2.02.02.02.02.0Main Engine ScreenMain Engine ScreenMain Engine ScreenMain Engine ScreenMain Engine Screen2.1 Power-up Add Fuel Message:2.2 Main Scre

The Main Engine Screen provides the aircraft system and engine instruments you will view most frequently during aflight. There is important informati

2.3 RPM and Manifold Pressure:The RPM and M.P. instruments incorporate a digital readout and ananalog arc. The color of the digital readout will ref

132.5 Engine Analyzer:The Engine Analyzer Display has five operating modes: EGT/CHT, Normalized, Lean ROP, Lean LOP andDigital. The MVP’s current m

14the hottest and coldest EGTs and the hottest and coldestCHTs. A differential limit may be set in the “EGT/CHT BarGraph Setup” screen. Information

Important Notice***** MUST READ *****Page 1 of 4If you think it is not important to read this manual, you’re wrong! This manualcontains important op

152.5.4 “Lean - LOP” Operating Mode: This operating mode was designed to assist the pilot in leaning theengine Lean-of-Peak EGT. As you lean, the E

162.7 “System” Annunciator:Between the RPM and M.P. instruments is a “System” annunciator. If any function on the System Screen goes intothe red or

Power-up Announcement: When the MVP is powered up and the Voice Alarm Control Panel switch is placed inthe “ON” position, the MVP will announce, “Voi

3.03.03.03.03.0System ScreenSystem ScreenSystem ScreenSystem ScreenSystem Screen3.1 Trim Indicator (OEM and Experimental):3.2 Flap Indicator (OEM an

The System Screen is intended to display system functions and the configuration of the aircraft. This gives the pilotone location (i.e., one screen)

3.4 Gear Up Warning (OEM and Experimental):The MVP can provide a gear up voice warning if the following functions are monitored: Gear Position, Manif

4.04.04.04.04.0Flight Data ScreensFlight Data ScreensFlight Data ScreensFlight Data ScreensFlight Data Screens4.1 “Help” Screen:4.2 System Screen:4.

A menu of the Flight Data Screens may be found by pressing the“Menu” button when displaying the Main Engine Screen. When theFlight Data Screen Menu o

“K Factor Adjustment” Section:If after filling the fuel tanks you find an error in the fuel “Calc’d Used Since Fill up” field (as shown on thescreen)

274.4 “Fuel Management” Screen:The “Fuel Management” screen is divided into the following foursections:Fuel Level Data:This section displays the fuel

Important Notice***** MUST READ *****Page 2 of 4This manual does not make any recommendations as to specific operating parameters or controllingmetho

28“Dist. Reserve:” Distance you can fly beyond your Way Point based on current Distance to Empty andDistance to Way Point. If the Time Reserve drops

The Tach Timer records the total number of hours the engine is run above 1300 RPM. The Tach Timer may be setin the “Engine Data, GPS, Timers, etc. Se

30What makes the MVP’s Checklists so powerful is the fact that they are interactive. Next to each item is a “check”box. The Select knob allows you t

31Opening a New Flight Plan: A new Flight Plan may be opened in place of the one displayed by pushing the Menubutton while viewing the Flight Plan to

32Reading a General Info File from a USB Data Stick: A Gen Info File may be read from a USB Data Stickand stored into MVP memory by pushing the Menu

5.05.05.05.05.0Setup and Control ScreensSetup and Control ScreensSetup and Control ScreensSetup and Control ScreensSetup and Control Screens5.1 “EGT/

The “Setup and Control Screens Menu” section lists those screens you will most often use to change data duringflight. To view the available Setup and

36“Normalize EGT & CHT Now?”: Normalizing the EGT and CHT bar graph display will set all the EGTbars to the same level and all the CHT bars to th

37Flt #_Date X.csv # = Flight Number (same number stored in the Flight Log, Max Log and Min Log)Date = The date of the flight (example: 11-04-06).X =

5.3 “Voice and Display Controls” Screen:This screen allows you to control and/or set the following warningand display functions. For a voice to be h

Important Notice***** MUST READ *****Page 3 of 4Fuel Level Accuracy Limitations:The accuracy limitations of the MVP are listed below. It is the pilo

5.5 “System Configuration Screens Menu:”The System Configuration Screens Menu allows the installer access a number of setup and configuration screens

6.06.06.06.06.0System Configuration ScreensSystem Configuration ScreensSystem Configuration ScreensSystem Configuration ScreensSystem Configuration Sc

436.1 Password Protection:The MVP provides a number of screens for the pilot to use during flight, none of which require a password. It alsoprovides

446.2 System Configuration Screens Overview:The System Configuration Screens provide access to setup andcalibration data. By accessing this data you

“Write Files to USB Data Stick” Section:“Write All Checklists and Text Files”: This command writes all the Checklists, Flight Plans and GeneralInform

The “Retrieve ALL Backup Config Files” command reads all the stored configuration data on the USB DataStick. If the configuration data was NOT stored

Once the MVP has been configured for your aircraft the password should be set to a unique number to limit accessto the configuration data. Do not los

“Tach Time”: This field allows you to set the Tach Time for the engine. Tach Time should only be changed withthe engine off. Tach Time is a measure

49If the MVP cannot find a valid GPS signal, the Port 2 Receive Status field will switch (every six seconds)between “Trying 9600” and “Trying 4800.”

6.9 “EGT/CHT Bar Graph Limits and Color Setup” Screen:This screen allows you to program up to five color ranges for eachEGT and CHT cylinder. Every

Important Notice***** MUST READ *****Page 4 of 4Important Fuel Level Considerations:DO NOT RELY SOLELY ON THE FUEL LEVEL DISPLAYED ON THE MVP TODO NO

513. To detect a cylinder operating abnormally hot, you may want to set a red color range for each cylinderFrom approximately 30°F above peak EGT To

6.10 “Weight & Balance Setup” Screen:The data in this screen configures the “Weight and Balance” screen (found in the “Flight Data Screens Menu”s

53The tanks must be calibrated with the wings level and the aircraftset for level flight pitch. Start with the tanks empty.“Fuel Tank”: This field s

54“100% Max Power (Continuous at standard sea level)” Section: Enter the engine data requested in thissection from your POH or published performance

“Powered By”: The device that provides the Flap signal isnormally a control pot. This control pot can be powered bythe aircraft bus (preferred) or t

56Screen #2: This screen allows you to select a Main Engine Screen location on which the Function will bedisplayed.Screen #3: This screen allows you

6.18 “2. Function to Main Screen Mapping”Screen:This screen allows you to customize the Main Engine Screen bymapping a function into any one of the f

“Displayed Operating Range (From__To__):” These fields allow you to set the operating range of the Arc orHorizontal Strip Gauges. Set the “From” and

“Probe:” This field displays the Probe assigned to the EDC Input selected above. “Raw Input Value:” This field displays the value of the uncalibrate

“Snap to zero below:” If the Interim Value drops below the value set in this field, the Interim Value will beset to zero.“Proportional to Bus:” If t

Contents(Page 1 of 2)Warranty/Agreement----------------------------------------------------------------------------------------- 11.0 Introduction:

AAAAAAppendixAppendixAppendixAppendixAppendixSpecifications / FeaturesA1.0 Creating a Checklist, Flight Plan or General Information FileA2.0 Recorde

Specifications / Features0425052Rev. D: 12/31/08Models: MVP-50P, MVP-50T, EDC-33P and EDC-33TMVP-50P and MVP-50TWeight: 1.9 Lbs.Environmental: Desi

Volts:Measured on pin 35 of the EDC Top Connector.Range: 0 to 40 volts.Sensitivity: 6400 counts per volt.Note: A VI-221 or FM-VA-MVP-xx may be used to

EDC-33T (Both RPM Channels):Input Trigger: +.39V / 0V (Hysteresis)Input Resistance: 20K ohmsMax RPM: 125 Hz.Sensitivity: 772.52 sensor counts per Hz.

* A Reference junction is provided to accommodate TC probes. Temp channel 8 is closest to the “RefDiode” and is best used for measuring OAT.Resistive

Airspeed (indicated airspeed) and TAS:Airspeed calculations are based on a NASA equation. True Airspeed will be displayed when the follow-ing is true

2. The “To” value in the “Display Operating Range” field must be set to the same value as the RedLimit for the EGTs. Note: This is the same value fou

Flaps:Analog input signals are calibrated using the “Flaps, Trim and Special Function Calibration” screen.Annunciators:The MVP-50x will display annunc

“REF” - If the reference for any function has a problem or a derived value used to calculate the functionhas a problem, the display for the function w

A1.0 Appendix:Creating a Checklist, Flight Plan or General Information FileA1.1 Overview:You can create your own Checklists, Flight Notes (Plans), o

5.0 Setup and Control Screens: ------------------------------------------------------------------ 335.1 EGT/CHT Bar Graph Setup Screen: -----------

~b or ~B BLUE~g or ~G GREEN~p or ~P PINK (PURPLE)~k or ~K BLACK~w or ~W WHITE A1.4 Word Wrap Formatting:Wor

A1.7 USB Memory Stick Directory Structure:In order to help organize the data, we have provided three directories for text files on the USB memory sti

A2.0 Appendix:Recorded Flight Data FormattingA2.1 File Name Format:Individual flights are recorded and stored in the MVP with a unique file name.Exa

ZULU Time: 22:26:37Engine Hours: 283.82 HoursTach Time: 334.67 HoursData Logging Interval: 6 secTIME,MSTR_WRN,RPM;RPM,F.FLOW;G/HR,FUEL L;GAL,FUELR;G

A2.3 Yellow and Red Recording Interval:Normally flight data will be recorded at a rate set in the USB and Data Recording screen. At the momentany Fu

A3.0 Appendix:Calibrating Airspeed1. Connect the Calibrated Pressure Source to the pitot tube and static ports as required.2. Navigate to the “5. E

A4.0 Appendix:Adding Custom Voice Warning Files to the MVPThe MVP can be set to play a separate .wav file as a waring for each function that enters a

Testing .wav files on the MVP:Testing .wav files on the MVP:Testing .wav files on the MVP:Testing .wav files on the MVP:Testing .wav files on the MVP:

A5.0 Appendix:Setting Up the Gear Position and Unsafe IndicatorsThe position of the landing gear is displayed on the MVP System Screen. When the whee

Option 2: Connect one channel on the EDC to the aircraft’s Nose Gear green down light. The state of allthree gears will be displayed on the MVP based

1Warranty / AgreementYou must read the entire Installation and Operating Instructions. If you do not agree to andYou must read the entire Installatio

Page 3 of 36. Navigate to the “4. Redlines, Limits and Color Setup” screen. Select the appropriate Gear for the Function.For each of the Gear Lights

A6.0 Appendix:Setting Up the Gear Warning FeatureThe MVP can provide a gear up voice warning if the following functions are monitored: Gear Position,

Page 1 of 3A7.0 Appendix:Setting Up the MVP to Monitor and Display an AnnunciatorAn Annunciator is displayed as a single light on the MVP. It canbe u

B. Monitoring a Signal that is Switched from an Open to Ground:EDCTemp or Resistive FuelLevel Channel.BusLoadVI-221VI-221Device, Switch orRelayIf a Lo

Page 3 of 36. Navigate to the “2. Function to Main Screen Mapping” screen or the “3. Function to System ScreenMapping” screen as appropriate. Place t

2Electronics International is not responsible for shipping charges or damages incurred under this Warranty.No representative is authorized to assume a