Installation Manual Instruction Manual

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FAA Approved Installation Manual for the Report No 908

EDM-900 and EDM-930 Page 1 of 50 Rev J

Primary Engine Data Management System Date 5-24-14

TABLE OF CONTENTS

Section Page

Revisions ______________________________________________________________________________________ 2

2. Read This First _________________________________________________________________________________ 2

3. Instrument Labeling______________________________________________________________________________ 3

4. Primary TSO Label ______________________________________________________________________________ 3

5. Operation and Abbreviations ______________________________________________________________________ 4

6. Remote Alarm Light EDM 900 _____________________________________________________________________ 5

7. Locating and Installing the Indicator and Remote Alarm Display (RAD and Alert Light) ________________________ 8

8. EDM-900/930 Key information installation __________________________________________________________ 10

9. Routing the Wiring Harnesses_____________________________________________________________________ 11

10. Pressurized Aircraft wire Routing__________________________________________________________________ 11

11. Power Connection ______________________________________________________________________________ 12

12. Probe Wiring __________________________________________________________________________________ 12

13. Exhaust Gas Temperature Probe (EGT) Installation ___________________________________________________ 13

14. Cylinder Head Temperature (CHT) Probe Installation__________________________________________________ 14

15. Radial Engine CHT (spark plug gasket) _____________________________________________________________ 14

16. Outside Air Temperature (OAT) Probe Installation ____________________________________________________ 14

17. Oil Temperature Probe Installation ________________________________________________________________ 15

18. Oil Pressure Sensor Installation ___________________________________________________________________ 15

19. Fuel Pressure Sensor Installation using combination sensor _____________________________________________ 16

20. Ammeter Shunt Installation _______________________________________________________________________ 17

21. General Fuel Flow Transducer Installation __________________________________________________________ 18

22. Fuel Level Sender Wiring Types ___________________________________________________________________ 20

23. Fuel Flow Totalizer, Refuel Question _______________________________________________________________ 26

24. GPS Interface _________________________________________________________________________________ 27

25. Manifold Pressure (MAP) Sensor __________________________________________________________________ 27

26. RPM Sensor installation _________________________________________________________________________ 28

27. EDM-900/930 Specifications and Limitations_________________________________________________________ 30

28. EMI Radio Test and functional check: ______________________________________________________________ 31

29. Component Parts_______________________________________________________________________________ 32

30. Weight and Balance Data ________________________________________________________________________ 34

31. Pilot Programming _____________________________________________________________________________ 34

32. Programming the HP Constant ____________________________________________________________________ 35

33. Programming the MAP __________________________________________________________________________ 35

34. Selecting Fuel Pressure Type (EDM-900 only)________________________________________________________ 35

35. Customizing Non-Primary Data (EDM900 only) ______________________________________________________ 36

36. K Factor______________________________________________________________________________________ 36

37. Fine tuning the K Factor _________________________________________________________________________ 37

38. Adjusting the K Factor___________________________________________________________________________ 38

39. Programming Accumulate Trip Total _______________________________________________________________ 38

40. Trouble Shooting _______________________________________________________________________________ 39

41. GPS Interface Diagnostics _______________________________________________________________________ 40

42. Connector Pin Assignments on EDM, J1 through J5 _______________________________________________ 41

43. Connector Pin Assignments on EDM, J1 through J5 ___________________________________________________ 42

44. J3 RPM, MP, Oil-P_____________________________________________________________________________ 45

45. Appendix A Connector Pin Assignments on EDM, J1-J2 Only with ARINC 42 ______________________________ 49

46. Appendix B ICA _______________________________________________________________________________ 50

The Owner of the EDM-900/930 must keep this manual

J.P. INSTRUMENTS

PO BOX 7033

HUNTINGTON BEACH CA

Last printed 6/2/2014 10:18:00 AM

Summary of content (50 pages)

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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 1 of 50 Rev J Date 5-24-14 TABLE OF CONTENTS Section 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31. 32. 33. 34. 35. 36. 37. 38. 39. 40. 41. 42. 43. 44. 45. 46.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 2 of 50 Rev J Date 5-24-14 1. Revisions REV Description Date Approval G Added new pictures of 900 and 930, page 6. Abbreviations page 4. Revised how the JPI data base functions, page 3. Added revision box. Page 2. Added fuel level calibration, page 22. Renumbered all pages. 9-28-2011 JFP H Revised to include new trouble shooting section for ICA and renumber pages.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 3 of 50 Rev J Date 5-24-14 3. Instrument Labeling The TSO label on the instrument is marked as to the instrument configuration.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 4 of 50 Rev J Date 5-24-14 5. Operation and Abbreviations The EDM-900/930 is a combined electronic indicating system which simultaneously displays to the pilot powerplant and aircraft systems operating parameters. It includes the following indicating systems; replacing all previous primary digital and/or analog instruments: Message Area Abbreviation in parenthesis.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 5 of 50 Rev J Date 5-24-14 6. Remote Alarm Light EDM 900 The remote alarm light is a Red or Yellow light depending on the alarm condition. The EDM-900 incorporates a single light that alerts the pilot that a problem existing within the engine.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System RAD EDM-930 Display Report No 908 Page 6 of 50 Rev J Date 5-24-14
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 7 of 50 Rev J Date 5-24-14 EDM-900 TFT Flat panel display Portrait Mode Remote Alert Light With the placard “Engine” EDM-900 TFT Flat panel display Landscape Mode EDM-900 system mounts in a 3.125 inch diameter instrument panel hole in either a portrait or landscape position depending on panel hole location. By holding the Step button ( first on left) for approx.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 8 of 50 Rev J Date 5-24-14 7. Locating and Installing the Indicator and Remote Alarm Display (RAD and Alert Light) Single Engine Aircraft EDM-900/930 A) The EDM-900/930 display should be located as close as possible to the pilot with an unobstructed view and for easy access to the buttons on the instrument. The least desirable view angle is landscape looking up.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 9 of 50 Rev J Date 5-24-14 Mounting bracket for the EDM-900 EDM-900 Model: Mounts in a standard 3.1/8” instrument hole. First, place the mounting bracket on the instrument and tighten the clamp hex screw until you can just remove the instrument from the bracket.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 10 of 50 Rev J Date 5-24-14 5. EDM Display Installation Choose the Proper Installation Location The display is best located within the natural scan and easy reach of the pilot. The recommended mounting location is defined as the distance from the vertical centerline of the Primary Flight Instruments to the outer edge of the further most gauge displayed on the EDM.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 11 of 50 Rev J Date 5-24-14 Be sure to verify that this matches your aircraft. Note: If your EDM should ever have to be replaced with a different unit, the factory will reprogram it to match your configuration. You should always retain your fuel quantity calibration records, as these may need to be manually reentered in a different or serviced unit. 9.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 12 of 50 Rev J Date 5-24-14 11. Power Connection The EDM automatically adapts to either a 14 or 28-volt electrical system. Master Bus power wire to the EDM should be 20ga copper connected directly to the master solenoid located at the battery to avoid a line drop when cranking. A 5 amp circuit breaker is required. Connect the EDM ground wire to the engine block.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 13 of 50 Rev J Date 5-24-14 13. Exhaust Gas Temperature Probe (EGT) Installation Use the J2 connector harness 700700 or 700702 labeled E1 through E4 or E6. Remove the existing EGT gauge and Probe. Replace with JPI probe M-111 in all exhaust stacks. EGT probe Drill no. 40 pilot hole, then no. 30 hole.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 14 of 50 Rev J Date 5-24-14 13.3 TIT for second Turbine Inlet Temperature Use the J1 connector harness 790200 and insert the yellow wire into the connector pin 18 and the red wire into pin 19.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 15 of 50 Rev J Date 5-24-14 temperature like "125 IAT". On non-turbo engines the IAT in reality is the Carburetor temperature and displayed as “34 CRB.” 16.2 Carburetor Probe Installation (optional) Use the J1 connector harness 790200 and insert the yellow wire into the connector pin 5 and the red wire into pin 6. All wiring must be type K thermocouple wire.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 16 of 50 Rev J Date 5-24-14 18.1 Alternate method of installation keeping the original sensors in the aircraft operational The oil pressure sensor should tee off the oil pressure line feeding the original aircraft gauge or the oil pressure switch is removed and the sender is installed in that location. 19.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 17 of 50 Rev J Date 5-24-14 19.1 Adding a non-primary gauge to the system Requirements: All EDM930 and EDM960 units manufactured after Sep 15, 2012 have the EDM Configuration Editor built into a separate utility memory area of the EDM. To start the EDM Configuration Editor, hold the left two EDM buttons (STEP & LF) while powering up the EDM.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 18 of 50 Rev J Date 5-24-14 Master switch contactor Alternator F G B - BATT + Master switch Bus + Starter external shunt Starter solenoid Ammeter Configuration Master switch contactor Alternator F G B - BATT + + Master switch Bus external shunt Starter Starter solenoid Load Meter Configuration 20.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 19 of 50 Rev J Date 5-24-14 The EDM-900/930 receives signal from any installed FloScan Transducer with the following FloScan P/N’s embossed on to the top of the transducer. The K-Factor is marked on the side of the Transducer and on a white ticket. Wire per drawing 700744, Route the JPI wires along the existing wiring bundle lacing every foot.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 20 of 50 Rev J Date 5-24-14 22. Fuel Level Sender Wiring Types The EDM has the capability to interface to the aircraft’s fuel level system. It is also used to directly read the fuel senders for fuel calibration (no other equipment is needed).
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 21 of 50 Rev J Date 5-24-14 Example harness arrangement for an aircraft with resistive output senders Resistive Harness PN 790719-3
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 22 of 50 Rev J Date 5-24-14 22.3 Voltage Output Type Sender System Voltage output type systems usually have a convertor box. This is typical with the ‘Pennycap’ brand capacitive sender system. The Pennycap convertor box measures sender capacitance and converts it to a DC voltage output signal for the aircrafts fuel level gauge.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 23 of 50 Rev J Date 5-24-14 Getting Started…Collecting Fuel Level Calibration Data using the EDM as a meter. 1. With power off, hold in Button 4 (Button 1 being far left) and then turn on power. For each EDM monitored tank, create a paper table with the desired number of calibration points (2 to 5) and at what volume each will be.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 24 of 50 Rev J Date 5-24-14 22.4.1 After you have collected your data After you have collected your data…Entering / Editing Fuel Level Calibration Data The Fuel Table Editor is a spreadsheet type format allowing you to easily see the volume and related calibration values side by side. You can easily navigate through the cells to enter values. 1.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 25 of 50 Rev J Date 5-24-14 3. Tap USER when you see ‘Do you want to restore user table?’ (Note: tapping FACTORY causes the fuel table stored on the Key Card to over-write any previous user entries in the fuel table. Use FACTORY if you want to start from the original factory default). 4. Tap POINTS when you see ‘Do you want to edit the table?’. 5.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 26 of 50 Rev J Date 5-24-14 7. Tap TANK to select the next active tank and repeat previous step. Continue until all tanks ‘points’ have been set. 8. Tap TABLE. You see ‘Fuel Table Data’ ( White at top of screen) with a table. You may change any of the fuel levels in the left column except for empty. You will enter the readings taken previously on paper into the right column. 9.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 27 of 50 Rev J Date 5-24-14 1 and 2 again until the display (5 sec.) changes and you see FACTORY . At this point you will see MAIN = XX., adjust with the “Plus and Minus buttons. Tap next for AUX=XX and adjust. Tap button twice to finish and save. 24. GPS Interface Use the J4 connector harness 700708 labeled RS232 OUT TO GPS (white) and RS232 IN FROM GPS (gray).
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 28 of 50 Rev J Date 5-24-14 Manifold Pressure Calibration The manifold pressure must be calibrated to the ambient air pressure. Enter the current ambient barometric pressure. The engine must not be running. This setting is not the same as the altimeter setting that you receive from ATIS or Unicom. It will vary with field elevation. Use the chart below to calculate the MP FACTOR.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 29 of 50 Rev J Date 5-24-2014 Slick Magnetos engine engine Bendix Magnetos Connector to harness Connector to harness Slick 6000, 4000 series non-pressurized Bendix -20, -21, -200, 1200 series non-pressurized JPI 420815-1 JPI 420815-2 Mount sensor side of bracket towards magneto body Mount sensor side of bracket towards magneto body, positioned over the magnet armature Sensor ring
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 30 of 50 Rev J Date 5-24-2014 27. EDM-900/930 Specifications and Limitations The following parameters must be customized for the aircraft into which the EDM-900/930 is installed. Factory set limits or default values for EDM-900/930 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 31 of 50 Rev J Date 5-24-2014 28. EMI Radio Test and functional check: Even through the EDM-900/930 has been tested to DO-160E Section 20 (EMI) the installation itself could creates radio interference on specific frequencies. The following test is to insure that this does not exist.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 32 of 50 Rev J Date 5-24-2014 29.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 33 of 50 Rev J Date 5-24-2014 2 Ring Terminals 2 Screws and Nuts 6-32 X1/4" 1 Fiberglass tube 3/8” x 5” 29.6 Component Parts list for OIL Temperature probe (KIT 1250) 1 P/N 400509 OIL probe 1 AN900-10 crush washer 2 Ring Terminals 2 Screws and Nuts 6-32 X 1/4" 1 Fiberglass tube 3/8” x 5” 29.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 34 of 50 Rev J Date 5-24-2014 29.13 Components Parts list for pressurized RPM sensor P/N depends on Magneto make and model Slick 6000………………………….….P/N 420809 Bendix magneto 20, slick 600………P/N 420806 Bendix Dual ………………………….P/N 420808 Bendix 1200………………………….P/N 420807 30.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System END? Y END? Y Report No 908 Page 35 of 50 Rev J Date 5-24-2014 STEP exits the pilot programming mode. LF reenters pilot programming mode. 32. Programming the HP Constant You must adjust the HP Constant once for your aircraft. You must perform this adjustment in the air while the aircraft is in flight between 5,000 and 8,000 feet MSL. 1.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 36 of 50 Rev J Date 5-24-2014 35. Customizing Non-Primary Data (EDM900 only) You can customize – change or re-order non-primary data channels in the non-primary portion of the EDM display (non-primary values are displayed as text gauges without redline values – See Pilot’s Guide for more information).
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 37 of 50 Rev J Date 5-24-2014 37. Fine tuning the K Factor The K factor shown on the fuel flow transducer does not take into account your aircraft’s particular installation. Fuel hose diameters and lengths, elbows, fittings and routing can cause the true K factor to be different from that shown on the fuel flow transducer. You must use the following procedure to fine tune the K factor. 1.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 38 of 50 Rev J Date 5-24-2014 38. Adjusting the K Factor This procedure is different than for setting other parameters. 1. If you haven’t already done so, start the Pilot Program Mode by clearing all alarms by tapping step repeatedly, then simultaneously hold the STEP and LF buttons (for about five seconds), until you see the word PROGRAM, followed by ‘FUEL ? N’. 2.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 39 of 50 Rev J Date 5-24-2014 40. Trouble Shooting Diagnostic Testing on Startup and During Flight When your EDM is first turned on it tests internal components, calibration and integrity of the probes. During flight, probes are constantly checked for inconsistent or intermittent signals.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 40 of 50 Rev J Date 5-24-2014 NO 50MV Calibration error. Return unit to factory. NO 2.5V Calibration error. Return unit to factory. WARNCAL, WARNCFG Transient warning messages. Return unit to factory. HOBSERR The time of the most recent flight may not be reflected in the HOBBS meter. Return unit to factory. HOBSBAD The HOBBS data has been corrupted. Return unit to factory.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 41 of 50 Rev J Date 5-24-2014 42.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 42 of 50 Rev J Date 5-24-2014 43.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System J1 Report No 908 Page 43 of 50 Rev J Date 5-24-2014 For 4 and 6 cylinder installations yel 1 red 2 OIL temperature sensor yel 3 red 4 IND temperature sensor yel 5 red 6 Carb temperature sensor yel 14 red 15 OAT yel 16 red 17 TIT 1 sensor yel 18 red 19 TIT 2 sensor Remote temperature/voltage alarm light (option) gray 12 +12 or +24 vdc power lead red 13 Aircraft engine ground lead black 25 J
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 44 of 50 Rev J Date 5-24-2014
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System 44.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System Report No 908 Page 46 of 50 Rev J Date 5-24-2014 J4 (FF, GPS, AMP 2 ) White 1 Gray 2 Data out to GPS Serial communications Data in from GPS Main FF 700900-1, (201) -2 (231) white 4 red 5 OUT IN black 6 OUT White 12 Return FF 700900-1, (201) -2 (231) Optional IN NC 9 Right low fuel switch 10 11 13 White 14 Gray 15 5 optional Remote fuel flow alarm light (option) 6 Left low fuel switch FF2
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System 44.
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FAA Approved Installation Manual for the EDM-900 and EDM-930 Primary Engine Data Management System J-5 Harness with i2s fuel pressure sender.
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FAA Approved Installation Manual for the Report No 908 EDM-900 and EDM-930 Page 49 of 50 Rev J Primary Engine Data Management System Date 5-24-2014 45.
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FAA Approved Installation Manual for the EDM-900, PN 790000-A, EDM-930, PN 790000-C Primary Engine Data Management System 46. Appendix B ICA Report No 908 Page 50 of 50 Rev J Date 5-24-2014 Refer to: Supplement No: 905-01 Revision: E or later Check the web page, jpinstruments.