J.P. Instruments EDM 960 Twin Primary Installation Manual User Manual

Page 28

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FAA Approved Installation Manual for the EDM-960 system Report No 909

Primary Engine Data Management System Page 28 of 46 Rev D

Date 2-6-2014

33. EDM-960 system Specifications and Limitations
The following parameters must be customized for the aircraft into which the EDM-960 system is installed.

Factory set limits or default values for EDM-960

1. TIT 1650 F

TSO-C43

2. CHT 450 F

TSO-C43

3. Oil Temp Low 90 F

TSO-C43

4. Oil Temp HI 230F

TSO-C43

5. Oil Press low 15 psi

TSO-47

6. Oil Press Hi 100 psi

TSO-47

7. Vacuum 0- 15”hg

TSO-47

8. RPM 2700 Limit and range

TSO-C49

9. RPM set to cyl 6

TSO-C49

10. Map 32 In hg HI

TSO-C45

11. Map setting 29.90 In Hg

TSO-C45

12. Fuel Pressure Hi 35 psi Injected

TSO-47

13. Fuel Pressure Lo 15 psi Injected

TSO-47

14. Fuel Pressure Hi 8 psi Carb

TSO-47

15. Fuel Pressure Lo .5 psi Carb

TSO-47

16. Fuel Flow 24 GPH

TSO-C44

17. K-factor 29.99
18. Carburetor filter smoothing 1
19. Ammeter configuration (load or charge-discharge). Load NON TSO
20. HC-120 (% of HP)

NON TSO

21. Fuel Level Resistive/Capacitive

TSO-55

22. Low fuel 10 Gal
23. Low time 45 Min
24. Main tank 75 gallons
25. Aux tank 0
26. GPS set at GARMIN
27. Diff 500 degrees

TSO-C43

28. CLD 60 degrees per minute

TSO-C43

29. Amps limit 100 amps

NON TSO

30. Record time, 6 sec intervals

NON TSO

31. Tach Time based on cruise RPM setting of 2400 true

NON TSO

During start-up the EDM may reset (typical on 14 vdc systems). This is normal due to extremely low battery voltage
due to starter amperage draw. The conditions and test required for TSO approval of this article are minimum
performance standards. It is the responsibility of those desiring to install this article either on or within a specific type or
class of aircraft to determine that the aircraft installation conditions are within the TSO standards. The article may be
installed only if installation of the article is approved by the Administrator. The functions of Volts, Amps, and Horse
Power were tested to DO-160D and DO-178B, but not TSO’d since no TSO exist for these functions. Deviation granted
for TSO-C49b to include digital display and sensor. All TSO required probes, transmitters and sensors also tested to
DO-160D.

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