J.P. Instruments EDM 960 Twin Primary Installation Manual - Manual (Page 3)

FAA Approved Installation Manual for the EDM-960 system Report No 909
Primary Engine Data Management System Page 3 of 46 Rev D
Date 2-6-2014
3. Instrument Marking
The TSO label on the instrument is marked as to the instrument’s configuration and DO-160 and DO-178 testing.
The EDM-960 system consists of one (1) EDM-930 Display P/N 790000-C-120, two (2) EDM-950’s P/N 790000-B-
(xxx), two RADs P/N-790749, and all related wiring and connectors.
Model Number / Part Number Description
EDM-930 PN 790000-C- [120] Display only with TFT (liquid crystal) Type
EDM-950 PN 790000-B- [XXX] DAU (Data Acquisition Unit)
PN 790749 RAD (Remote Alarm Display)
PRIMARY INSTRUMENTS NON-PRIMARY INSTRUMENTS
EGT FUEL
FLOW
Remote
Display
EGT
4-9
Time to
empty
OAT, AMP, VOLTS, CARB, IAT
CHT FUEL
PRESS
TIT OAT
CARB
Required to
WP
Shock Cooling
Lean Find
OIL TEMP RPM CDT Volts
Amps
Reserve at
WP
Differential EGT
OIL
PRESS
MAP FUEL
Quantity
IAT MPG Percent of HP
Example PN 790000-(X)-(XXX) (X) denotes EDM-900 or EDM-930, (XXX) denotes Part Number for a specific
aircraft with or without and engine STC. Each PN is specific to a Make and Model Aircraft with or without STC.
In which the information is gathered from the Aircraft POH or STC Data sheet.
Aircraft type
w/engine STC No. if
applicable
JPI assigned Data Base Part No. per
Limits found in the POH or engine STC
for a specific aircraft
Part No. Displayed on 930
RAD at Start-up or 900
message area
Cessna 182-P 534 790000-X-534
Cessna 182-P, STC12345NW 875 790000-X-875
4. Primary TSO Label