JPInstruments Primary/TSO Instrument Order Work Sheet Rev. IR 04/2016 Marki0404ng and Configuration Requirements JJ
Marking and Configuration Requirements
for Certified Aircraft JPInstruments will configure your EDM to the range generated. A configuration file for a primary instrument limits, markings and hardware outlined for the specified can only be generated or changed by JPInstruments. If aircraft listed on this form. All data will be provided by any of the information provided on this form is wrong, the pilot/owner and the mechanic and must be verified there will be a reprogramming fee to change the for accuracy. The data must match the POH/AFM and configuration. IMPORTANT: The information in this reflect any changes required by any AD’s, Supplements document must be verified for accuracy and match the or STC’s. Your limits and marking information may be aircraft’s hardware and POH/AFM marking cross-checked against the instruments currently requirements. It is up to the installer/aircraft owner to mounted in your aircraft panel. verify applicability of their aircraft with the STC AML for This document must be completed and signed by the the Primary Instrument they wish to install. Applicability aircraft owner AND by an FAA certificated mechanic. is assumed to have been verified by submission of this This form should then be delivered to JPInstruments, at order form. Provide a copy of your original AFM/POH which time a configuration file for a specific EDM will be and STC’s along with corresponding AFMS.
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If data supplied in this document is incomplete or missing, we cannot process your order.
Aircraft Information Example
Customer Name Peter Pilot
Customer Phone # 555-555-5555
FAA Certificated A&P Mechanic's Marty Mechanic Name FAA Certificated A&P Mechanic's 555-555-5555 Phone # A&P Mechanic's FAA Certificate # 12345678
Aircraft Make & Model Cessna, 182R
Engine Manufacturer & Model Continental, O-470U
Aircraft Registration Number & N5555H, T18208223 Serial # Aircraft Year 1969
# of Cylinders & Max Engine 6, 230 HP Horsepower Tachometer Markings (Primary) Configured by: Verified by: Color Range Date: Date: Example Red Red, 2700
Green Green, 2000 to 2500
Yellow
White
Blue
Clear/Black
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EGT Markings: If markings are not specified in the POH/AFM, write “No Limits”
Configured by: Verified by: Color Range Date: Date: Example Red No Limits
Green
Yellow
Clear/Black
CHT Markings (Primary): N/A Configured by: Verified by: Color Range Date: Date: Example Red Red, 460°F and Above
Green Green, 200 to 400°F
Yellow Yellow, 400 to 460°F
Clear/Black
Manifold Pressure Marking: N/A Primary Gauge Non-Primary Gauge Note: MAP is used for calculating % horsepower so all primary instruments will get MAP. s
Configured by: Verified by: Color Range Date: Date: Example Red Line
Green Green, 15 to 25
Yellow
Clear/Black
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If markings are not specified in the POH/AFM, default values will be used. Amps: A 100 Amp/50mv shunt is provided in the kit and must be used in place of the existing shunt.
Is the Amps a measurement of the Alternator output current or the Battery current (check one)? Charge/Discharge Load Meter
Configured by: Verified by: Color Range Date: Date: Example Red Line Red, 50 Amps
Green
Yellow Requirements for Certified Aircraft
Fuel Pressure Markings : N/A Primary Gauge Non-Primary Gauge (If F.P. is optional)
Aircraft Fuel Pressure configuration:
Fuel Pressure monitored at the Fuel Pump (Unmetered). Turbocharged system and the Fuel Pressure is referenced to the Upper Deck Pressure (you will get an upper deck referenced transducer). Metered Fuel Pressure monitored at the Flow Divider. Gravity Feed system with no Fuel Pump (Fuel Pressure can NOT be monitored). Fuel Pressure will NOT be monitored. Configured by: Verified by: Color Range Date: Date: Example Red Line Red, 14 PSI
Green Green, 9 to 14 PSI
Yellow Red, 9 PSI
Oil Pressure Markings (Primary) Configured by: Verified by: Color Range Date: Date: Example Red Line Red, 100 PSI
Green Green, 40 to 90 PSI
Yellow Yellow, 25 PSI
Clear/Black
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Oil Temperature Markings (Primary) Configured by: Verified by: Color Range Date: Date: Example Red Red, 240°F
Green Green, 65 to 200°F
Yellow Yellow, 200 to 240°F
Clear/Black Optional Functions
Configured by: Verified by: Volts Date: Date:
Specify 12-Volt or 24-Volt system: (check one)? 12V 24V
Carb Temp Markings: N/A Configured by: Verified by: Color Range Date: Date: Recommended Limits Red
Green Green, 41 to 70°F
Yellow Yellow, 5 to 41°F
TIT Markings : N/A Primary Gauge Non-Primary Gauge
Configured by: Verified by: Color Range Date: Date: Example Red Red, 1650°F
Green Green, Below 1650°F
Yellow
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Volts 2: (check one)? YES NO
Example Specify 12-Volt or 24-Volt system: ______12 volts
A 100 Amp shunt is provided in the kit. Amps 2: (check one)? YES NO You will get a second shunt for the second Amp reading.
Is the Amps a measurement of the Alternator output current or the Battery current (check one)? Charge/Discharge Load Meter Color Range Example Red Line Red, 50 Amps
Green
Yellow
Fuel Qty. Gages: YES NO If NO, please complete “Full Fuel Level (Usable)” so that we can set up the fuel totalizer for you.
Important Information: The EDM can provide fuel level readings for straight and level flight and is only as accurate as the sending units. When calibrating the EDM to the fuel tank, the aircraft must be in flight attitude. The EDM cannot correct for inconsistent or non-repeatable readings from a Resistive Fuel Level Sensor. Unfortunately, many Resistive Fuel Level Sensors (and in some cases even new units) exhibit these problems. If you find inconsistent or inaccurate fuel level readings (due to a defective Resistive Fuel Level Sensor), you must have the sensor replaced or repaired. Read the “WARNING” in the EDM Installation Manual. JPI can display 4 Tanks maximum. If you have 6 Tanks, you will have to retain your two tip tank gauges.
Probe Type: Switch Operated Fuel Gauges? Fuel Tank Pennycap, Gull, (check one)? YES NO Resistive, CIES Full Fuel Level Name Example Frequency or (Usable) (9 Characters Max) CIES voltage output. L Main, Res, 40 gal
R Main, Res, 40 gal
Center, Front, Aft 20
Aux, Res, 20 gal
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Additional IAT TIT Clamp On CARB TEMP CDT Options YES YES Screw In YES YES $195 each (x2 for twins) Fill in markings boxes above (Page 5) Fill in markings boxes above (Page 5) Optional l Functions
Magneto Part No. Magneto Brand Magneto Type or Other Tach Generator
Part no. Left ______Bendix Slick Pressurized Dual Teledyne Cont. Motors Non - pressurized UMA Part no. Right ______Light Speed Other______
Do you currently have a Tanis heating system occupying your cylinder head temperature pockets?
NO YES, If yes JPI Bayonet probes must be used for CHT and an alternate Tanis heating system will have to be used.
Fuel Flow: Primary Gauge Non-Primary Gauge Note: F/F is used for calculating % horsepower
Configured by: Verified by: Color Range Date: Date: Example Red Red line, 25gph
Green Green, 3 to 25gph
Yellow
White
Clear/Black Clear/Black, 0 to 3gph
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Ordering an EDM: 900 930 960
If ordering an EDM-960, where will you install the DAU’s? Engine Firewall_____is standard with 10ft. leads. DAU installation in the cockpit_____requires 20ft. leads at an additional cost.
Note: Airframe Hobbs and Tach time will be entered during installation and programming by the installer using the Factory Programming function. Non-primary gauge options are also installer/customer configurable and will not be displayed on initial power up. Use EDMConfig to enable. Fuel quantity gauges will be Red X’d until the fuel tables have been completed and saved in the EDM.
Fuel flow: Please answer the following questions for the correct fuel flow transducer.
Is your fuel system gravity fed? NO YES Is your engine carbureted with an engine driven pump? NO YES Is your engine fuel injected NO YES Do you have a Pressure Carburetor with a fuel return? NO YES
Thank you for your order. JPInstruments: Fax (714)557-9840, (714)557-3805, (800)345-4574
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We (the undersigned) have entered and verified all the limits, markings and aircraft configurations listed in this worksheet to be correct and taken from the information in the aircraft’s POH/AFM which includes any changes mandated by any AD’s, Supplements and STC’s. We understand there is important information in the Installation and Operating Instructions that must be read before installing the EDM900/930/960 and flying the aircraft.
**** Verified that range and configuration information is complete and accurate ****
______Owner/Pilot’s Printed Name Owner/Pilot’s Signature Date
______Mechanic’s Printed Name Mechanic’s Signature Date
Check box to verify that you are sending a copy of the original AFM/POH and any STC’s with corresponding AFMS that affect the power plant instrument markings.
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