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FAA APPROVED    INSTALLATION MANUAL FOR THE EGT-701  Report 103  

 
INSTALLING THE EGT-701 SCANNER®

                              

1/20/09 

Rev-E       Page 20 of 30 

 

 

 

Fuel Flow Units (Fuel Flow Option) 

Selects the units in 

all

 parameters where fuel quantity or fuel rate is displayed. If you change this parameter, it does 

not

 change the 

numerical value of the fuel tank capacity. You must do this manually. For example if you change from Gal. to Lbs., the tank 
capacity will be interpreted as 50 Lbs. rather than 50 gallons; the EGT-701 will not convert 50 Gal to equivalent pounds. 
 

Main Tank Capacity (Fuel Flow Option) 

Enter the total capacity of the main tanks in the fuel flow units selected. If you have tank tabs (but no auxiliary tanks) and 
sometimes fill only to the tabs, set the main tank capacity to the capacity up to the tabs. 

Auxiliary Tanks (Fuel Flow Option) 

If you do not have auxiliary tanks or tank tabs, answer “No.” If you answer yes, you will be asked to input the capacity of the 
auxiliary tanks in the fuel flow units selected. If you have tank tabs and sometimes fill only to the tabs, set the auxiliary tank 
capacity to the difference between full tank capacity and tab capacity. 

Low Time Alarm Limit (Fuel Flow Option) 

Select the value of the time remaining, in minutes, that triggers the alarm. Time remaining is calculated at the current fuel flow 
rate. 

Low Fuel Alarm Limit (Fuel Flow Option) 

Select the value of the fuel remaining, in the selected fuel flow units, that triggers the alarm. Fuel remaining is calculated at the 
current fuel flow rate. 

Carburetor? (Fuel Flow Option) 

Different response filters are used depending on whether your engine is carbureted or fuel injected. The filter for a carbureted 
engine has a slower response time to reduce sudden fluctuations in readings. 

 

29) Troubleshooting 

a) 

A missing column in the display on start up

 indicates that the diagnostic routine has found an open 

wire or probe with a poor connection. The error message will indicate which channel to examine. 

b) 

A missing column in the display during flight 

indicates a widely varying or erroneous temperature 

value. The probe is deleted from the indexing to prevent false alarms. 

c) 

Start up OPEN PRB message.

 If one of the temperature probe circuits is open, the display indicates 

OPEN PRB followed by one of these messages: EGT 1, EGT 2, EGT 3, EGT 4, EGT 5, EGT 6, EGT 7, 
EGT 8, EGT 9, CHT 1, CHT 2  , CHT 3, CHT 4, CHT 5, CHT 6, CHT 7, CHT 8, CHT 9, OIL, IND, OAT, 
TIT. Check the connector at the instrument and verify that a female pin is not recessed in the connector. 
Check the crimps where the probe is connected to the wiring harness. 

d) 

A negative reading

 (- in front of the number) indicates reverse polarity on the red and yellow 

thermocouple wire to probe. 

e) 

Ohmmeter check.

 Remove the connector from the rear of the instrument and measure the resistance 

of the probe lead pairs. The reading should be about 10 ohms. At the connections between the probe 
and the wiring harness in the engine compartment, the resistance should read about 2 ohms. 

f) 

All readings varying rapidly.

 Verify that the Instrument is 

grounded at the engine block

 for single 

engine installations. If an adapter probe is being used insure that it is screwed in tightly and grounded. 
Remove the factory original probe that is in the adapter and note if problem is resolved. If so an ohm 
ground exists between the engine and the adapter probe. 

Содержание EGT-701

Страница 1: ...TING INSTRUCTIONS 14 17 INDICATOR INSTALLATION RECORD 16 18 ENGINE OPERATION 16 19 LIMITATIONS OPERATION 16 20 COMPONENT PARTS LIST FOR EGT PROBE 17 21 COMPONENT PARTS LIST FOR CHT PROBE 17 22 COMPONE...

Страница 2: ...ll the necessary parts prior to beginning the installation g Do NOT use aluminum fittings with the FXT 201 or FXT 231 fuel flow transducer h Write down the K factor engraved on the side of the fuel fl...

Страница 3: ...nal distance of 2 to 4 inches from the exhaust flange is recommended See fig 2 If the recommended distance is impractical because of obstructions slip joints or bends in the exhaust system then positi...

Страница 4: ...d on the aircraft equipment list as Optional Equipment or not listed at all it may be replaced by the EGT CHT SCANNER 5 CYLINDER HEAD TEMPERATURE PROBE CHT SPARK PLUG GASKET Most factory installed cyl...

Страница 5: ...il temperature gauge and sensor must remain Check for oil leaks and safety wire before first flight Oil Probe Location Alternate Oil Probe Location Lycoming Engines front view Continental Engines The...

Страница 6: ...0505 C is installed by removing the 3 8 or 1 8 pipe plug located on the front of the engine inline with the push rods This oil galley feeds the valve lifters Insert the JPI 1 8 NPT probe supplied with...

Страница 7: ...SIDE AIR TEMPERATURE PROBE OAT Install the OAT probe P N 400510 in the airframe manufactures recommended location If this is not possible it is recommended that the OAT probe be placed in clean airflo...

Страница 8: ...it away from any hot exhaust pipes The hose support or fitting may be on the input or output line of the fuel flow transducer Secure the end of the transducer to any convenient point on the engine wit...

Страница 9: ...701 is supplied with special Teflon insulated Chromel Alumel factory assembled wiring harness configured for the correct number of cylinders The wire harness is marked E 1 EGT 1 C 1 CHT 1 etc TIT is m...

Страница 10: ...with a crimp on ring terminal provided The ring terminals may be crimped with a service type tool however AMP part number 48518 crimp tool is recommended Verify the quality of each crimp with a sharp...

Страница 11: ...he airframe or engine since abrasion will destroy this high temperature wire Connect the JPI RPM sensor to the wiring harness using the 3 pin connector supplied Secure thermocouple wires along the rou...

Страница 12: ...his MP FACTOR by the altimeter setting that you receive from ATIS or unicom For example if the field elevation is 1700 ft and the altimeter setting is 30 1 the MP FACTOR is 0 9400 from the table Multi...

Страница 13: ...non pressurized engine Mount sensor side of bracket towards magneto body Bendix 20 21 200 1200 series non pressurized JPI 420815 2 Connector to harness engine Connector to harness Slick 6000 4000 ser...

Страница 14: ...F Depress the LF button will change the value of the rate or Oat in o C or o F Exit by Depressing STEP If the EGT 701 buttons are not depressed for 10 minutes the system will start scanning automatic...

Страница 15: ...30 system mounts in a 3 125 inch instrument panel hole in either a portrait or landscape position depending on panel hole location By holding the Step button white for approx 10 seconds and arrow will...

Страница 16: ...01 SPECIFICATIONS and LIMITATIONS OUTPUT FUNCTIONS ALL OPTIONS FACTORY LIMITS EGT Exhaust Gas Temp K Max limit 2500o F 1650 o F CHT Cylinder Head Temp J K Max limit 600o F 450 o F TIT Turbine Inlet Te...

Страница 17: ...als 23 Components Parts list for OAT probe PN 1220 1 P N 400509 OAT probe 2 Ring Terminals 2 Screws and Nuts 6 32 X1 4 1 Fiberglass tube 1 2 X 4 24 Components Parts list for Manifold pressure sensor p...

Страница 18: ...r example I9 00 7 Tap STEP for next digit I9 00 8 Tap or Hold LF to change flashing digit I8 00 9 Tap STEP for next digit I8 00 10 Repeat steps 7 and 8 for the remaining two digits 11 Verify the K fac...

Страница 19: ...H BAT Battery high voltage limit set in 0 5 volt increments 8 5 L BAT 30 0 L BAT Battery low voltage limit EGT DIF 30 DIF 990 DIF EGT difference limit set in 10 increments CHT HI 90 H CHT 500 H CHT C...

Страница 20: ...ed depending on whether your engine is carbureted or fuel injected The filter for a carbureted engine has a slower response time to reduce sudden fluctuations in readings 29 Troubleshooting a A missin...

Страница 21: ...arburetor engines at normal cruise display a DIF of 125 to 175o F spread between cylinders Injected engines at normal cruise display a DIF 50 to 90o F spread between cylinders All cylinders are measur...

Страница 22: ...FAA APPROVED INSTALLATION MANUAL FOR THE EGT 701 Report 103 INSTALLING THE EGT 701 SCANNER 1 20 09 Rev E Page 22 of 30 FIG 1...

Страница 23: ...and tighten the clamp hex screw until you can just remove the instrument from the bracket The Mounting bracket is then placed behind the instrument panel hole and screwed 6 32 x screws in place using...

Страница 24: ...FAA APPROVED INSTALLATION MANUAL FOR THE EGT 701 Report 103 INSTALLING THE EGT 701 SCANNER 1 20 09 Rev E Page 24 of 30 EDM 730 830 Layout...

Страница 25: ...FAA APPROVED INSTALLATION MANUAL FOR THE EGT 701 Report 103 INSTALLING THE EGT 701 SCANNER 1 20 09 Rev E Page 25 of 30...

Страница 26: ...FAA APPROVED INSTALLATION MANUAL FOR THE EGT 701 Report 103 INSTALLING THE EGT 701 SCANNER 1 20 09 Rev E Page 26 of 30...

Страница 27: ...FAA APPROVED INSTALLATION MANUAL FOR THE EGT 701 Report 103 INSTALLING THE EGT 701 SCANNER 1 20 09 Rev E Page 27 of 30 FIG 6...

Страница 28: ...FAA APPROVED INSTALLATION MANUAL FOR THE EGT 701 Report 103 INSTALLING THE EGT 701 SCANNER 1 20 09 Rev E Page 28 of 30 Fig 7...

Страница 29: ...FAA APPROVED INSTALLATION MANUAL FOR THE EGT 701 Report 103 INSTALLING THE EGT 701 SCANNER 1 20 09 Rev E Page 29 of 30 Fig 9...

Страница 30: ...e are no field adjustments and or calibration requirements for the EDM 700 730 series instrument after initial installation ICA is not required Maintenance of nonfunctioning or malfunctioning componen...

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