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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 4 of 30 

        Press & hold 'STEP' and 'LF' keys simultaneously until you see 
                  'PROGRAM' and  'RATE 4'.  (Note: Bargraph disappears) 

 

        Now press & hold 'STEP' and 'LF' simultaneously again until you see 
                  'ORIG. TIT' and 'ORIG. T-N'. 

 

        Tap 'LF' once to change to 
                  'ORIG. T-Y'. 

 

        Tap 'STEP' once to display 
                  'CAL TIT' and 'TIT+  0'. 

 

        This is the correction added to (+), or subtracted from (-) the EDM reading for TIT (at high temperatures). 

 

        Hold in 'LF' to raise the correction, or tap 'LF' to lower it. 

 

        For example, if the EDM read 100 less than the ship's TIT, 
        Then hold in 'LF' until you see 
                  'TIT+100'. 

 

        Adjust the correction slightly if a difference between the EDM 
        and the ship's gage still exists. 

 

        Now tap 'STEP' once to complete setup. 
 
 

 
4)  CYLINDER HEAD TEMPERATURE PROBE (CHT), BAYONET

 

 

The Bayonet probe 5050-T has the 3/8-24 adaptor boss as part of the probe and is screwed into the base of the 
cylinder (See fig-2).  The bayonet probe has a screwdriver slot to facilitate tightening.  

 

NOTE: Required original equipment that has a Red Line may not be replaced by the EGT-701 TIT or CHT installation.  
This includes but is not limited to all aircraft with adjustable cowl flaps and on aircraft with placards on the instrument 
panel showing a climb air speed, for cooling, different from the best rate of climb air speed. 

 

If a previously installed TIT, CHT or EGT is listed 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 cylinder head temperature gauges utilize a 

bayonet

 or 

screw-in

 resistive type probe that 

occupies one of the bayonet sockets.  This probe is not compatible with the thermocouple probes required for the 
EGT-701.  
 
The spark plug gasket probe, P/N M-113, replaces the standard copper spark plug gasket on one spark plug.  The 
plug chosen, upper or lower, should be the one that provides the best correlation with the other temperature probes.   
Due to the spark plug location, the gasket probe may read 25

o

F higher or lower than the factory probe.   The probe is 

usually placed on the plug that receives the most direct cooling air. After many removals the probe may be annealed 
for re-use. Heat and quench in water.  At additional cost an adapter probe P/N  M-113-3/8 is available that permits the 
factory CHT probe and a JPI probe to fit the same bayonet location. 
 
 

6) INDUCTION AIR TEMPERATURE PROBE (IAT) / CARB TEMP

 
Induction Air temperature probe, IAT, is installed just after the inter-cooler (OUT) and the Compressor Discharge 
Temp (CDT) just before the inter-cooler (IN).  The probe is an EGT probe and installed the same way as an EGT 
probe.  A large clamp is supplied to fit around the airport leaving the inter-cooler or a 1/8 NPT is available.  IAT option 
is displayed as an independent digital temperature like "125 IAT".   On non-turbo engines the IAT in reality is the 
Carburetor temperature and displayed as “34 CRB”. 
 
 

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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