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EGT-100 Exhaust Gas Temperature Indicator 

Page 3 of 11

 

 

Aerospace Logic Inc. 

3150 Ridgeway Drive, Unit #43, Mississauga, Ontario, L5L 5R5, CANADA 

Tel. (905) 569-3887 | Fax. (416) 352-5854 | Email. sales@aerospacelogic.com 

www.aerospacelogic.com 

EGT-100 Operations & Installation Manual – Ver. 1.9 – June 5, 2003 

 

3. Installation

 

 
Ensure that the thermocouple probes have been installed PRIOR to installing the 
instrument. 

See Probe Installation for full details (Section 6).

 

 
The EGT-100 will fit any standard 2 ¼” aircraft mounting hole.  Place the 
instrument in the hole from the rear of the panel and then attach it with the four 
screws provided. If you need to replace the screws, ensure that the threads do 
not penetrate the instrument more than ½”. Screws that penetrate the instrument 
further will cause severe damage to the instrument. 
 

WARNING 

 

This instrument is a highly sensitive and accurate instrument, however without 
proper wiring and connections it is possible to induce temperature reading errors. 
 

Please read and follow all instructions carefully to ensure proper operation.

 

 
The instrument has been software calibrated and never needs recalibration 
provided no wiring modifications are made at installation time. 
 
Now connect the supply and dimmer wiring. These wires may be trimmed to any 
desired length. 
 

RED

   

Master switched 14/28V bus (Instrument is internally fused) 

BLUE 

 

28V Dimmer control (if required) 

WHITE

  

14V Dimmer control (if required) 

 

NEXT CONNECT THE BLACK WIRE TO A GROUND POINT ON THE ENGINE 

 

BLACK

 

Aircraft supply ground connected on engine ground point. 

 
Wherever possible ensure that connection to the probe ends is made on the 
cockpit side of the firewall. If this is not possible ensure that the junction between 
the signal wiring from the instrument and the probe is in the coolest possible 
location in the engine compartment. 
 
Next connect the probe signal wiring. These wires are the red/yellow twisted 
pairs. Each cylinder is identified by a color tag on the specific twisted pair.  
 

Do NOT

 un-twist these cable pairs. They are designed to reduce signal noise.  

 

Do NOT

 trim the thermocouple probe wires under any circumstances. 

 
Where possible 

do NOT

 strap the signal wiring to other aircraft wiring. 

 

Trim

 these wires to length if necessary, but 

do not

 remove the color code tags. 

Summary of Contents for EGT-100 Series

Page 1: ...0 Exhaust Gas Temperature Indicator This instrument is a complex precision instrument manufactured to exceed Airborne Equipment Standards DO 160D DO 178B and TSO C43c standards In order for your instr...

Page 2: ...ensure that it is functioning correctly In turn the main processor validates the independent monitoring processor Any failure detected in either processor and your instrument display will be shut down...

Page 3: ...ure proper operation The instrument has been software calibrated and never needs recalibration provided no wiring modifications are made at installation time Now connect the supply and dimmer wiring T...

Page 4: ...e purchased a complete instrument and probe kit appropriate connectors for interconnection of the signal wires and probe leads are provided If you have purchased only the instrument NO connectors are...

Page 5: ...Page 5 of 11 Aerospace Logic Inc 3150 Ridgeway Drive Unit 43 Mississauga Ontario L5L 5R5 CANADA Tel 905 569 3887 Fax 416 352 5854 Email sales aerospacelogic com www aerospacelogic com EGT 100 Operatio...

Page 6: ...the setup mode the display bar will remain blank The CYL digit and the four digit display shows the parameter value and type as per the enclosed instructions In order to set the manufacturer specified...

Page 7: ...ch once to the S position and release The low limit will now be saved and applied to all cylinders The display will move to the next parameter H High Temperature Limit Set The high temperature limit s...

Page 8: ...splay the STEP message for approximately five seconds before starting the step process Once started it will step through all cylinders When the last is reached it will revert back to the first 1 Displ...

Page 9: ...nt and should be used during leaning and normal operations Leaning in the automatic mode ensures that no cylinder is overheated during the process If the instrument is switched from the automatic mode...

Page 10: ...Section Thermocouple Signal Wire Junction Where possible plan the installation such that the junction between the thermocouple and signal wire takes place on the cockpit side of the firewall If this i...

Page 11: ...for thermocouple sensor linearity Minimum 256 times measurement validation before display Operating Temperature 15 C to 55 C 5 F to 131 F Power Consumption 370mA Max daytime operation 50mA Min nightt...

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