- General Electric CF34-10E high bypass turbofan
- FADEC
- 18,500 lbs thrust
- twin spool
- 3 stage low pressure axial booster driven by a 4 stage low pressure turbine (N1)
- 9 stage axial flow compressor with variable inlet guide vanes driven by a 1 stage high pressure turbine (N2)
- single-stage wide chord fan
- Cold section
- Accessory gearbox (AGB)
- Combustion Liner and stage 1 nozzle assembly
- High pressure turbine (HPT) / low pressure turbine (LPT)
| Position | Annunciator |
| N1 gauge | OFF |
| FAIL |
| above N1 gauges | TO-1/2/3 |
| FLEX TO-1/2/3 |
| between N1 gauges | ATTCS |
| RSV |
| below N1 gauges | REV |
| ITT gauge | FIRE |
| IGN A |
| IGN B |
| IGN A B |
| IGN OFF |
Engine Fuel System
Engine Oil System
Engine Start System
Ignition System
Categories: Embraer 170/190 | Engine
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