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Created by Liliana Andrea Cardona Medina
over 5 years ago
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| Question | Answer |
| On the ATR600, the IESI (Integrated Electronic Stand-by Instrument) | Combines the Stand-By Horizon, the Stand-By Airspeed Indicator, the Stand-By altimeter and the Stand-By Compass |
| The two CAC (Core Avionic Cabinet) | Control and authorize the operation of A/C avionic systems only |
| The Yellow Arrow on the Speed Scale indicates | The current Aircraft Speed |
| The Altitude Selection Bug is set | Using the ALT SEL rotary selector on the FGCP |
| Where is the Airspeed, Altitude and Vertical Speed information located | On the EFIS |
| The two Attitude and Heading Reference Systems (AHRS) provide the following data | Pitch, roll, heading and ground speed |
| PROP BRK blue light is illuminated on the engine start panel and is displayed on the EWD when | Engagement or disengagement conditions are met |
| Each DC starter/generator during engine start acts as an electric motor driving HP via | Reduction Gearbox |
| Is the fuel heated to prevent icing | No, it is not necessary |
| The Reduction GearBox drives | The ACW generator, the fuel HP pump, the propeller and the associated control accessories |
| What is the important thing that you need to do before opening the Cockpit Emergency Hatch | It is important to disconnect the electrical connector and the water drain |
| During landing, when does the idle-gate move rearward to the Ground Idle position | Only after all gear shock absorber are compressed |
| "A ""GATE"" prevents PL angle reduction below FI" | At take-off as soon as both main landing gears absorbers are released |
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