Term
| Autopilot Controls which 2 trim motors |
|
Definition
|
|
Term
| What CAS will indicate pusher safe mode |
|
Definition
|
|
Term
| Hydraulic CAS in the air for |
|
Definition
| Low Pressure or pump operating more than 2 minutes |
|
|
Term
| Hydraulic CAWS on the ground for |
|
Definition
| Pump on in the air 6 times in an hour |
|
|
Term
| Gear warning horn will sound when gear is up and |
|
Definition
- Flaps greater than 15 - Speed less than 130 and PCL Idle - Radar Altitude less than 200' and power set less than 10 psi |
|
|
Term
| Failure of the hydraulic system, Nitrogen accumulator holds pressure for |
|
Definition
|
|
Term
| 4 Systems used for Air/Ground determination |
|
Definition
- LH main gear proximity switch - RH main gear proximity switch - Radar Altimeter - Calibrated airspeed |
|
|
Term
|
Definition
| Passenger door and over wing exit |
|
|
Term
| When should the inertial separator be open |
|
Definition
| Icing or F.O.D. conditions |
|
|
Term
| 3 pilot inputs for the FCU |
|
Definition
|
|
Term
| Systems inoperative when MOR is in use |
|
Definition
| Ng Governor, Nf Governor, Torque limiter |
|
|
Term
| PCL operations past idle detent prohibited |
|
Definition
| Engine off, in air, or using MOR |
|
|
Term
|
Definition
|
|
Term
| Overspeed Governor limits Np to |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
| Bleeding off Py air from the FCU |
|
|
Term
| Auto fuel balancing turns on automatically when there is a difference of |
|
Definition
|
|
Term
| Takeoff prohibited with fuel imbalance of |
|
Definition
|
|
Term
| Red oil quantity CAS will illuminate when |
|
Definition
| Low oil quantity and engine is off |
|
|
Term
| The oil cooler door is connected to |
|
Definition
|
|
Term
| The torque limiter limits torque by |
|
Definition
| Bleeding off Py air from the FCU |
|
|
Term
| During engine start, starter will automatically disconnect when |
|
Definition
|
|
Term
| Igniters will come on automatically when |
|
Definition
| ITT less than 500 C and Ng greater than 10% |
|
|
Term
| Reason for a fire detector CAS |
|
Definition
| Fire detection system inoperative |
|
|
Term
| What brings the propeller to a feathered pitch |
|
Definition
|
|
Term
|
Definition
OAT > 0°C - standby 0°C <-> -16°C - 45/45/off > -16°C - 90/90 |
|
|
Term
|
Definition
|
|
Term
| What determines how much fuel is delivered to the engine |
|
Definition
|
|
Term
|
Definition
| Tank less than 20 gallons |
|
|
Term
|
Definition
| 500 to run ground operations. 1000 for engine start |
|
|
Term
| What bus automatically shuts off with a Gen 1 failure |
|
Definition
- Non-essential Bus - Cabin Bus - Gen 1 Bus |
|
|
Term
| ACS will automatically shut down for |
|
Definition
| Overpressure or over Temperature in the system |
|
|
Term
| Air used to inflate de-ice boots supplied from |
|
Definition
| Compressed air from the engine |
|
|
Term
| What systems will cause the Takeoff Configuration CAS to illuminate |
|
Definition
Flaps not set to 15 or 30 Trim not set Condition Lever not in Flight Idle |
|
|