350 Systems Validation Flashcards

1
Q

Describe the operation of the vent flap?

A

The purpose of the vent flap is to prevent opening of the main cabin door while the aircraft is pressurized

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2
Q

Where is the baggage weight placard located?

A

Aft bulkhead

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3
Q

What must the status of the microwave switch be during critical phases of flight?

A

Off

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4
Q

Where is the therapudic oxygen mask located?

A

Aft pyramid, bottom drawer

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5
Q

The radio altitude is not displayed, and when Manual Arm is selected, the spoilers do not deploy. What is the cause?

A

No valid radio altitude. Possibly due to the antenna positioned over sloping terrain

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6
Q

Climbing through FL350 the stick pusher activates inadvertently. What action is taken?

A

MSW ………(PF)…… Press&Hold

Refer to inadvertent pusher activation QRC.

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7
Q

At FL410 you experience moderate to severe turbulence. What action is required?

A

Slow to .75 Mach

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8
Q

During approach the PF calls for flaps 30 at 180 KIAS. What action should the PM take?

A

Delay flap extension until 175K

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9
Q

What are the three sources of information to the air data computers?

A

Total pressure(Pitot), Static pressure (static ports) and Total temperature (TAT) inputs.

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10
Q

During cruise, you observe ROLL caution on the PFD, and an EFIS MISCOMPARE caution CAS. What is the appropriate action?

A

Identify the operative side information and exchange controls if necessary. Consult FCOM1 or QRH2 for a ROLL PFD annunciation and an the EFIS MISCOMPARE CAS procedure. Consider a degradation of RVSM capability

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11
Q

Describe the IFIS aircraft symbol limitation for taxi and approach charts

A

Advisory only. Not for navigation.

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12
Q

On an LPV approach, you recieve a TAWS GLIDESLOPE warning. What action should be taken?

A

Execute a missed approach.

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13
Q

Why is the automatic mode of the RTA-4100 Weather Radar the reccommended mode to operate in?

A

Automatic mode provides automatic gain and tilt adjustment, including; overflight protection, temperature compensated gain, and PAC (Path Attenuation Compensation )Alert (Gain Plus)

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14
Q

How will Path Attentuation Compensation be displayed?

A

An amber bar behind the displayed echo.

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15
Q

What mode will the weather radar automatically set after landing?

A

Standby after 65 sec WOW.

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16
Q

Explain the Yaw Dampers two purposes.

A

Prevent dutch roll and turn coordination.

17
Q

The engine fails at 500 feet agl and the PF calls for autopilot on. Is this allowed?

A

No, must wait for 700agl feet to engage the autopilot.

18
Q

What is the easiest way to disengage the autopilot and yaw damper at the same time?

A

With the autopilot/yaw damper disconnect bar.

19
Q

During Takeoff LWING OVERHEAT Warning CAS displays at 100K. Will this CAS will be inhibited? What action should be taken?

A

No. Take off should be continued.

20
Q

Passing the ETP enroute from KSFO to PHNL, the passenger notifies you that a laptop is on fire. Where is guidance on how to handle this event?

A

Aircraft Shipset, General Emergency, LIthium Ion Battery Fire-PED Fire Bag Guidance

21
Q

With the boarding lights on and battery power only, how is the battery power protected?

A

A timer shuts off lights after 20 min

22
Q

During de-ice before starting engines with Cabin DC power off, how can the passengers be provided with reading lights?

A

With the Cabin Lights switch

23
Q

How long before descent should you advise the owner that the seat belt lights will be illuminated?

24
Q

During cruise, ATC is not heard on Comm 1 and the Comm 1 frequency is amber. What action should be taken?

A

Switch to Comm 2 or Comm 3

25
One of the static dischargers on the bullet fairing is missing. What action should be taken?
Consult the CDL and defer.
26
On the ground, a buzzer is heard and the white ELT ON CAS message is displayed. What should be checked?
Ensure the ELT switch has not been placed to ON.
27
When the FADEC aborts the start, what actions should be accomplished?
Run switch to OFF, Start switch CRANK for 30 sec, refer to QRH L/R START ABORTED
28
Describe the times the FADEC will activate the ingnition.
EGT changes faster than FADEC parameters, N2 changing faster than FADEC parameters, Aircraft Stall.
29
When the APU ECU has shutdown the APU for protective reasons, how will we know?
APU SHUTDOWN Cyan CAS message.
30
During the Before Start, flows a Cyan Bleed Loop Fault CAS is displayed. What is the appropriate action?
Consult the Smart Ops Guide.