350 Systems Validation

Question 1

Describe the operation of the vent flap?

Answer 1

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

Question 2

Where is the baggage weight placard located?

Answer 2

Aft bulkhead

Question 3

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

Answer 3

Off

Question 4

Where is the therapudic oxygen mask located?

Answer 4

Aft pyramid, bottom drawer

Question 5

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

Answer 5

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

Question 6

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

Answer 6

MSW ………(PF)…… Press&Hold

Refer to inadvertent pusher activation QRC.

Question 7

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

Answer 7

Slow to .75 Mach

Question 8

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

Answer 8

Delay flap extension until 175K

Question 9

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

Answer 9

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

Question 10

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

Answer 10

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

Question 11

Describe the IFIS aircraft symbol limitation for taxi and approach charts

Answer 11

Advisory only. Not for navigation.

Question 12

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

Answer 12

Execute a missed approach.

Question 13

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

Answer 13

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

Question 14

How will Path Attentuation Compensation be displayed?

Answer 14

An amber bar behind the displayed echo.

Question 15

What mode will the weather radar automatically set after landing?

Answer 15

Standby after 65 sec WOW.

Question 16

Explain the Yaw Dampers two purposes.

Answer 16

Prevent dutch roll and turn coordination.

Question 17

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

Answer 17

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

Question 18

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

Answer 18

With the autopilot/yaw damper disconnect bar.

Question 19

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

Answer 19

No. Take off should be continued.

Question 20

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?

Answer 20

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

Question 21

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

Answer 21

A timer shuts off lights after 20 min

Question 22

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

Answer 22

With the Cabin Lights switch

Question 23

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

Answer 23

10 min

Question 24

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

Answer 24

Switch to Comm 2 or Comm 3

Question 25

One of the static dischargers on the bullet fairing is missing. What action should be taken?

Answer 25

Consult the CDL and defer.

Question 26

On the ground, a buzzer is heard and the white ELT ON CAS message is displayed. What should be checked?

Answer 26

Ensure the ELT switch has not been placed to ON.

Question 27

When the FADEC aborts the start, what actions should be accomplished?

Answer 27

Run switch to OFF, Start switch CRANK for 30 sec, refer to QRH L/R START ABORTED

Question 28

Describe the times the FADEC will activate the ingnition.

Answer 28

EGT changes faster than FADEC parameters, N2 changing faster than FADEC parameters, Aircraft Stall.

Question 29

When the APU ECU has shutdown the APU for protective reasons, how will we know?

Answer 29

APU SHUTDOWN Cyan CAS message.

Question 30

During the Before Start, flows a Cyan Bleed Loop Fault CAS is displayed. What is the appropriate action?

Answer 30

Consult the Smart Ops Guide.