Ice And Rain

Question 1

What condition would cause an amber “PITOT HT FAIL” message to be displayed on the CAS?

Answer 1

• Pitot heat switch selected OFF

- Pitot tube heater elements not energized

Question 2

How is the engine intake area heated?

Answer 2

By using engine 12th stage HP air routed through the bleed air pressure-regulating valve to the engine cowl anti-ice valve.

Question 3

If one of the wing anti-ice valves is inoperative, how does the system transfer wing heat from one side to the other?

Answer 3

Through an uncontrolled crossover duct

Question 4

What is the minimum cowl anti-ice pressure?

Answer 4

4 psi

Question 5

What is the maximum allowable speed for windshield wiper operation?

Answer 5

200 knots

Question 6

If wing anti-ice is selected ON prior to takeoff, what is the effect on the autothrottle system?

Answer 6

The autothrottles would engage; however, it is not permissible to use theautothrottles for takeoff when wing anti-ice is used

Question 7

If a crack occurs in an outer windshield ply, what is the effect on the windshield heat system?

Answer 7

The heat for the affected windshield will be inoperative

Question 8

What is indicated by a blue “WING A/I, L-R” advisory CAS message?

Answer 8

Both wing anti-ice switches have been selected ON

Question 9

If both bleed air switches are selected to OFF, what is the effect on the engine anti-ice system?

Answer 9

Engine anti-ice is not available with both bleed air switches OFF

Question 10

When is cowl anti-ice required to be used on the ground?

Answer 10

During taxi and takeoff when the static air temperature is less than +10º C and visible moisture, wet runways, or precipitation is present

Question 11

When is wing anti-ice required?

Answer 11

Operation of the Wing Anti-Ice System is required if icing conditions are imminent or immediately upon detection of ice formation on wings, winglets, or windshield edges.

Question 12

What is indicated by a “WING WARM” advisory light on the overhead annunciator panel?

Answer 12

The wing has reached a temperature of 100º F

Question 12

What is the limitation for continued flight with a cracked windshield?

Answer 12

• If the crack is in either main structural ply, reduce cabin differential to 7.5 psi for the remainder of flight
• Maintain current airspeed / mach or slower for remainder of flight

Question 14

What is indicated by an amber left or right “WING HOT” CAS message?

Answer 14

The temperature of the respective wing has exceeded 180º F

Question 15

The LOW COWL PRESS warning CAS message will occur when?

Answer 15

s/n 1000-1189 w/ ASC 243 and s/n 1190 and subs pressure drops below 4 psi (±1), after a 15s delay

NOTE: As long as the pressure is not lower than 4 psi, the aircraft will have enough bleed air to prevent ice formation.