SELF-CHECK 5 / ICE & RAIN PROTECTION (Ch. 16) Flashcards
Which of the following systems are used to protect the aircraft and aid the air crew when operating in ice and rain conditions?
A. Engine Anti-icing, Ice detectors, Probe heats
B. Windshield heat, Windshield wipers
C. Wing/Stab De-icing boots
D. All of the above
D. All of the above.
How are the wing and horizontal stabilizer de-ice boots inflated?
A. Hydraulically
B. Electrically
C. Pneumatically
D. All of the above
C. Pneumatically.
How are the wing and horizontal stabilizer de-ice boots deflated?
A. Hydraulically
B. Electrically
C. Vacuum
D. All of the above
C. Vacuum.
How are the engine inlet P1/T1probes heated?
A. Bleed air
B. Electrically
C. Vacuum
D. Solar power
B. Electrically.
How is engine anti-ice activated?
A. By pushing the ANTI-ICE ENGINE PROBE and NACELLE L and R pushbuttons on the center pedestal
B. By pulling a Lever
C. Hydraulically
D. By pushing the ANTI-ICE ENGINE PROBE and NACELLE L and R pushbuttons on the overhead panel
D. By pushing the ANTI-ICE ENGINE PROBE and NACELLE L and R pushbuttons on the overhead panel.
The HEAT-PROBES switch heats which items?
A. Pitot probes
B. Static ports
C. Total Air Temperature probe and Angle of Attack probe
D. All of the above
D. All of the above.
The windshields are electrically heated and maintain a constant windshield temperature automatically when the HEAT W/S L and R switches are turned on.
A. True
B. False
A. True.
The G200 may or may not have windshield wipers.
A. True
B. False
A. True.
How many ice detectors are installed on the G200?
A. One
B. Two
C. Three
D. Four
B. Two.
What is the infl ation/suction cycle of the G200 de-ice boots?
A. 42 seconds of inflation followed by 18 seconds of suction
B. 40 seconds of inflation followed by 18 seconds of suction
C. 18 seconds of inflation followed by 42 seconds of suction
D. 18 seconds of inflation followed by 40 seconds of suction
C. 18 seconds of inflation followed by 42 seconds of suction.
The ALT position of the De-ice system rocker switch uses an alternate timer but has the same operation cycle as the NORMAL position.
A. True
B. False
A. True.
The pressure regulating and shutoff valve is powered to the open position before engine start and whenever the engine anti-ice is turned off. In the event of a loss of electrical power, the valve will close, supplying heat to the anti-ice system.
A. True
B. False
B. False.
The TAT probe is mounted on the ___ side of the forward fuselage.
A. Left
B. Right
C. Center
D. The roof
B. Right.
The main AOA probe heating element is fully powered in flight or when the PROBE HEAT switch is set to the _______ position.
A. On
B. Auto
C. Override
D. Off
C. Override.
How many windshield zones are heated in the LOW position of the W/S heat?
A. One
B. Two
C. Three
D. Four
C. Three.
