Study Guide: Air Systems FM 6.20 Flashcards
1) 757: The ISOLATION VALVE light is illuminated. What does this indicate?
a) The isolation valve has overheated
b) The isolation valve is open
c) The isolation valve is not in the commanded position
d) The isolation valve has sensed an overpressure
c) The isolation valve is not in the commanded position
2) 757: The right DUCT LEAK light is illuminated. What does this indicate?
a) The engine bleed system pressure is excessive
b) A high temperature bleed air leak is detected
c) A bleed air leak in the engine anti-ice duct is detected
d) Overpressure is detected in either wing anti-ice duct
b) A high temperature bleed air leak is detected
3) 757: The right engine BLEED AIR OFF light is illuminated. What is the position of the
right engine bleed air valve?
a) Closed
b) In transit
c) Open
d) Unable to be determined using the graphic
a) Closed
4) 757: The right engine BLEED light is illuminated. What does this indicate?
a) The right engine bleed air valve is failed close
b) The right engine high pressure valve is open at low engine thrust
c) The right engine low pressure valve is closed
d) The right engine bleed air temperature is excessive
d) The right engine bleed air temperature is excessive
5) 757: The APU BLEED AIR VALVE light is illuminated and EICAS advisory message APU
BLEED VAL is displayed. What does this indicate?
a) The APU bleed air valve is open
b) The APU bleed air valve is closed
c) The APU bleed air valve is operating normally
d) The APU bleed air valve is not in the commanded position
d) The APU bleed air valve is not in the commanded position
767: The right engine bleed air overheat (OVHT) light is illuminated. What does this
indicate?
a) An engine bleed air overheat
b) A high temperature bleed air leak is detected
c) The HPSOV and/or PRV valve has failed in the full open position
d) The engine bleed system pressure is excessive
a) An engine bleed air overheat
7) 757/767: The engine bleed air valves (pressure regulating and shut off valve [PRSOV])
are __________________.
a) Electrically controlled and pressure actuated
b) Pressure controlled and pressure actuated
c) Pressure controlled and electrically actuated
d) Electrically controlled and electrically actuated
a) Electrically controlled and pressure actuated
8) 757: The left engine HI STAGE light is illuminated. What does this indicate?
a) The left engine bleed system temperature is excessive and the engine high
pressure bleed air valve is automatically locked open
b) The left engine bleed system temperature is excessive and the engine high
pressure bleed air valve is automatically locked closed
c) The left engine bleed system pressure is excessive and the engine high pressure
bleed air valve is automatically locked open
d) The left engine bleed system pressure is excessive and the engine high pressure
bleed air valve is automatically locked closed
d) The left engine bleed system pressure is excessive and the engine high pressure
bleed air valve is automatically locked closed
9) 757/767: The pressurization system is in the automatic mode when the cabin altitude
mode selector is set to AUTO 1 or AUTO 2. According to the graphic, what would the
pressurization system do if the AUTO 2 controller were to fail?
a) The AUTO INOP light illuminates
b) Cabin altitude automatically descends to 4000 feet
c) Control is automatically switched to the MAN controller
d) Control is automatically switched to the AUTO 1 controller
d) Control is automatically switched to the AUTO 1 controller
10) 757/767: On the ground, when does the pressurization system begin pressurizing the
aircraft?
a) When the airplane passes 400 feet RA
b) When the airplane passes 50 feet RA
c) When the throttles are advanced for the takeoff
d) At nose strut extension plus 20 seconds or 400 feet RA, whichever occurs first
c) When the throttles are advanced for the takeoff
11) 757/767: The AUTO INOP light is illuminated. According to the graphic, what could
cause this?
a) AUTO 2 is inoperative
b) AUTO 1 is inoperative
c) The AUTO RATE knob was moved beyond the index mark
d) Both AUTO controllers have failed
d) Both AUTO controllers have failed
12) 757/767: The AUTO RATE knob sets limit for cabin altitude rate of climb or descent
when mode selector is in AUTO 1 and AUTO 2 modes. Index mark establishes
approximately ___ FPM climb and ___ FPM descent limits.
a) 1000, 300
b) 800, 300
c) 600, 400
d) 500, 300
d) 500, 300
13) 757/767: What will occur if the selected (AUTO 1 or AUTO 2) pressurization controller
fails?
a) Control is automatically switched to the other controller
b) Cabin altitude automatically descends to 4000 feet
c) Control is automatically switched to the MAN controller
d) The AUTO INOP light illuminates
a) Control is automatically switched to the other controller
14) 757/767: If a return to the departure airport is necessary, how must the crew set the
pressurization system?
a) The MAN position must be selected on the controller and manual operation used
for landing
b) The opposite AUTO position used for takeoff must be selected
c) The AUTO RATE knob must be moved to the index position for landing
d) The landing altitude must be reset for return to the departure airport
d) The landing altitude must be reset for return to the departure airport
15) 757/767: On the cabin altitude control panel, the AUTO INOP light is illuminated. What
can cause this?
a) The AUTO RATE knob is moved beyond the index mark
b) AUTO 1 is inoperative
c) MODE SELECT switch is in MAN
d) AUTO 2 is inoperative
c) MODE SELECT switch is in MAN