Air Systems (FM: 6.20) Flashcards
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 position disagrees with the commanded position
d) The isolation valve has sensed an overpressure
C) The isolation valve position disagrees with the commanded position
757: The right DUCT LEAK light is illuminated. What does this indicate?
a) High bleed overpressure in the pneumatic duct is detected
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
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 determine by the graphic
A) Closed
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
757: The APU BLEED AIR VALVE light is illuminated. What is the position of the APU bleed air valve?
a) Selected closed, but open
b) Selected closed, and fully closed
c) Selected open, and fully open
d) Selected open, but not open
D) Selected open, but not open
767: The right engine bleed air overheat (OVHT) light is illuminated. What does this indicate?
a) The engine bleed air temperature is excessive
b) An overpressure condition has been detected
c) A high temperature bleed air leak is detected
d) The HPSOV & PRV, when commanded, failed to open
A) The engine bleed air temperature is excessive
757/767: The engine bleed air valves (pressure regulating and shut off valve [PRSOV]) are __________________.
a) Electrically controlled and pneumatically actuated
b) Pneumatically controlled and pneumatically actuated
c) Pneumatically controlled and electrically actuated
d) Electrically controlled and electrically actuated
A) Electrically controlled and pneumatically actuated
757: The left HI STAGE light is illuminated. What does this indicate?
a) The left engine HI STAGE valve position is now based on throttle position
b) The left engine HI STAGE valve is locked at the mid position
c) The left engine HI STAGE valve has been locked open
d) The left engine HI STAGE valve has been locked closed
D) The left engine HI STAGE valve has been locked closed
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
757/767: According to the previous question’s graphic, if a return to DEN is made, what is required by the crew?
a) Select the opposite AUTO position used for takeoff
b) The controller must be reset to DEN altitude
c) Set the AUTO RATE knob to the index position for landing
d) Select MAN on the controller and use manual operation for landing
B) The controller must be reset to DEN altitude
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
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
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
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
757/767: If a return to the departure airport is necessary, how must the crew set the pressurization system?
a) Select MAN on the controller and use manual operation for landing
b) Select the opposite AUTO position used for takeoff
c) Set the AUTO RATE knob to the index position for landing
d) Reset the landing altitude for the return to the departure airport
D) Reset the landing altitude for the return to the departure airport