SV Air Systems Flashcards

1
Q

757/767 if the pack automatic control system failed, what would be indicated

A

The INOP light only

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2
Q

757/767 the AUTO RATE knob sets limit … index mark establishes approximately ___ FPM climb and ___ FPM descent limit

A

500,300

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3
Q

757/767 the FWD cab compartment temperature inop light is illuminated. What is a possible cause

A

Fault or overheat in the zone temperature controller

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4
Q

767 the right engine bleed air overheat light is illuminated. What does this indicate

A

An engine bleed air overheat

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5
Q

757/767 the auto inop light is illuminated, what could cause this?

A

Both auto controllers have failed

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6
Q

757 the two cargo compartments are heated by discharge air… supplemental heating is accomplished by

A

An electric heater in the duct downstream of the fan

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7
Q

757/767 the R pack has shut down due to the compressor temperature exceedance … is that the correct indication

A

Yes the inop and pack off lights should be illuminated

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8
Q

767 eicas advisory message fwd eqpt smoke displays and ____

A

The smoke light illuminates

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9
Q

767 the equipment cooling system NO COOLING light is illuminated. What position is the switch in

A

OVRD

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10
Q

757/767 On the ground when does the pressurization system begin pressurizing the aircraft

A

When the throttles are advanced for takeoff

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11
Q

757 the right engine bleed air off light is illuminated what is the position of the right engine bleed air valve

A

Closed

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12
Q

757/767 on the cabin altitude control panel, the auto inop light is illuminated

A

MODE SELECT switch is in MAN

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13
Q

757/767 what will occur if the selected auto 1/2 controller fails

A

Control is automatically switched to the other controller

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14
Q

757 757: Air is circulated through the forward E/E racks by one of two supply fans. If the operating fan fails, what starts the alternate fan?

A

Pressing the EQUIP COOLING switch to the ALTN position

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15
Q

757: The right engine BLEED light is illuminated. What does this indicate?

A

The right engine bleed air temperature is excessive

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16
Q

757/767: What will the pack do when both the INOP and PACK OFF lights illuminate?

17
Q

757/767: If there were to be excessive pack outlet temperature, which lights) would illuminate?

18
Q

757/767: On the ground, what would cause the high flow schedule to be automatically activated for both packs during single-engine taxi?

A

APU supplying air to both packs

19
Q

767: The equipment cooling system OVHT light is illuminated. What caused it’s illumination?

A

There is low airflow or high temperature sensed

20
Q

757/767: The engine bleed air valves (pressure regulating and shut off valve [PRSOV) are

A

Electrically controlled and pressure actuated

21
Q

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

Control is automatically switched to the AUTO 1 controller

22
Q

767: The equipment cooling system VALVE light is illuminated. What is a possible cause for it’s illumination?

A

One or more forward equipment cooling supply or exhaust valves are not in their commanded position after engines are started

23
Q

757/767: The high flow schedule is automatically activated to provide higher-than-normal air flow when

A

One pack is inoperative

24
Q

757: High flow to the opposite pack is inhibited when:

A

The RPM of either engine falls below a preset value

25
757: The APU BLEED AIR VALVE light is illuminated and EICAS advisory message APU BLEED VAL is displayed. What does this indicate?
The APU bleed air valve is not in the commanded position
26
757: The ISOLATION VALVE light is illuminated. What does this indicate?
The isolation valve is not in the commanded position
27
757: The left engine HI STAGE light is illuminated. What does this indicate?
The left engine bleed system pressure is excessive and the engine high pressure bleed air valve is automatically locked closed
28
753/767: The aircraft is divided into temperature zones.
4
29
757/767: If a return to the departure airport is necessary, how must the crew set the pressurization
The landing altitude must be roset for return to the departure airport
30
757/767: If you position one of the compartment temperature control knobs to the OFF position, what will happen?
The associated compartment INOP light will illuminate
31
757: The right DUCT LEAK light is illuminated. What does this indicate?
A high temperature bleed air leak is detected