systems 3 - Auxiliary system + ESIS Flashcards

1
Q

The purpose of the APU is to _________.

A

Provide a pneumatic air source and an electrical power source.

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2
Q

What is the primary function of the ESU?

A

Automatic starting and continuous operational monitoring.

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3
Q

What is the minimum accumulator pressure, prior to beginning the APU start sequence?

A

2,800 psi

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4
Q

What should be done if during ground operation at high ambient temperatures the APU OIL HOT caution appears or the OIL HOT capsule illuminates?

A

The APU should be shut down immediately to prevent damage, and after a 30-minute cooling period, the oil level should be checked

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5
Q

The ESU will shut down the APU for any detected problems except for an _____ caution

A

The ESU will shut down the APU for any detected problems except for an APU OIL HOT caution

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6
Q

During emergency start override mode, all fault conditions are masked, except for:

A

overspeed

underspeed

short during start

start fuel

main fuel

max fuel outputs

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7
Q

Emergency override is obtained by cycling the APU start switch at least _____ times within _____ seconds

A

5 , 5

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8
Q

The DESU will remain in emergency mode for a maximum of _____ minutes, after which time the APU will revert to normal mode.

If the original fault still exists, the APU will _____

A

2

Shut down

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9
Q

What happens when you pull the APU T Handle?

A

Arms the directional valve

Sends stop signal to the DESU

Cuts of fuel to the APU

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10
Q

What function does the thermal protection switch provide?

A

Activates the shut off switch between 90° and 96° C to prevent cabin overheating

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11
Q

What are the three possible heated air sources for the aircraft on the ground?

A

Bleed air from the engines, APU, or external source.

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12
Q

What would you do to get outside air into the cockpit?

A

Turn on the vent blower

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13
Q

The Fire Detection System provides fire warning in the cockpit in case of what?

A

Fire in either engine compartment or the APU compartment.

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14
Q

Describe the fire detectors?

A

The fire detectors are solid state photoconductive cells that react to infrared radiation.

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15
Q

Upon an impact of 10 g or more, the omni directional impact switch automatically fires both containers releasing fire extinguishing agent into what?

A

Both engine compartments

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16
Q

If no AC power is available _____ fire ext must be used. Also the No. ____ Engine can not be extinguished without AC power

A

Reserve

2

17
Q

What does a broken or missing red thermal discharge safety port indicate?

A

What does a broken or missing red thermal discharge safety port indicate?

18
Q

When AC power is not available, fire fighting capability is lost on which engine?

A

2 Engine.

19
Q

At airspeeds greater than _____ KIAS or during periods of reduced rain intensity the windshield wipers may _____ noticeably. If this occurs, wipers must be parked immediately to avoid wiper motor failure.

A

120 KIAS

Slow

20
Q

Once finished with the windshield wipers the switch should be placed into what position to return the wipers to the normal position?

A

PARK

21
Q

To prevent damage to the windshield, do not operate the windshield wipers when?

A

The windshield is dry

22
Q

What could be used on the windshield to help improve the visibility?

A

Rain repellent.

23
Q

The temperature of each windshield anti ice panel is controlled to a heat level of about _____°C

A

43

24
Q

How many windshield anti-ice switches are there?

A

Three. COPILOT, CTR, PILOT.

25
Q

If the APU is the sole source of power the ______ and ______ can’t be used simultaneously

A

Windshield anti-ice, Backup pump.

26
Q

If ice accumulates on the windshield what could happen?

A

Ice shedding can cause engine FOD

27
Q

To prevent unintentional discharge of the cargo hook explosive cartridge, the pilot shall call off each procedural step of which test?

A

The emergency release circuit test

28
Q

What are the three modes of release?

A

Normal, Manual, and Emergency

29
Q

What is the maximum weight that may be suspended from the cargo hook?

A

9,000 pounds.

30
Q

Pitot static pressure is sent to what aircraft components?

A

ADC’s

31
Q

Pitot heat and anti-ice shall be on during operations in visible moisture with ambient temperature of ________and below?

A

4°C

32
Q

The brake wear indicator provides a ______ means of checking the level of wear on the brake pads (pucks)?

A

Visual

33
Q

How many Weight on Wheel (WOW) switches are installed on the landing gear?

A

2, one on each

34
Q

Do not exceed a touchdown sink rate of ___feet-per-minute on level terrain and ___ feet-per-minute on slopes with gross weights of up to 16,825 pounds; above 16,825 pounds gross weight do not exceed ___feet-per-minute on level terrain and ___ feet-per-minute on slopes?

A

540, 360, 300, 180

35
Q

The two external components that provide display information to the ESIS are:

A

ADC & Magnetometer

36
Q

The BATTERY STBY INST switch is located where in the cockpit?

A

Upper Console

37
Q

A beeping tone can be heard when the the aircraft is on the ground with AC power removed if the BATTERY STBY INST switch is in which position?

A

ARM

38
Q

The ESIS battery should supply power to the instrument for at least ______ Min

A

30