Electrical System Learjet 45XL (1/25/2024) Flashcards

1
Q

The ________ electrical system is powered by _______ engine driven generators.

A

DC/two

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2
Q

How many batteries does the system have?

A

Two main batteries and an emergency battery

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3
Q

_______ power is provided by ______ engine driven _______________ for windshield heat.

A

AC/two/alternators

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4
Q

_________ or _________ can provide power prior to engine start

A

APU/GPU

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5
Q

How many generators are there and how many amps are they?

A

Left, right, and APU. 300 amps

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6
Q

What happens if one Gen fails?

A

NON ESS buses are shed, can be reselected

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7
Q

What happens if two Gen fail?

A

NON ESS buses and MAIN buses are shed, MAIN buses can be reselected

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8
Q

What is an indication of alternator failure?

A

No windshield heat

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9
Q

How many batteries are there and where are they located?

A

Two batteries, tailcone

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10
Q

Describe the main batteries (type, amp/hour, power time if gens fail)

A

lead acid, 38 amp/hour, 50 minutes

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11
Q

What is the minimum voltage for starting?

A

24 volts

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12
Q

Batteries can be re-charged by the APU, GPU, or Gens, unless they go below what voltage?

A

14 volts

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13
Q

________ _________ automatically close if a generator is lost.

A

Bus tie

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14
Q

Turn on the _______________ battery approximately 10 seconds after the Main battery or the O2 masks will drop.

A

Emergency

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15
Q

Describe the emergency batteries (type, amp/hour, power time if gens fail)

A

lead acid, 10 amp/hour, 60 minutes of power after dual gen failure

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16
Q

Red collared CB’s are items on the _________________ _____

A

Emergency bus

17
Q

External power enters into what bus?

A

Left main bus

18
Q

Ideal GPU (volts/amps)

A

28 volts/1000-1100 amps

19
Q

Where can the GPU voltage be read?

A

EICAS

20
Q

What does the White CAS message “EXTERNAL POWER” mean?

A

It means that the GPU is connected, but does not indicate that the GPU is powering the airplane.

21
Q

What does the AVAIL annunciation on the GPU switch mean? (3 things)

A

Power is available, it is the correct polarity, voltage is not fluctuating

22
Q

Batts will charge with external power as long as ___________ switches are on

A

BATT

23
Q

What is the APU fuel flow and rpm?

A

100-150 pph/70,000

24
Q

Where does the APU power enter?

A

Right main bus

25
Q

Where are the APU intake and exhaust located?

A

Intake on the left, exhaust on right upper fuselage

26
Q

There are no indications of __________ or ________ on control panel (APU)

A

RPM/ITT

27
Q

___________ __________ sounds if shutdown occurs to alert crew

A

Ramp horn

28
Q

Weight on wheels is required for what to operate?

A

APU

29
Q

Where does the fuel come from and what is energized when the APU is running?

A

Right wing, right standby pump

30
Q

No ________ ___________ with APU running

A

gravity refuel

31
Q

What are the OAT for APU operation? (2 items)

A

With blowers, up to 125 F

Without blowers, up to 100 F

32
Q

What do the following indications mean for APU? “ADD”, “LOW”, Blue LED, Fan Fail Indication

A

10 ounces below full oil, 18.5 ounces below full oil, can run 5 hours max, possible fault or fail, no ops above 100F/38C

33
Q

What items run of the hot battery bus? (These items always have power and you need to make sure that they are switched off)

A
  • Battery compartment light
  • Baggage compartment light and pylon light when door is open
  • Both cockpit OVRHD swivel lights
  • Refueling panel digital gauge
  • Oxygen test switch in external panel in nose