002-139 ELEC Flashcards

1
Q

FSI Splash Screen

A

Nothing

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2
Q

Electrical System

A

Nothing

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3
Q

Lesson Objectives

A

Discuss

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4
Q

Lesson Organization - System Overview

A

Discuss

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5
Q

Electrical System

A
  • Power supplied by
    • 1 - Main Battery - 44Ah (24V)
    • 1 - Aux Battery - 13 Ah, 27Ah, 28 Ah (24 V)
    • 2 - Starter Generators
    • External Power
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6
Q

Cockpit Controls & Indications

A

Discuss

  • MFD Synoptic Page
  • MFD CAS window
  • Electrical Panel
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7
Q

Lesson Organization - DC Power

A

Discuss

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8
Q

DC Power System

A
External Power
* 30.5 Volts Maximum
Main Battery
*  Ni-cad / 24V / 44Ah
Aux battery
*  Ni-Cad / 24 V / 13 Ah, 27Ah,  28 Ah
DC Generators
*
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9
Q

Main Battery

A
  • Ni-Cad
  • 44Ah / 24 Volts
  • MAIN BATT HOT = 65*C
  • Master Battery Switch connects Main and Aux batteries to the Essential busses (Main Battery = K1 , Aux Battery K2)
  • Main Battery Switch connects the Main Battery to the #1 Main Bus (K3)
  • K1 Relay - Essential Bus
  • K3 Relay - Main Bus 1
  • Minimum voltage for start = 23 volts
  • Provide power to the Starter/generators for engine starting
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10
Q

Auxiliary Battery

A
  • Ni-Cad / 24 V / 13 Ah, 27Ah, 28 Ah
  • AUX BATT HOT = 65*C
  • Powers the Battery Bus all of the time
  • Aux Battery relay (K4) and master battery (K2) relays connect the aux battery to the ESS BUSSES (K2) and MAIN BUS 2(K4).
  • Master Battery Switch connects Main and Aux batteries to the Essential busses (Main Battery = K1 , Aux Battery K2)
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11
Q

Battery Limitations

A

Discuss information on the slide

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12
Q

External Power

A
  • Right hand nose section
  • 3 Pins
  • Ext PWR switch connects external power to the Main Bus 1
  • EXT POWER DOOR CAS message
  • Overvoltage 30.5 Volts the external power is disconnected from the system.
  • When External power is introduced to the system, the Starter/Generators and Batteries will be disconnected from the system
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13
Q

Generator Control Units (GCU)

A
  • Located below the baggage compartment
  • Maintains 28V DC to the aircraft busses
  • 1(2) DC GEN HOT CAS message
  • Protection for:
    • OVERVOLTAGE
    • UNDERVOLTAGE - <5V
    • FEEDER FAULT - Deferential feeder current exceeds 125 A
    • BUS FAULT - Over current > 550A - Logic will try to clear the fault within 6 seconds if unsuccessful the Starter/Generator will disconnect
    • REVERSE CURRENT - >10% of the rated load
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14
Q

DC Starter / Generators

A
  • Installed on the accessory gearbox of its respective engine
  • Acts as both a starter and generator.
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15
Q

DC Generator Load Indications

A

Discuss generator limitations and display.

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16
Q

DC Starter / Generator Limitations

A

Discuss Starter Generator Limitations

17
Q

Lesson Organization

A

Discuss

18
Q

DC Electrical Load Distribution

A

Discuss

19
Q

Power Distribution Panels (PDP)

A
  • Main busses are contained in PDPs
20
Q

Power Distribution

A

Discuss power distribution

21
Q

Main & Essential Buses

A

Discuss what systems are on the various busses

22
Q

Services lost during bus failures

A

Discuss what is lost if a main or non-essential bus fails

23
Q

Services available after bus failures

A

Discuss what would be available if the Essential bus was the only power available.

24
Q

Bus Load Voltage Limitations

A

Discuss Bus load Limitations

25
Q

Circuit Breaker Panels

A

Discuss The circuit breaker panel

26
Q

Lesson Organization

A

Discuss slide

27
Q

Power Distribution Operation

A

Discuss switchology and symbology of synoptic page

28
Q

Power Distribution Buses

A
  • Normal Flight - Generators feed the the main buses and allow the batteries to be charged.
  • Main buses power the essential and non-essential buses.
  • If both generators fail, AUX BAT feeds ESS 1 and ESS 2 MAIN BATT feeds ESS 1 & 2 and Main 1 & 2. Non-essential busses are not powered.
  • With external power connected the #1 MAIN BUS is powered and with the BUS TIE closed power is supplied to all BUSES.
  • The batteries are not charged when the external power is connected.
29
Q

Lesson Organization

A

Discuss