Electrical system Flashcards

1
Q

What is the purpose of the Electrical Power Generation and Distribution System (EPGDS)?

A

It supplies electrical energy for all onboard electrical equipment and provides energy conversion

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2
Q

What are the components of the DC generation system in the Q400?

A

The DC generation system includes three NiCad batteries

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3
Q

How is power distributed in the Q400 electrical system?

A

Power is distributed by an electrical bus system that reconfigures automatically during individual power source and bus failures by opening and closing bus tie contactors.

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4
Q

How can AC and DC aeroplane services be operated?

A

They can be operated from the AC generators or AC external power alone.

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5
Q

What is the function of the ELEC SYS pushbutton on the ESCP panel?

A

It displays the electrical system page on the MFD when set to SYS. There is no action with another push.

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6
Q

What happens when the STBY BATT switch is selected ON?

A

It connects the standby battery to the left main feeder bus unless external power is connected

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7
Q

What does the AUX BATT switch control?

A

It connects the auxiliary battery to the left main feeder bus

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8
Q

What does the MAIN BATT switch do?

A

It connects the main battery to the right main feeder bus under normal operations and disconnects during emergency conditions or when a bus fault is present.

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9
Q

What is the purpose of the BATTERY MASTER switch?

A

It disconnects or connects the main

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10
Q

What is the function of the GEN 1 and 2 switches?

A

They allow the DC GCU to connect the generators to their associated feeder buses.

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11
Q

How does the MAIN BUS TIE switch operate?

A

It manually ties the left and right main feeder buses

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12
Q

What happens when the BUS FAULT RESET switch is pressed?

A

It reinitializes the EPCU after a bus isolation to enable subsequent bus fault monitoring.

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13
Q

What is the role of the DC EXT PWR switch?

A

It powers the left and right main feeder buses

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14
Q

What voltage tolerance must be met for the DC EXT PWR to be connected?

A

The applied voltage must be within 22 ± 1VDC to 31 + 0.5/-0.75VDC.

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15
Q

What is the function of the AC EXT PWR switch?

A

It connects AC external power to the variable frequency buses and powers all AC and DC buses on the aeroplane.

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16
Q

What is the purpose of the External Power Protection Unit (AC PPU)?

A

It ensures only AC power within specifications is allowed on the bus.

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17
Q

How is the AC PPU activated?

A

By checking for voltage level

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18
Q

What system monitors electrical parameters in the flight deck?

A

The Electronic System Indicating Displays (ESID) monitor system parameters.

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19
Q

What are the main sources of DC power on the Q400?

A

Main

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20
Q

What is the priority of DC buses in the Q400?

A

The priority is Battery

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21
Q

Where are the main and auxiliary batteries located?

A

In the lower left nose compartment of the aircraft.

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22
Q

What capacity do the main and auxiliary batteries have?

A

They each have a capacity of 40 amp-hours.

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23
Q

How long can the aircraft operate on batteries in flight?

A

The aircraft can operate for 45 minutes or more using battery power for essential services.

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24
Q

What happens when the BATTERY MASTER switch is turned ON?

A

Three contactors close

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25
Q

Can battery power be applied to the secondary buses?

A

No

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26
Q

What temperature limitation applies to battery operation?

A

Battery temperature should be equal to or greater than -20°C prior to dispatch

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27
Q

What are the charging characteristics of the 40Ahr batteries?

A

Charging voltage must be between 28 and 32 VDC for full recharging. A low voltage cart cannot fully charge the batteries.

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28
Q

What happens if DC external power voltage is below 28VDC?

A

The batteries will discharge and not be fully restored.

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29
Q

What is the function of the starter/generators?

A

They act as starter motors and revert to generator operation after engine start to supply 28.5VDC to the feeder buses.

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30
Q

What is the role of the Generator Control Unit (GCU)?

A

It monitors and controls generator output and disconnection in case of faults.

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31
Q

What are Transformer Rectifier Units (TRUs) responsible for?

A

They convert 115-volt variable frequency AC power into 28VDC for the aircraft’s DC buses.

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32
Q

Where are the TRUs located?

A

In the nose of the aircraft.

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33
Q

What happens if a TRU fails?

A

The EPCU reconfigures the power system

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34
Q

How does the APU Starter/Generator function?

A

It supplies 28VDC to the essential

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35
Q

How is fault tolerance achieved in the DC power system?

A

The EPCU automatically reconfigures power flow and ensures operation with up to two power source failures.

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36
Q

What happens when both DC generators fail in flight?

A

The TRUs supply DC power to both the main and secondary buses through vertical bus ties.

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37
Q

What occurs during emergency mode in the EPCU?

A

The batteries disconnect from the main buses

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38
Q

What protection is provided for the DC buses?

A

The EPCU and DC GCUs protect against short circuits on the main and secondary buses.

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39
Q

What happens when a main bus fault occurs?

A

The EPCU isolates the bus

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40
Q

What caution lights come on during a main bus fault?

A

The MAIN BATTERY or AUX and STBY BATTERY caution lights

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41
Q

What is the function of the MAIN BUS TIE switch during a fault?

A

It is locked out by the EPCU and cannot be operated manually.

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42
Q

How does the EPCU react if a secondary bus fault occurs?

A

It transfers the fault to the opposite TRU

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43
Q

How are engine starts powered in the Q400?

A

Engine starts can be powered by batteries

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44
Q

What batteries are used for starting if ground power is unavailable?

A

The main and auxiliary batteries are used for engine starting.

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45
Q

How does the EPCU monitor bus faults during engine starting?

A

The EPCU disconnects the standby battery during the start sequence and reconnects it afterward.

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46
Q

What is the role of the vertical and horizontal bus ties?

A

They connect main and secondary buses during power source failures or faults.

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47
Q

What is the maximum current provided by the starter/generators?

A

The starter/generators provide a maximum of 400 amps.

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48
Q

What type of overheat protection is provided for the TRUs?

A

The TRUs have overheat sensors that activate caution lights when the temperature exceeds the limit.

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49
Q

What happens if a TRU overheats?

A

The corresponding TRU HOT caution light comes on

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50
Q

What is the purpose of the AC GEN caution lights?

A

They indicate that the AC generators are not supplying power to the variable frequency buses.

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51
Q
A
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52
Q

What type of batteries are used in the Q400?

A

NiCad batteries

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53
Q

How many main batteries does the Q400 have?

A

Two

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54
Q

Where are the main batteries located?

A

Lower left nose compartment

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55
Q

What voltage do the TRUs convert AC to?

A

28 VDC

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56
Q

How many engine-driven starter/generators are there?

A

Two

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57
Q

What does the EPCU stand for?

A

Electrical Power Control Unit

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58
Q

What is the nominal voltage of a fully charged battery?

A

24 VDC

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59
Q

Where is the standby battery located if no APU is installed?

A

Tail compartment

60
Q

What is the capacity of the auxiliary battery?

A

40 amp-hours

61
Q

What is the voltage of AC generators in the Q400?

A

115 Volts AC

62
Q

What color is the DC EXT PWR ON indication on the MFD?

63
Q

What happens when the MAIN BUS TIE switch is set to ON?

A

It connects the left and right main feeder buses

64
Q

What is the purpose of the BUS FAULT RESET switch?

A

To reinitialize the EPCU

65
Q

What does the DC EXT PWR switch do?

A

Powers the buses from DC external power

66
Q

What is the maximum DC voltage tolerance for the external power connection?

67
Q

How many Transformer Rectifier Units (TRUs) are in the Q400?

68
Q

At what engine speed does the starter/generator switch to generator mode?

69
Q

What is the maximum output of the starter/generator in amps?

70
Q

What is the voltage range of the TRUs during operation?

A

26 to 29 VDC

71
Q

Where is the APU starter/generator located?

A

Tail cone section

72
Q

What does the L TRU caution light indicate?

A

The left TRU is offline or failed

73
Q

How long can the aircraft operate on batteries during emergency flight?

A

45 minutes or more

74
Q

What is the nominal output of the APU starter/generator?

75
Q

How does the EPCU handle a bus fault?

A

It isolates the bus and locks out the contactors

76
Q

How many bus tie contactors are there in the Q400 DC system?

77
Q

What condition triggers the EPCU to operate in emergency mode?

A

Loss of both DC generators and at least one TRU

78
Q

What does the EPCU monitor for the DC subsystem?

A

Bus faults and short circuits

79
Q

What does the DC GEN caution light signify?

A

The generator is not supplying power to the bus

80
Q

What happens when both TRUs fail?

A

DC generators power both main and secondary buses

81
Q

What causes the MAIN BAT HOT warning light to come on?

A

High battery temperature

82
Q

What voltage must be met for batteries to recharge fully from an external DC cart?

A

At least 28 VDC

83
Q

What are the two conditions under which the standby battery is automatically disconnected?

A

DC external power connected

84
Q

What is the maximum temperature that causes the battery temperature digits to turn yellow?

A

50°C to 65°C

85
Q

What is the main function of the Generator Control Unit (GCU)?

A

To control and monitor the generator’s output

86
Q

What happens if the EPCU detects a fault on the main bus?

A

The EPCU isolates the bus and sends a trip signal to the GCU

87
Q

What does the EPCU do when it operates in emergency mode?

A

Disconnects the batteries from the main buses

88
Q

Where are the TRUs located on the Q400?

A

In the nose section

89
Q

What protection is built into the external DC power supply system?

A

External DC Power Protection to avoid incorrect voltage or polarity

90
Q

What is the voltage trip point for the AC external power under-voltage protection?

91
Q

What happens if the AC PPU detects incorrect phase rotation?

A

AC external power is not allowed on the bus

92
Q

What is the function of the MAIN BUS TIE switch during a fault condition?

A

It is locked out by the EPCU

93
Q

How does the EPCU handle an overheat condition on the generator?

A

The #1 DC GEN HOT or #2 DC GEN HOT light comes on

94
Q

What condition will cause the standby battery to be diode isolated during engine start?

A

Battery power alone is used during engine start

95
Q

How many essential buses are powered by the battery master switch?

96
Q

What type of electrical power does the APU generator provide?

97
Q

What happens if a TRU overheat condition persists?

A

The TRU will be taken offline

98
Q

Which buses are automatically reconfigured by the EPCU during power source failure?

A

Main and secondary buses

99
Q

What is the maximum over-voltage trip point for AC external power?

100
Q

What is the output power capacity of the TRUs in amps?

A

300 Amps max

101
Q

What indication is shown when DC external power is connected correctly to the aircraft?

A

DC EXT PWR ON indication (green) on the MFD

102
Q

What is the purpose of the EPGDS in the Q400?

A

To supply electrical energy for onboard electrical equipment

103
Q

How many TRUs are in the Q400 electrical system?

104
Q

How does the DC generation system reconfigure in case of power source failure?

A

By automatic closing and opening of bus tie contactors

105
Q

What is the voltage output of the Q400’s AC generators?

106
Q

What powers the 28VDC system in the Q400?

A

Two Transformer Rectifier Units (TRUs)

107
Q

How is external power connected to the aircraft’s electrical system?

A

Through external AC or DC power receptacles

108
Q

What is the function of the ESCP pushbutton for electrical system display?

A

It displays the electrical system page on the MFD

109
Q

What does the STBY BATT switch do?

A

It connects the standby battery to the left main feeder bus

110
Q

How many batteries can power both essential buses when selected?

A

Any battery can power both essential buses

111
Q

What happens when the GEN 1 or GEN 2 switch is turned off?

A

The associated generator shuts off

112
Q

What does the BUS FAULT RESET switch do?

A

It reinitializes the EPCU after a bus fault

113
Q

What happens when the external DC power is connected correctly?

A

The DC EXT PWR ON indication shows green

114
Q

How does the EPCU protect against incorrect DC external power?

A

It monitors voltage

115
Q

What is the function of the external power switch for AC power?

A

It connects AC external power to the variable frequency buses

116
Q

What protection is provided for AC external power?

A

External Power Protection Unit (AC PPU)

117
Q

What color indicates that AC external power is connected?

118
Q

How are electrical parameters monitored in the flight deck?

A

Through the Electronic System Indicating Displays (ESID)

119
Q

What type of batteries are located in the Q400 nose compartment?

A

Main and auxiliary batteries

120
Q

How many amps are the main and auxiliary batteries?

A

40 amp-hours each

121
Q

What happens when the BATTERY MASTER switch is turned on?

A

It connects all three batteries to the essential buses

122
Q

Can battery power be applied to the secondary buses?

123
Q

What battery temperature should be met before dispatch?

A

Equal to or greater than -20°C

124
Q

How much load is supplied by the starter/generator after engine start?

A

28.5 VDC and up to 400 Amps

125
Q

What happens if a generator overheat condition occurs?

A

The DC GEN HOT caution light comes on

126
Q

What do TRUs convert AC power to?

127
Q

How are the TRUs cooled?

A

By internal cooling fans

128
Q

What happens when a TRU fails?

A

The EPCU reconfigures the system and the other TRU powers both secondary buses

129
Q

Where is the APU starter/generator located?

A

In the tail cone section

130
Q

What is the main function of the APU starter/generator?

A

To supply 28VDC to the DC buses on the ground

131
Q

What happens when both DC generators fail?

A

The TRUs power both main and secondary buses

132
Q

How does the EPCU ensure mission completion after power source failure?

A

By automatically reconfiguring the bus system

133
Q

What is the function of the vertical bus tie contactors?

A

They connect main and secondary buses in case of power source failure

134
Q

What happens during emergency mode in the EPCU?

A

The batteries disconnect from the main buses

135
Q

What triggers the EPCU to operate in emergency mode?

A

Loss of both DC generators and at least one TRU

136
Q

What happens during a main bus fault?

A

The EPCU isolates the bus and locks out the contactors

137
Q

What does the MAIN BAT HOT warning light indicate?

A

High main battery temperature

138
Q

How are main bus failures handled?

A

The EPCU isolates the affected bus and trips the GCU

139
Q

What happens when a secondary bus fault occurs?

A

The fault is transferred to the opposite TRU

140
Q

How are the starter/generators connected to the bus system?

A

Through the Generator Control Unit (GCU)

141
Q

What is the output of the TRU in amps?

A

300 Amps max

142
Q

How are batteries charged during flight?

A

By the DC generators supplying 28.5 VDC

143
Q

What happens if external power cart voltage is below 28 VDC?

A

The batteries will discharge

144
Q

What is the output voltage range of the TRUs?

A

26 to 29 VDC

145
Q

What happens if both TRUs and generators fail?

A

The EPCU isolates the buses and connects the batteries for emergency power