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BBJ Electrical
updated 4-21-12
66
Aviation
Professional
04/21/2012

Additional Aviation Flashcards

 


 

Cards

Term
The purpose of the AC ground service bus is to power:
Definition
The cabin lighting
Term
The TR
Definition
115 volts AC to 28 volts DC
Term
Which is the power source for the AC standby bus?
Definition
Transfer bus 1 under normal conditions
Term
True/False
If the AC source powering a transfer bus fails, the transfer bus will remain unpowered.
Definition
False
Term
True/False
A high oil temperature in the IDG would cause an automatic disconnect of the IDG.
Definition
True
Term
The TR3 cross bus tie relay automatically opens at glide slope capture to:
Definition
Prevent a single bus failure from affecting both navigation receivers and Flight Control Computers (FCCs)
Term
In flight, if the APU is supplying both AC Transfer busses, positioning the BUS TRANS switch to OFF will:
Definition
Cause AC Transfer bus No.2 to lose power
Term
The TR3 Disconnect Relay:
Definition
Automatically opens at glide slope capture during a Flight Director or Autopilot ILS approach
Term
The Engine Integrated Drive Generators (IDGs):
Definition
Allow the generator to maintain a constant speed throughout the normal range of operation
Term
After the loss of all generators, a fully charged battery can furnish power to the STANDBY Bus equipment for a minimum of:
Definition
60 minutes
Term
The cross bus tie relay:
Definition
Opens up if BUS TRANSFER switch is moved to OFF
Term
Illumination of the GND POWER AVAILABLE light indicates:
Definition
Ground power is connected and meets airplane power quality standards
Term
For ground service, a ground service switch is placed:
Definition
On forward attendant's panel
Term
The GROUND POWER AVAILABLE light will extinguish when:
Definition
The AC ground power cart has been disconnected
Term
One basic principle of operation for the B737 electrical system is:
Definition
There is no paralleling of the AC power sources
Term
True/False
Because engine generators power the transfer busses directly, and transfer busses are connected by a bus tie system, the loss of an engine driven generator will not necessarily result in the loss of any bus(ses).
Definition
True
Term
True/False
The modified DC system architecture resulted in the TR3 disconnect relay found in the B737-300 thru 500 being replaced with a cross bus tie relay. The cross bus tie relay opens automatically under the same circumstances as did the TR3 disconnect relay.
Definition
True
Term
The SOURCE OFF light will illuminate:
Definition
When the source selected to power the transfer bus has failed and the automatic bus transfer function has closed the BTBs to power the transfer bus from another source

When the source selected to power the Transfer bus and the automatic transfer function have both failed resulting in the transfer bus being. unpowered

When the TRANSFER BUS OFF light is illuminated
Term
When the STANDBY POWER Switch is OFF:
Definition
The STANDBY PWR OFF light will be illuminated
Term
Illumination of the BAT DISCHARGE light indicates:
Definition
Excessive battery discharge is detected with the battery switch ON
Term
In the event that the airplane battery is depleted, the APU can be started using DC external power.
Definition
False
Term
Illumination of the blue GEN OFF BUS light indicates:
Definition
The IDG is not supplying power to its associated transfer bus
Term
When the aircraft batteries is the only source of power:
Definition
The captain's inboard and outboard displays operate until the battery is discharged
Term
Illumination of the GEN BUS OFF light indicates:
Definition
The IDG is not supplying power to its associated Transfer bus
Term
True/False
It is possible to power one transfer bus with external power and the other transfer bus with the APU.
Definition
False
Term
The crew fails to properly accomplish normal procedures and takes off with the APU powering both Transfer busses (SELECT THE INCORRECT STATEMENT)
Definition
Both Main busses may become inoperative above 400 feet RA or after 12 sec. from lift-off
Term
True/False
AC amperage can be observed on the AC ammeter for the source selected by the AC meter selector.
Definition
True
Term
During cruise, one engine driven generator drops off-line. Indications that the crew should see include:
Definition
A SOURCE OFF light and a GEN OFF BUS light
Term
Illumination of the DRIVE light indicates:
Definition
IDG failure or
IDG automatic disconnect due to high oil temperature or 
IDG disconnected through the drive disconnect switch
Term
Both AC Transfer busses can be powered simultaneously by:
Definition
A single IDG on the ground or inflight
The APU generator while on the ground or inflight
Term
On the ground, with the battery switch OFF and STANBY POWER Switch in AUTO, the Battery Bus is:
Definition
Not powered
Term
The TR UNIT will illuminate in flight if:
Definition
TR1 fails or TR2 and TR3 fail
Term
The ELEC light will illuminate in flight if:
Definition
The ELEC light only operates on the ground
Term
What is the significance of an illuminated ELEC light?
Definition
The DC system or standby system equipment has failed
Term
With external DC power connected to the external DC power receptacle:
Definition
There is no external DC power receptacle
Term
Illumination of the STANDBY POWER OFF light indicates:
Definition
The AC Standby Bus is unpowered or
The DC Standby Bus is unpowered or  
The Battery Bus is unpowered
Term
With the STANDBY switch in the AUTO position, the loss of all engine or APU electrical power results in the automatic switching from the normal power source to the alternate source for standby power:
Definition
Either inflight or on the ground
Term
In flight if APU is the only source of electrical power:
Definition
All galley busses are automatically shed
Term
True/False
With the STANDBY POWER switch in AUTO (guarded position). In flight, or on the ground, loss of all AC power. AC Standby bus is powered by battery through static inverter & DC Standby bus is powered by battery.
Definition
True
Term
DC voltage and amperage may be read on the DC voltmeter and ammeter for the battery and each of the 3 TRs. The Standby power and battery bus displays only Dc voltage. Normal indication is : ______ volts
Definition
26 +/-4
Term
True/False
The purpose of the static inverter is to convert 24 volt DC power from the battery to 115V AC power to supply the AC standby bus during the loss of normal electrical power.
Definition
True
The power supply to the inverter is controlled by the standby power switch and the battery switch on the overhead panel
Term
The two nickel-cadmium batteries can provide standby power for a minimum of _____ minutes (if fully charged).
Definition
60
Term
DC busses powered from the battery following a loss of both generators are:
Definition
Battery bus
DC Standby bus
Hot battery bus & Switched hot battery bus
Switched hot battery bus is powered whenever the battery switch is ON
Term
True/False
If the TR UNIT light is illuminates in flight, it indicates that one or more TR\'s have failed and you are supposed not to use the AFDS approach mode.
Definition
True
Term
True/False
An illuminated TR UNIT light while on the ground indicates that at least two TRs have failed.
Definition
False
Term
What is the purpose of the GROUND SERVICE switch?
Definition
Provide manual control of ground service busses
Enables servicing airplane using external power without activating AC transfer busses.
Term
Either generator or the APU can power both transfer buses. In the event a power source fails, what is required for that transfer bus to be powered by the opposite transfer bus power source?
Definition
The BUS TRANS switch must be in the AUTO position
Term
Normal AC voltmeter indication for the APU generator with the AC busses loaded:
Definition
110 to 125 volts
Term
Illumination of the STANDBY POWER OFF light indicates:
Definition
AC standby bus unpowered
Term
53. DC voltage and amperage may be read on the DC voltmeter and ammeter for the battery and each of the three TRs. The standby power and battery bus displays only DC voltage. Normal indication is:
Definition
26 +/- 4 volts
During primary charge cycle operation battery voltage can be as high as 30 +/- 3 volts
Term
True/False
Both On the ground and in flight a amber ELEC light comes on to indicate that a fault exists in DC power system or standby power system.
Definition
False
The ELEC light is inhibited in flight
Term
Galley busses are powered from:
Definition
The AC Transfer busses
Term
How many TRs are required to power the entire DC system?
Definition
Two TRs
Term
What is the source of power for TR3?
Definition
Transfer bus 2
Term
What is the source of power for TR2?
Definition
Transfer bus 2
Term
The switched hot battery bus is powered whenever:
Definition
The battery switch is ON
Term
The purpose of the cross tie relay is to:
Definition
Isolate DC bus 1 from DC bus 2
Term
What is the source of power for TR1?
Definition
Transfer bus 1
Term
On the ground, with the BATTERY switch OFF and STANDBY POWER Switch in BAT, the switched hot battery bus is:
Definition
Not powered
Term
The main battery charger is powered through:
Definition
AC ground service bus 2
Term
Which bus supplies electrical power to the auxiliary battery charger?
Definition
AC ground service bus 1
Term
True/False
The auxiliary battery operates in parallel with the main battery when the battery is powering the standby bus.
Definition
True
Term
The electrical system incorporates an automatic load shedding feature. What is the first bus that is shed?
Definition
Galleys on transfer bus 2 are shed first
Term
The electrical system incorporates an automatic load shedding feature. What is the second bus that is shed?
Definition
Galleys on transfer bus 1
Term
After an overload situation has been resolved, how do you recover the galley buses?
Definition
It happens automatically
Term
True/False
Once disconnected, the IDG can be reconnected in flight.
Definition
False
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