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45 Cards in this Set
- Front
- Back
When would the BAT DISCHARGE light illuminate? |
With the battery switch ON, indicates excessive battery discharge |
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On the ground what is meant when the TR UNIT light is illuminated? |
Any TR unit has failed |
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In flight what is meant when the TR UNIT light is illuminated? |
TR1 failed OR TR2 and TR3 failed **Verify it on the Electrical panel |
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Can the ELEC light illuminate in flight? |
No, only on the ground |
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What does the ELEC light illuminated indicate? |
A fault exists in the DC OR standby system |
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Does the IFE/PASS SEAT switch work? |
No, placarded inoperative |
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When does the IDG automatically disconnect? |
High IDG oil temperature |
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Can the IDG be reconnected in flight? |
No, on the ground, engine not running |
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Does the APU have an IDG? |
No, it has it own generator |
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When connecting one source of power to a transfer bus what happens to the previous source? |
The previous source automatically disconnects |
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Where is the Ground Service switch? |
Forward Flight Attendants panel |
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How many IDG's are there? |
2 |
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What AC busses do the Transfer busses power? |
2 Galley busses, Main bus and Ground Service bus
AC Transfer bus 1 also supplies power to AC Standby bus Also power TRU's |
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What does BTB stand for and what do they do? |
Bus Tie Breakers
If a power source supplying the Transfer bus fails the BTBs will allow the opposite transfer bus to be powered off that power source |
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What is the automatic generator online feature? |
If the airplane takes off with the APU powering both transfer busses and the APU is either shutdown or fails the Engine generators are automatically connected to their related transfer bus. This can only occur once per flight |
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For single generator operation what is load shed and on what transfer bus does this occur first? |
Galley and Main bus on AC Transfer bus 2 are shed first followed by Galley and Main busses on Transfer bus 1 if more shedding is required. |
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Is load shedding automatic? |
Yes |
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Once dual generators are supplying power to their individual transfer busses after load shedding does the load restoration occur automatically? |
Yes |
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In flight if the APU is the only source of electric power what gets load shed? |
All galley and main busses |
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When does the DRIVE light illuminate? |
Engine shutdown HOT (High IDG Oil Temp) Engine shutdownHOT (High IDG Oil Temp)IDG FaultIDG manually disconnected IDG Fault IDG manually disconnected |
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A single battery can provide standby power for how long? |
30 minutes |
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Dual batteries can provide standby power for how long? |
60 minutes |
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How many TR Units are there and how are they powered? |
3 Powered by the AC Transfer busses |
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What is the difference between a Hot battery bus and a battery bus? |
Hot Battery bus items are directly linked to the battery and can drain it without the battery switch being turned ON.
A battery bus relies on the battery switch being ON to receive DC power. The same is true with the switched hot battery bus in the 737 |
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With the BUS TRANSFER switch in AUTO what happens during a FD or A/P ILS approach at glideslope capture? |
The cross tie repay opens which causes the DC system to isolate to prevent a single failure from affecting both sides of the DC power system and therefore both sides of the AP/FD Nav equipment |
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Single and Dual batteries voltage? |
22-30 volts |
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With a loss of all Engine and APU electrical power what is the standby source and what busses are powered? |
The battery is the Standby Power source. It powers; DC standby bus AC Standby bus using a static inverter Battery Bus Hot Battery Bus Switched hot Battery bus |
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Once the battery charger has finished charging the batteries does it do anything else? |
It reverts to TR mode and powers the Hot Battery bus and the switched hot battery bus |
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What does the static inverter do? |
Converts DC from the battery to AC power during loss of normal electrical power to power the AC standby bus |
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On standby power what displays will be working? |
Captain side DU, upper DU, Captain CDU Captain nav radios (Nav, ADF) RMI Clock Left IRS Crossfeed valve |
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How are emergency exit lights powered? |
A seperate battery which last 20 minutes. They charge when the switch is in the OFF position |
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What does the APU GEN OFF BUS light indicate? |
The APU is running and not powering any AC transfer bus |
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What does the GEN OFF BUS light indicate? |
IDG is not supplying power to the related transfer bus (breaker is open) |
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What does the SOURCE OFF light indicate? |
No source has been MANUALLY selected to power the related transfer bus OR The manually selected source has been disconnected |
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How are the IDG's cooled? |
Engine fan air and fuel flow |
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When the GROUND POWER AVAILABLE light is illuminated what does that mean? |
Ground power is connected and meets the power quality standards |
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Using external power can the Ground Service busses be powered without applying power to the whole system? |
Yes, the forward flight attendant panel switch GROUND SERVICE can be pushed to directly apply power to ground service busses without powering the system using external power |
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When will the GEN OFF BUS light extinguish after the IDG is running? |
When the GEN switch is turned on to power the associated AC TRANSFER bus |
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When will the TRANSFER BUS OFF light illuminate? |
When the associated AC Transfer Bus is not being powered |
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When will the STANDBY PWR OFF light illuminate? |
When there is no power supplied to the ONE OR MORE of the following busses; DC Standby Bus AC Standby Bus Battery Bus |
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What are some systems the CAB/UTIL switch provide power to? |
Galley busses Logo lights |
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What does the DC bus tie relay do on a A/P or F/D ILS approach? |
Opens to allow each AP to be powered by its own source (DC bus 1 and 2) |
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What does moving the standby power switch to BAT do? |
Forces battery power to operate the Standby buses; AC standby DC Standby |
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What is IDG power output? |
Three phase, 115 volt, 400hz AC |
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What is the DC System voltage? |
28 volt |