Navigation Block Flashcards
When will the EFIS control panel be inoperative?
Any electrical failure which results in a loss of power to the front EADI or rear EHSI
Loss of the generator also means loss of
systems powered on the generator bus (if the bus tie is open) and loss of battery charging
Anytime the starter switch is NOT in the ____ position, the generator will not function.
NORM
The starter will drain battery in less than __ minutes if left on.
10 minutes
What are indications that the generator is inoperative?
DC voltmeter below 25 volts and ammeter discharging
If the generator fails and the bus tie switch is opened, how long will the main battery last for?
At least 30 minutes
(however, battery voltage and ammeter cannot be directly monitored due to loss of the associated display)
With generator failed and the bus tie closed, the generator and battery buses will remain powered until
16 volts
Whenever power is lost, the ABOS bottle valve will?
remain in the last selected position
If the main battery is depleted/fails, OBOGS will?
be inoperative
What happens to the cockpit when power to the battery bus is lost?
the cockpit will depressurize
When will the GEN BUS annunciator illuminate?
- if there is an actual loss of the generator bus
- if the CWS circuit breaker on the generator bus circuit breaker panel in the front cockpit is open
If the GEN BUS annunicator illuminates without actual loss of the the GEN BUS, you should?
Check the CWS circuit breaker on the generator bus. If it is open, do NOT reset it
If the CWS circuit breaker is open without accompanying indications of generator bus failure?
the generator bus is functioning normally (and do NOT reset the CWS breaker)
If the generator bus is failed, should you open the bus tie switch?
NO (you do not want to isolate the busses). With an operating generator and the bus tie switch in NORM, the generator will continue to charge the battery and power the battery buses.
What things are still operative if you have a generator bus failure?
Back-up UHF comm
GPS (FCP…fly RNAV)
EADI (composite)
FCP EFIS control head
Battery Bus (w/ bus tie closed)
The BAT BUS annunciator will illuminate if:
- an actual loss of the battery bus
- the CWS circuit breaker on the battery bus circuit breaker panel in the FCP is open
- the current limiter on the battery bus has failed
What is an indicator of the CWS circuit breaker being open?
illumination of the BAT BUS (or GEN BUS) annunciator. All other systems will operate normally
What are indications that the current limiter and/or actual battery bus failure?
- illumination of the BAT BUS annunciator
- multiple failures of items on the battery bus (TRIM OFF, OIL PX, HYDR FL LO, PMU STATUS)
-
MOST NOTICEABLE
EADI, GPS, AEDD, and power off flags in the standby ADI, standby turn and slip indicator, and pressurization
If the standby attitude gyro off flag appears after the battery bus has failed, the indicator will continue to operate for at least __ minutes?
9 minutes
What will happen once power to the battery bus is lost?
the cockpit will depressurize
If the battery bus fails, should you open the BUS TIE switch?
Yes. Place the BUS TIE switch to OPEN to isolate the generator bus from any potential battery or battery bus faults.
How long will the Aux Bat power the standbys and backup UHF radio for?
approximately 30 minutes
Why should you select ALTN with a battery bus failure (and the aux bat on)?
Selecting ALTN will bypass the audio amplifier and provide raw audio for UHF, sidetone and aural warning, with no volume control. Neither intercom nor VHF audio will be heard while switched to ALTN.
If you have a battery bus failure, will the gear and flaps work normally? What about the emergency system?
Neither the gear nor the flaps will operate normally with a battery bus failure. Plan to use the emergency gear extension handle. Emergency flaps should still work (via the hot battery bus) as long as the main battery has not failed. HOWEVER, LANDING GEAR AND FLAP POSITION INDICATORS WILL NOT BE POWERED.