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.
If the battery bus has failed, can you confirm the via the position indicators? What about the AoA vane?
No…?
With normal flap extension and loss of power to the battery bus?
the flaps will retract
What items will still be operative if the battery bus fails?
EHSI (fly VOR approach)
RCP EFIS control panel
VHF radio
Primary airspeed/altitude
PEDD
RMU and Transponder
What does it mean if the BUS TIE annunciator illuminates in flight?
the battery bus and generator bus have been disconnected at the bus bar crosstie
What should you consider if the BUS TIE illuminates in flight?
If other caution/warning annunciations are present, refer to the appropriate procedures. If no other annunciations occur, the generator bus will continue to operate normally and items on the battery bus will continue to function as long as battery power exists. Battery power can be prolonged by turning off non-essential equipment
What will be operative if both the battery and generator fails?
Only items powered by the Aux Bat for 30 minutes
(standby gages and associated lighting, fire detection system (FIRE 1 only), and UHF radio)
If the main battery fails, how do you extend the flaps?
Trick question…you can’t
During all electronic display failures, the pilot should:
confirm indications in both cockpits, reference alternate data sources/standby instruments, and check circuit breakers
What is indicated by multiple display failures without a GEN BUS or BAT BUS annunciator illuminated?
Avionics Bus Failure
What is the indications for a total AHRS failure?
- ATTITUDE FAIL
- HDG on the EHSI
(3. X over the rate-of-turn scale)
When accomplishing inflight AHRS alignment, the aircraft must be in straight and level unaccelerated flight for a minimum of
30 seconds
With a total AHRS failure, are the GPS and VOR needles accurate?
GPS and VOR needles will continue to provide accurate bearing information, but are slaved to the frozen EHSI compass card (it won’t rotate). Exercise caution when using GPS or VOR needles for navigation.
What 2 indications must you have for a total AHRS failure?
Attitude fail on the EADI and HDG on the EHSI
What is the indication of an inoperative RMU?
if RMU blanks during flight and returns with off condition displayed
What should you squawk with a radio failure?
7600 (unless a more significant emergency exists)
If you experience radio failure in VMC, what should you do?
Fly recovery ground track at VFR hemispherical altitudes to the appropriate radar termination point (pink pages)
If you experience radio failure in IMC, what should you do? (generally)
Depends on where you are, but generally arc on the 13 DME towards the ILS of the last landing runway at 4,000’
Aircrew must notify the controlling agency and SOF of their intention to divert prior to?
reaching minimum fuel for diversion
When choosing a divert field, do not fly through marginal weather to the primary, secondary, or designated divert field when?
fuel conditions permit a safe recovery to another suitable field
To the max extent possible, when diverting to a field, fly a(n)?
overhead pattern
What does the diversion chart in the IFG assume?
Max Range (@ 10,000’)
Standard Day
NO WIND
What speed should you fly through thunderstorms?
A penetration airspeed of 180 KIAS is recommended. Do not exceed Turbulent Air Penetration Speed (Vg) of 195 KIAS. Trim the aircraft and do not CHASE the airspeed