MH-65E STAN Bank Complete Latest set
with Questions and correct Answers
TRUE/FALSE: The main gearbox and engines share the same overtemp warning. - correct
answer- ✅FALSE
TRUE/FALSE: Following the first engine start, even though the MFDs are operating, the CDU
TDL pages should be used
as a primary reference for the second engine start. - correct answer- ✅TRUE
The System Manager partitions are contained in which MFDs?
A. 1 & 2
B. 2 & 3
C. 3 & 4
D. 1 & 4 - correct answer- ✅D. 1 & 4
TRUE/FALSE: There will be no aural warning if the Flight Director becomes uncoupled from the
AFCS. - correct answer- ✅FALSE
In the event that primary flight information is lost on the MFDs, the __________ can be
referenced for airspeed, attitude, and heading. - correct answer- ✅SFI
The _______________ Page is the primary source for diagnosing and analyzing any warning,
caution or advisory
annunciation. - correct answer- ✅ENGINE INDICATING AND CREW ALERTING SYSTEM
(EICAS)
Which bus is not affected when placing the Emergency Electrical Cutoff Switch to OFF? -
correct answer- ✅BATTERY BUS
The Aerosonic Sensor Unit (ASU) of the SFI accepts pitot (total) and static pressure input from
the _______________ Pitot/Static System. - correct answer- ✅PILOT'S/NO. 2
The Static Bypass Switch for the _______________ static system is located on the
_______________. - correct answer- ✅PILOT'S/NO. 2
AVIONICS RACK
PANEL
The alternate static pressure valve is used to switch from the _______________ static pressure
ports to
_________________________ pressure in the event of icing or an obstruction. - correct
answer- ✅EXTERNAL
,INTERNAL CABIN
When using the training switch, the idled engine spools down to ____ RPM N2 at a
preprogrammed rate and the good
engine will increase power up to approximately 62% torque. - correct answer- ✅320 RPM
A safety feature built into the training switch FADEC logic ensures that the idled engine will
provide power up to the actual ______ stop in the event of NR mismanagement. - correct
answer- ✅OEI
TRUE/FALSE: The First Limit (N1, TOT or Torque) is displayed on the right corner of the PFD. -
correct answer- ✅FALSE
TRUE/FALSE: Once an engine is shutdown by the DECU via the BIM, overspeed protection is
automatically inhibited on the second engine - correct answer- ✅TRUE
____ and _____ components are labeled conventionally, No. 1 for the left side and No. 2 for the
right side. - correct answer- ✅AIRFRAME and AVIONICS
Aircrew shall not use the _______ if a Level 1 FADEC failure is noted. - correct answer-
✅TRNG SWITCH
The lift capability of the rotor system is limited by the actual collective stop and NR will not
increase above ______ RPM in the Training Mode until the collective is reduced to a power
level below the good engine topping. - correct answer- ✅320
A Level _______ FADEC (redundancy failure) can be accessed by selecting the Engine Faults
page on the CDU. - correct answer- ✅Level 1
A Level FADEC _______ failure is indicated on the EICAS page with a GOV LVL 1 caution when
the FADEC control switch is in the IDLE or OFF position. - correct answer- ✅Level 1
A Level 1 FADEC failure is indicated on the EICAS page with a _______ caution when the
FADEC control switch is in the IDLE or OFF position. - correct answer- ✅GOV LVL 1
A Level ___ FADEC failure is indicated on the EICAS page with a GOV LVL 2 caution. - correct
answer- ✅Level 2
A Level 2 FADEC failure is indicated on the EICAS page with a caution.
A. GOV LVL 1
B. GOV LVL 2
C. NONREDUNDANT FAILURE
D. FADEC FAIL - correct answer- ✅B. GOV LVL 2
Level _____ , or major FADEC failure is indicated on the EICAS page with a FADEC1/FADEC2
FAIL caution along with illumination of the red engine status light. - correct answer- ✅Level 3
Level 3, or major FADEC failure is indicated on the EICAS page with a FADEC1/FADEC2 FAIL
caution along with illumination of the red ______. - correct answer- ✅ENGINE STATUS LIGHT
, TRUE/FALSE: During a Level 3 FADEC Failure, fuel flow on the affected engine will be frozen at
its present value. - correct answer- ✅TRUE
Due to FADEC logic, returning the TRNG switch back to the flight position should be completed
with the PFD Torque Display less than _____% and the NR stable at 355 RPM (or 365 RPM) to
preclude use of _______ . - correct answer- ✅40%
ACTUAL OEI TIMES
The NR HI mode is used during hover flight, single engine operations, and other demanding low
speed maneuvers as it provides a greater margin for NR droop as well as .
A. increased engine performance
B. increased tail rotor authority
C. increased torque margin
D. significantly greater lift capability - correct answer- ✅B. increased tail rotor authority
When one or more of the parameters associated with an engine are in the caution range, the
data display label and perimeter (box) will be ______ . In the warning range, the data display
label and perimeter (box) will be ______ . - correct answer- ✅Yellow
Red
No fire extinguishing capability is provided for the _____ . - correct answer- ✅MAIN GEARBOX
COMPARTMENT
If operating above _____ ft MSL, both boost pumps shall be on to prevent a possible feed tank
failure. - correct answer- ✅8000 ft
(Circle One) Indicated / Actual fuel is determined at a nose level attitude. - correct answer-
✅Actual
In the normal hover attitude (4 degree nose up), indicated fuel is approximately _____% less
than actual fuel. - correct answer- ✅10%
When the fuel quantity on the individual side drops to _____ lbs., the respective fuel quantity
and tape will turn yellow. - correct answer- ✅100 lbs
TRUE/FALSE: When the LEFT or RIGHT fuel displays drops to zero pounds, the respective
feed tank light will illuminate. - correct answer- ✅FALSE
Failure of the left forward ejector, aft cell ejector or both boost pumps will result in trapped fuel
and the only indication to the aircrew will be illumination of the corresponding _______ warning
on the EICAS page. - correct answer- ✅FEED TANK
TRUE/FALSE: Placing the emergency electrical cutoff switch to CUTOFF removes power to the
2000 psi isolation valve, - correct answer- ✅TRUE
with Questions and correct Answers
TRUE/FALSE: The main gearbox and engines share the same overtemp warning. - correct
answer- ✅FALSE
TRUE/FALSE: Following the first engine start, even though the MFDs are operating, the CDU
TDL pages should be used
as a primary reference for the second engine start. - correct answer- ✅TRUE
The System Manager partitions are contained in which MFDs?
A. 1 & 2
B. 2 & 3
C. 3 & 4
D. 1 & 4 - correct answer- ✅D. 1 & 4
TRUE/FALSE: There will be no aural warning if the Flight Director becomes uncoupled from the
AFCS. - correct answer- ✅FALSE
In the event that primary flight information is lost on the MFDs, the __________ can be
referenced for airspeed, attitude, and heading. - correct answer- ✅SFI
The _______________ Page is the primary source for diagnosing and analyzing any warning,
caution or advisory
annunciation. - correct answer- ✅ENGINE INDICATING AND CREW ALERTING SYSTEM
(EICAS)
Which bus is not affected when placing the Emergency Electrical Cutoff Switch to OFF? -
correct answer- ✅BATTERY BUS
The Aerosonic Sensor Unit (ASU) of the SFI accepts pitot (total) and static pressure input from
the _______________ Pitot/Static System. - correct answer- ✅PILOT'S/NO. 2
The Static Bypass Switch for the _______________ static system is located on the
_______________. - correct answer- ✅PILOT'S/NO. 2
AVIONICS RACK
PANEL
The alternate static pressure valve is used to switch from the _______________ static pressure
ports to
_________________________ pressure in the event of icing or an obstruction. - correct
answer- ✅EXTERNAL
,INTERNAL CABIN
When using the training switch, the idled engine spools down to ____ RPM N2 at a
preprogrammed rate and the good
engine will increase power up to approximately 62% torque. - correct answer- ✅320 RPM
A safety feature built into the training switch FADEC logic ensures that the idled engine will
provide power up to the actual ______ stop in the event of NR mismanagement. - correct
answer- ✅OEI
TRUE/FALSE: The First Limit (N1, TOT or Torque) is displayed on the right corner of the PFD. -
correct answer- ✅FALSE
TRUE/FALSE: Once an engine is shutdown by the DECU via the BIM, overspeed protection is
automatically inhibited on the second engine - correct answer- ✅TRUE
____ and _____ components are labeled conventionally, No. 1 for the left side and No. 2 for the
right side. - correct answer- ✅AIRFRAME and AVIONICS
Aircrew shall not use the _______ if a Level 1 FADEC failure is noted. - correct answer-
✅TRNG SWITCH
The lift capability of the rotor system is limited by the actual collective stop and NR will not
increase above ______ RPM in the Training Mode until the collective is reduced to a power
level below the good engine topping. - correct answer- ✅320
A Level _______ FADEC (redundancy failure) can be accessed by selecting the Engine Faults
page on the CDU. - correct answer- ✅Level 1
A Level FADEC _______ failure is indicated on the EICAS page with a GOV LVL 1 caution when
the FADEC control switch is in the IDLE or OFF position. - correct answer- ✅Level 1
A Level 1 FADEC failure is indicated on the EICAS page with a _______ caution when the
FADEC control switch is in the IDLE or OFF position. - correct answer- ✅GOV LVL 1
A Level ___ FADEC failure is indicated on the EICAS page with a GOV LVL 2 caution. - correct
answer- ✅Level 2
A Level 2 FADEC failure is indicated on the EICAS page with a caution.
A. GOV LVL 1
B. GOV LVL 2
C. NONREDUNDANT FAILURE
D. FADEC FAIL - correct answer- ✅B. GOV LVL 2
Level _____ , or major FADEC failure is indicated on the EICAS page with a FADEC1/FADEC2
FAIL caution along with illumination of the red engine status light. - correct answer- ✅Level 3
Level 3, or major FADEC failure is indicated on the EICAS page with a FADEC1/FADEC2 FAIL
caution along with illumination of the red ______. - correct answer- ✅ENGINE STATUS LIGHT
, TRUE/FALSE: During a Level 3 FADEC Failure, fuel flow on the affected engine will be frozen at
its present value. - correct answer- ✅TRUE
Due to FADEC logic, returning the TRNG switch back to the flight position should be completed
with the PFD Torque Display less than _____% and the NR stable at 355 RPM (or 365 RPM) to
preclude use of _______ . - correct answer- ✅40%
ACTUAL OEI TIMES
The NR HI mode is used during hover flight, single engine operations, and other demanding low
speed maneuvers as it provides a greater margin for NR droop as well as .
A. increased engine performance
B. increased tail rotor authority
C. increased torque margin
D. significantly greater lift capability - correct answer- ✅B. increased tail rotor authority
When one or more of the parameters associated with an engine are in the caution range, the
data display label and perimeter (box) will be ______ . In the warning range, the data display
label and perimeter (box) will be ______ . - correct answer- ✅Yellow
Red
No fire extinguishing capability is provided for the _____ . - correct answer- ✅MAIN GEARBOX
COMPARTMENT
If operating above _____ ft MSL, both boost pumps shall be on to prevent a possible feed tank
failure. - correct answer- ✅8000 ft
(Circle One) Indicated / Actual fuel is determined at a nose level attitude. - correct answer-
✅Actual
In the normal hover attitude (4 degree nose up), indicated fuel is approximately _____% less
than actual fuel. - correct answer- ✅10%
When the fuel quantity on the individual side drops to _____ lbs., the respective fuel quantity
and tape will turn yellow. - correct answer- ✅100 lbs
TRUE/FALSE: When the LEFT or RIGHT fuel displays drops to zero pounds, the respective
feed tank light will illuminate. - correct answer- ✅FALSE
Failure of the left forward ejector, aft cell ejector or both boost pumps will result in trapped fuel
and the only indication to the aircrew will be illumination of the corresponding _______ warning
on the EICAS page. - correct answer- ✅FEED TANK
TRUE/FALSE: Placing the emergency electrical cutoff switch to CUTOFF removes power to the
2000 psi isolation valve, - correct answer- ✅TRUE
