1
NATOPS (T6A) - NEW Questions with Detailed Verified
Answers (100% Correct Answers) /Already Graded A+
*Warning
Ans: Operating procedure that could result in personal injury or loss of life if
not followed
Caution
Ans: Operating procedure that could result in damage to the aircraft if not
followed
Note
Ans: Operating procedure that is considered essential to emphasize
*Shall/Will
Ans: Mandatory requirement
*Should
Ans: Desired/Preferred method
May
Ans: Suggested method
Chip detector:
-Location?
-Function?
Ans: -Top of RGB
-Detect ferrous material in oil
*If PMU function is lost/deactivated, the __________________________
resets to modulate oil pressure to the propeller pitch change piston to
maintain ___________ at or below ______________?
Approved By:
vPretest - Stuvia US
,2
Ans: mechanical overspeed governor; Np; 100+/-2%
*T/F: Starter and Ignition switches located in both cockpits?
Ans: True
A flexible cable connects the PCL to the ______________
Ans: FMU
____________________ monitors engine operating parameters and
illuminates the appropriate annunciator when necessary.
Ans: Engine data manager
*A fire warning system test switch, labeled ________________, is provided
on the _________________ left console test panel to verify the electrical
continuity of the two fire warning systems.
Ans: FIRE; Front Cockpit
The firewall shutoff handle, located on the front left console panel,
mechanically operates cables to close _____________ at the firewall, cutting
off ___________ and ______________ to the engine as well as cutting off
____________________ from the engine.
Ans: valves; fuel; hydraulic fluid; bleed air
Left and right wing tanks have a capacity of approximately ____________ lbs
each, while the collector tank holds approximately ______________ lbs.
Ans: 527; 47
To reset the auto balance system and the 2-minute timer, place the
_______________ switch to ____________ then return it to the
_____________ position.
Ans: fuel balance; manual/reset; auto
Approved By:
vPretest - Stuvia US
, 3
*During inverted flight, a weighted rod in the pickup valve closes off the
normal fuel pickup, and opens the inverted flight fuel pickup providing a
minimum of ____________ seconds of fuel regardless of orientation.
Ans: 60
If both the _____________ and the ________________ fail, the engine-
driven high pressure fuel pump will suction feed sufficient fuel for continued
engine operation.
Ans: electric boost pump; engine-driven low-pressure pump
*If the engine-driven high pressure pump fails, the engine will _______ and
cannot be _____________?
Ans: flame out; restarted
*If the bus tie fails, or is set to ___________, the amber BUS TIE annunciator
will illuminate, _______________ the battery and generator buses. Expect a
minimum of _____________ minutes of battery power to the battery bus
items.
Ans: OPEN; separating; 30
The pilot applying the ____________ pedal force determines the amount of
brake force used.
Ans: most
The system is ________________ actuated and ___________________
sequenced to extend and retract the landing gear and main gear doors.
Ans: hydraulically; electrically
*The aural landing gear position warning is a 250Hz tone repeated 5x per
second, transmitted through the audio system, and activates when any one of
the following conditions exist?
Approved By:
vPretest - Stuvia US
NATOPS (T6A) - NEW Questions with Detailed Verified
Answers (100% Correct Answers) /Already Graded A+
*Warning
Ans: Operating procedure that could result in personal injury or loss of life if
not followed
Caution
Ans: Operating procedure that could result in damage to the aircraft if not
followed
Note
Ans: Operating procedure that is considered essential to emphasize
*Shall/Will
Ans: Mandatory requirement
*Should
Ans: Desired/Preferred method
May
Ans: Suggested method
Chip detector:
-Location?
-Function?
Ans: -Top of RGB
-Detect ferrous material in oil
*If PMU function is lost/deactivated, the __________________________
resets to modulate oil pressure to the propeller pitch change piston to
maintain ___________ at or below ______________?
Approved By:
vPretest - Stuvia US
,2
Ans: mechanical overspeed governor; Np; 100+/-2%
*T/F: Starter and Ignition switches located in both cockpits?
Ans: True
A flexible cable connects the PCL to the ______________
Ans: FMU
____________________ monitors engine operating parameters and
illuminates the appropriate annunciator when necessary.
Ans: Engine data manager
*A fire warning system test switch, labeled ________________, is provided
on the _________________ left console test panel to verify the electrical
continuity of the two fire warning systems.
Ans: FIRE; Front Cockpit
The firewall shutoff handle, located on the front left console panel,
mechanically operates cables to close _____________ at the firewall, cutting
off ___________ and ______________ to the engine as well as cutting off
____________________ from the engine.
Ans: valves; fuel; hydraulic fluid; bleed air
Left and right wing tanks have a capacity of approximately ____________ lbs
each, while the collector tank holds approximately ______________ lbs.
Ans: 527; 47
To reset the auto balance system and the 2-minute timer, place the
_______________ switch to ____________ then return it to the
_____________ position.
Ans: fuel balance; manual/reset; auto
Approved By:
vPretest - Stuvia US
, 3
*During inverted flight, a weighted rod in the pickup valve closes off the
normal fuel pickup, and opens the inverted flight fuel pickup providing a
minimum of ____________ seconds of fuel regardless of orientation.
Ans: 60
If both the _____________ and the ________________ fail, the engine-
driven high pressure fuel pump will suction feed sufficient fuel for continued
engine operation.
Ans: electric boost pump; engine-driven low-pressure pump
*If the engine-driven high pressure pump fails, the engine will _______ and
cannot be _____________?
Ans: flame out; restarted
*If the bus tie fails, or is set to ___________, the amber BUS TIE annunciator
will illuminate, _______________ the battery and generator buses. Expect a
minimum of _____________ minutes of battery power to the battery bus
items.
Ans: OPEN; separating; 30
The pilot applying the ____________ pedal force determines the amount of
brake force used.
Ans: most
The system is ________________ actuated and ___________________
sequenced to extend and retract the landing gear and main gear doors.
Ans: hydraulically; electrically
*The aural landing gear position warning is a 250Hz tone repeated 5x per
second, transmitted through the audio system, and activates when any one of
the following conditions exist?
Approved By:
vPretest - Stuvia US
