NATOPS QUESTIONS AND ANSWERS
The NATOPS manual covers all of the information necessary for the aircraft's
safe and effective operation. These instructions give a broad overview of the
aircraft, its characteristics, and special _______ and _______ emergency
procedures. - ANSWER KNOWLEDGE.
NORMAL AND EMERGENCY
Under most circumstances, the NATOPS manual gives the best available
operational instructions; however, it is not a substitute for ________________. -
ANSWER SOUND JUDGMENT.
WARNING - ANSWER An operating process, practice, etc., that, if not
followed correctly, may result in bodily injury or death.
CAUTION - ANSWER An operating technique, practice, etc., that, if not
rigorously followed, may cause equipment damage or destruction.
NOTE - ANSWER An operational technique, condition, etc. that must be
emphasized.
SHALL/WILL- ANSWER indicates a necessary necessity.
SHOULD - ANSWER indicates a NON-MANDATORY, desirable, or
recommended manner of completion.
MAY - ANSWER indicates an acceptable or advised method of completion.
A chip detector is installed in the ____________ to detect ______ in the oil. -
ANSWER RGB.
,Ferrous material
If the PMU function is lost or deactivated, the mechanical flyweight overspeed
governor adjusts oil pressure to the propeller pitch change piston to keep Np at
or below _____. - ANSWER: 100% +/-2%
The starter and ignition switches are placed in ______ cockpits. ANSWER
BOTH.
A flexible cable connects the front PCL (electrically and mechanically) to the
FMU (fuel management unit).
The ____________ checks engine running parameters and displays the relevant
annunciation as needed. - ANSWER EDM (Engine Data Manager)
A fire warning system test switch labelled ____________ is located on the
____________ left console test panel to ensure the electrical continuity of the
two fire warning systems. - Answer Fire,
FRONT
The firewall shutoff handle, which is positioned on the front left console panel,
mechanically operates cables to close ____________ at the firewall, cut
____________ and ____________ to the engine, and turn off ____________
from the engine. ANSWER VALVES
FUEL,
Hydraulic fluid,
Bleed air
,The left and right wing tanks have a capacity of around ____________ pounds
each. The centre collector tank contains about. Weight: ____________ pounds.
ANSWER 527,
47
To reset the auto balance system and the 2-minute timer, move the
_______________ switch to ____________ and then back to the
_____________ position. - Answer FUEL BALANCE.
MAN RESET
AUTO
During the inverted flight, a weighted rod in the pickup valve switches off the
standard fuel pickup and opens the "inverted flight fuel pickup". This ensures a
minimum of ____________ of fuel regardless of direction. - ANSWER: 60
SECONDS
If the ____________ and ____________ fail, the engine-driven high-pressure
fuel pump will suction feed enough gasoline for the engine to continue
operating. - ANSWER: Electric Boost Pump,
Engine-driven low-pressure fuel pump
If the engine-driven high-pressure pump breaks, the engine will fail and cannot
be restarted. - ANSWER FLAME OUT.
, RESTARTED
The generator generates ____________ of power, which is enough to run all of
the equipment on the ____________ and ____________ buses and charge the
____________. - ANSWER: 28 VDC GENERATOR
BATTERY,
BATTERY.
The generator control switches, placarded gen, situated in each cockpit, are
magnetically and electrically connected, allowing the generator to be controlled
from the cockpit. - ANSWER HELD ON.
INTERLOCKED
If the bus tie fails or is set to ____________, the amber BUS tie annunciator
will illuminate, along with the battery and generator buses. Expect a minimum
of ____________ of battery power for the battery bus components. - ANSWER
OPEN.
SEPARATING,
Thirty minutes
The quantity of braking employed is determined by the pilot's application of the
______ pedal power. - ANSWER MOST.
The NATOPS manual covers all of the information necessary for the aircraft's
safe and effective operation. These instructions give a broad overview of the
aircraft, its characteristics, and special _______ and _______ emergency
procedures. - ANSWER KNOWLEDGE.
NORMAL AND EMERGENCY
Under most circumstances, the NATOPS manual gives the best available
operational instructions; however, it is not a substitute for ________________. -
ANSWER SOUND JUDGMENT.
WARNING - ANSWER An operating process, practice, etc., that, if not
followed correctly, may result in bodily injury or death.
CAUTION - ANSWER An operating technique, practice, etc., that, if not
rigorously followed, may cause equipment damage or destruction.
NOTE - ANSWER An operational technique, condition, etc. that must be
emphasized.
SHALL/WILL- ANSWER indicates a necessary necessity.
SHOULD - ANSWER indicates a NON-MANDATORY, desirable, or
recommended manner of completion.
MAY - ANSWER indicates an acceptable or advised method of completion.
A chip detector is installed in the ____________ to detect ______ in the oil. -
ANSWER RGB.
,Ferrous material
If the PMU function is lost or deactivated, the mechanical flyweight overspeed
governor adjusts oil pressure to the propeller pitch change piston to keep Np at
or below _____. - ANSWER: 100% +/-2%
The starter and ignition switches are placed in ______ cockpits. ANSWER
BOTH.
A flexible cable connects the front PCL (electrically and mechanically) to the
FMU (fuel management unit).
The ____________ checks engine running parameters and displays the relevant
annunciation as needed. - ANSWER EDM (Engine Data Manager)
A fire warning system test switch labelled ____________ is located on the
____________ left console test panel to ensure the electrical continuity of the
two fire warning systems. - Answer Fire,
FRONT
The firewall shutoff handle, which is positioned on the front left console panel,
mechanically operates cables to close ____________ at the firewall, cut
____________ and ____________ to the engine, and turn off ____________
from the engine. ANSWER VALVES
FUEL,
Hydraulic fluid,
Bleed air
,The left and right wing tanks have a capacity of around ____________ pounds
each. The centre collector tank contains about. Weight: ____________ pounds.
ANSWER 527,
47
To reset the auto balance system and the 2-minute timer, move the
_______________ switch to ____________ and then back to the
_____________ position. - Answer FUEL BALANCE.
MAN RESET
AUTO
During the inverted flight, a weighted rod in the pickup valve switches off the
standard fuel pickup and opens the "inverted flight fuel pickup". This ensures a
minimum of ____________ of fuel regardless of direction. - ANSWER: 60
SECONDS
If the ____________ and ____________ fail, the engine-driven high-pressure
fuel pump will suction feed enough gasoline for the engine to continue
operating. - ANSWER: Electric Boost Pump,
Engine-driven low-pressure fuel pump
If the engine-driven high-pressure pump breaks, the engine will fail and cannot
be restarted. - ANSWER FLAME OUT.
, RESTARTED
The generator generates ____________ of power, which is enough to run all of
the equipment on the ____________ and ____________ buses and charge the
____________. - ANSWER: 28 VDC GENERATOR
BATTERY,
BATTERY.
The generator control switches, placarded gen, situated in each cockpit, are
magnetically and electrically connected, allowing the generator to be controlled
from the cockpit. - ANSWER HELD ON.
INTERLOCKED
If the bus tie fails or is set to ____________, the amber BUS tie annunciator
will illuminate, along with the battery and generator buses. Expect a minimum
of ____________ of battery power for the battery bus components. - ANSWER
OPEN.
SEPARATING,
Thirty minutes
The quantity of braking employed is determined by the pilot's application of the
______ pedal power. - ANSWER MOST.
