NATOPS Exam Questions 100% Correct Answers Verified Latest 2024 Version
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NATOPS Exam Questions | 100% Correct
Answers | Verified | Latest 2024 Version
The NATOPS manual contains the necessary information for safe and efficient operation of the aircraft.
These instructions provide a general ____ of the aircraft, its characteristics, and specific ____ and ____
procedu...
NATOPS Exam Questions | 100% Correct
Answers | Verified | Latest 2024 Version
The NATOPS manual contains the necessary information for safe and efficient operation of the aircraft.
These instructions provide a general ____ of the aircraft, its characteristics, and specific ____ and ____
procedures. - ✔✔knowledge, normal, emergency
The NATOPS manual provides the best possible operating instructions under most circumstances, but it
is not a substitute for ______ - ✔✔sound judgement
Define warning: - ✔✔An operating procedure, technique, etc. which could result in a personal injury or
loss of life if not carefully followed.
Define caution: - ✔✔An operating procedure, technique, etc. which could result in damage to equipment
if not carefully followed.
Define note: - ✔✔An operating procedure, technique, etc. which is considered essential to emphasize.
Define should: - ✔✔Indicates a non-mandatory, desired, or preferred method of accomplishment
Define may: - ✔✔Indicates an acceptable or suggested means of accomplishment
A chip detector is mounted in the ____ to detect ____ in the oil. - ✔✔reduction gear box (RGB), ferrous
material
If PMU function is lost or deactivated, the mechanical overspeed governor resets to modulate oil
pressure to the propeller pitch change piston to maintain Np at or below ____. - ✔✔100 +- 2%
The Starter and Ignition switches are located in ____ cockpits. - ✔✔both
,A flexible cable connects the front PCL (electrically and mechanically) to the ____. - ✔✔fuel
management unit (FMU)
The ____ monitors engine operating parameters and illuminates the appropriate annunciator when
necessary. - ✔✔engine data manager (EDM)
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. - ✔✔FIRE, front
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.
- ✔✔valves, fuel, hydraulic fluid, bleed air
The left and right wing tanks have a capacity of approximately ____ pounds each (JP5/JP8). The central
collector tank holds approximately ____ pounds. - ✔✔527, 47
To reset the auto balance system and the 2-minute timer, place the ____ switch to ____ then return it to
the ____ position. - ✔✔FUEL BAL, MAN/RESET, AUTO
During inverted flight, a weighted rod in the pickup valve closes off the normal fuel pickup, and opens
the inverted flight fuel pickup. This provides a minimum of ____ of fuel regardless of orientation. - ✔✔60
seconds
If both the ____ and the ____ fail, the engine-driven high pressure fuel pump will suction feed sufficient
fuel for continued engine operation. - ✔✔electric boost pump, engine-driven low pressure pump
If the engine-driven high pressure pump fails, the engine will ____ and cannot be ____ - ✔✔flame out,
restarted
The generator provides ____ of power, which is sufficient to operate all the equipment on the ____ and
____ busses, and charge the ____. - ✔✔28VDC, generator, battery, battery
, The generator control switches, placarded GEN, located in ____ cockpit, are magnetically ____ and
electrically ____, which allows the generator to be controlled from ____ cockpit - ✔✔each, held on,
interlocked, each
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 ____ of battery power to the battery bus items. - ✔✔OPEN,
separating, 30 minutes
The pilot applying the ____ pedal force determines the amount of braking being used. - ✔✔most
The system is ____ actuated and ____ sequenced to extend and retract the landing gear and main gear
doors. - ✔✔hydraulically, electrically
The aural landing gear position warning is a 250 Hz tone repeated 5 times per second, transmitted
through the audio system and activates when any one of the following conditions exist: - ✔✔1. gear
handle not down, PCL below mid-range position (~87% N1), airspeed below 120 KIAS, and flaps up or in
takeoff
2. All gear not indicating down and locked with flaps landing
3. Weight on wheels with gear handle not down
An electromechanical actuator, installed in the center wing, is connected to a spring box assembly and
the centerline bellcrank to provide aileron (____) trim by actually moving the ____. - ✔✔roll, ailerons
A gust lock system is provided in the ____ to lock the aileron and rudder surfaces in the ____ position,
and the elevator in a ___ configuration when the aircraft is parked. - ✔✔front cockpit, neutral, down
The gust lock is disengaged by ____, ____, and ____ to the stowed position. - ✔✔lifting the yoke, moving
the control stick to the side and then aft, lowering the yoke
The stick shaker is activated at approximately ____ above stall speed (____). - ✔✔5 -10 kts, 15-16 units
An internal CFS handle, located on the ____ console behind the PCL in ____ cockpit, allows manual
activation of the fracturing system for the transparency over the ____ cockpit. - ✔✔left, each, respective
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