1
NATOPS Closed Book Questions with Detailed Verified
Answers (100% Correct Answers) /Already Graded A+
NATOPS publications provide the best available operating instructions for
______. However, no manual can cover everything situation or be a substitute
for _____; operational situations may require modification of the procedures
contained therein. Read these products thoroughly. As an aircrew member, it
is your responsibility to have a ____ knowledge of their contents.
Ans: Most circumstances, sound judgement, complete
Which is not a defined change recommendation for NATOPS changes?
Ans: Immediate
Revised text is indicated by a _____ in the outside margin of the page.
Ans: Black vertical line
Explanatory information about an operating procedure, practice, or condition,
etc., that may result in damage to equipment if not carefully observed or
followed.
Ans: Caution
Explanatory information about an operating procedure, practice or condition,
etc., that may result in injury, or death, or loss of aircraft if not carefully
observed or followed.
Ans: Warning
Explanatory information about an operating procedure, practice, or condition,
etc., that must be emphasized.
Ans: Note
__________ means extended flight is not recommended. The landing sight
and duration of flight are at the discretion of the pilot in command.
Approved By:
vPretest - Stuvia US
,2
Ans: LAND AS SOON AS PRACTICABLE
The MH-60R primary mission include _______
Ans: SUW, ASW, EW, CC, NCO
Secondary missions include ______, Air warfare (AW; e.g LSF) Health services
(HS e.g. MEDIVAC), Fleet support -Operations (FS-O e.g. SAR) _____,
Logistics (LOG; e.g. VERTREP) Combat Search and Rescue (CSAR)
Ans: Amphibious Warfare (AMW; e.g. Naval Surface Fire Support),
Intelligence Operations (INT; e.g. ISR)
______ significantly reduces the field of view and the success rate of obtaining
visual contact with a survivor when performing SAR lookout duties from the
SO window. Due to the visual restrictions, dedicated SAR missions should
consider removal of the _____ to enhance probability of detection / sighting of
survivor
Ans: Left hand extended pylon
Use of the sonobuoy launcher window is _____
Ans: Prohibited
The center rear seat shall be removed if ____
Ans: RAST probe is installed
The Simula seat ______ be removed during flights not requiring its use. When
installed the Simula seat creates an egress hazard for the Aircrewman.
Ans: Should
The primary passenger seat is the ____ seat position during single passenger
flights.
Ans: Instructor
Approved By:
vPretest - Stuvia US
,3
The center rear seat ____ be removed if RAST probe is installed. The RAST
probe prevents proper stroking of the seat in the event of a crash.
Ans: Shall
All essential engine electrical functions are powered by the ____. The engine
____ contains separate windings providing AC power to the igniter assembly,
DECU, and Ng signal to the vertical instruments.
Ans: Alternator
The ____ attenuates the magnitude and reduces the duration of the peak
vibratory loads produced by the main rotor at the main rotor blade passage
vibration frequency.
Ans: AVCS - Active vibration control system
In flight or on deck, the instantaneous nature of the AVCS commanded
vibrations can sometimes cause a vibration spike or a "_____" that is felt
throughout the aircraft. It can range in intensity from barely noticeable to
extremely uncomfortable and excessive.
Ans: Bump
Water-contaminated fuel may cause fluctuations/surges in one or both engines
with no associated ____ or ____ caution.
Ans: FUEL PRESS / FUEL FLTR BYPASS
A pressure refueling port is provided for standard ___-PSI pressure refueling
on the ground without electrical power.
Ans: 55
The minimum accumulator pressure required for starting the APU is
approximately __ PSI. It can be recharged using the accumulator hand pump.
With AC power available, the accumulator is charger by the backup hydraulic
pump.
Ans: 2,650
Approved By:
vPretest - Stuvia US
, 4
With a __ percent charge, normal battery life is 11 minutes for day operations
and 9 minutes for night operations
Ans: 80
During normal system operation, the selection of certain hydraulic systems and
Automatic Flight Control System (AFCS) functions may result in the ____ of
the related cautions.
Ans: Intermittent appearance
The central component of the AFCS is the ____.
Ans: digital AFCC
The crew hover function is activated from the AFCS CONTROL panel by
depressing the CREW HVR push button. It can only be achieved if the ____ is
already engaged.
Ans: Hover coupler mode
The crew hover trim grip has a control authority of +/- ____ KGS laterally and
longitudinally about the reference values selected on the LONG VEL and LAT
VEL in addition to the speed set by the cyclic four-way TRIM switch
Ans: 5
If the ___ outer ring is reached while the dome is in the water, there is a
significantly increased risk of the dome striking the aircraft including the
aircraft rotors which may result in aircrew injury and/or death.
Ans: 8.5 degree
The potentiometers on this panel are used to bias the cable angle sensors away
from the preset manufacturer cable angle sensor calibration and should
normally not require adjustment. In most cases, these potentiometers should
be set at zero (at the ___ o'clock position) prior to flight and not adjusted:
Ans: 12
Approved By:
vPretest - Stuvia US
NATOPS Closed Book Questions with Detailed Verified
Answers (100% Correct Answers) /Already Graded A+
NATOPS publications provide the best available operating instructions for
______. However, no manual can cover everything situation or be a substitute
for _____; operational situations may require modification of the procedures
contained therein. Read these products thoroughly. As an aircrew member, it
is your responsibility to have a ____ knowledge of their contents.
Ans: Most circumstances, sound judgement, complete
Which is not a defined change recommendation for NATOPS changes?
Ans: Immediate
Revised text is indicated by a _____ in the outside margin of the page.
Ans: Black vertical line
Explanatory information about an operating procedure, practice, or condition,
etc., that may result in damage to equipment if not carefully observed or
followed.
Ans: Caution
Explanatory information about an operating procedure, practice or condition,
etc., that may result in injury, or death, or loss of aircraft if not carefully
observed or followed.
Ans: Warning
Explanatory information about an operating procedure, practice, or condition,
etc., that must be emphasized.
Ans: Note
__________ means extended flight is not recommended. The landing sight
and duration of flight are at the discretion of the pilot in command.
Approved By:
vPretest - Stuvia US
,2
Ans: LAND AS SOON AS PRACTICABLE
The MH-60R primary mission include _______
Ans: SUW, ASW, EW, CC, NCO
Secondary missions include ______, Air warfare (AW; e.g LSF) Health services
(HS e.g. MEDIVAC), Fleet support -Operations (FS-O e.g. SAR) _____,
Logistics (LOG; e.g. VERTREP) Combat Search and Rescue (CSAR)
Ans: Amphibious Warfare (AMW; e.g. Naval Surface Fire Support),
Intelligence Operations (INT; e.g. ISR)
______ significantly reduces the field of view and the success rate of obtaining
visual contact with a survivor when performing SAR lookout duties from the
SO window. Due to the visual restrictions, dedicated SAR missions should
consider removal of the _____ to enhance probability of detection / sighting of
survivor
Ans: Left hand extended pylon
Use of the sonobuoy launcher window is _____
Ans: Prohibited
The center rear seat shall be removed if ____
Ans: RAST probe is installed
The Simula seat ______ be removed during flights not requiring its use. When
installed the Simula seat creates an egress hazard for the Aircrewman.
Ans: Should
The primary passenger seat is the ____ seat position during single passenger
flights.
Ans: Instructor
Approved By:
vPretest - Stuvia US
,3
The center rear seat ____ be removed if RAST probe is installed. The RAST
probe prevents proper stroking of the seat in the event of a crash.
Ans: Shall
All essential engine electrical functions are powered by the ____. The engine
____ contains separate windings providing AC power to the igniter assembly,
DECU, and Ng signal to the vertical instruments.
Ans: Alternator
The ____ attenuates the magnitude and reduces the duration of the peak
vibratory loads produced by the main rotor at the main rotor blade passage
vibration frequency.
Ans: AVCS - Active vibration control system
In flight or on deck, the instantaneous nature of the AVCS commanded
vibrations can sometimes cause a vibration spike or a "_____" that is felt
throughout the aircraft. It can range in intensity from barely noticeable to
extremely uncomfortable and excessive.
Ans: Bump
Water-contaminated fuel may cause fluctuations/surges in one or both engines
with no associated ____ or ____ caution.
Ans: FUEL PRESS / FUEL FLTR BYPASS
A pressure refueling port is provided for standard ___-PSI pressure refueling
on the ground without electrical power.
Ans: 55
The minimum accumulator pressure required for starting the APU is
approximately __ PSI. It can be recharged using the accumulator hand pump.
With AC power available, the accumulator is charger by the backup hydraulic
pump.
Ans: 2,650
Approved By:
vPretest - Stuvia US
, 4
With a __ percent charge, normal battery life is 11 minutes for day operations
and 9 minutes for night operations
Ans: 80
During normal system operation, the selection of certain hydraulic systems and
Automatic Flight Control System (AFCS) functions may result in the ____ of
the related cautions.
Ans: Intermittent appearance
The central component of the AFCS is the ____.
Ans: digital AFCC
The crew hover function is activated from the AFCS CONTROL panel by
depressing the CREW HVR push button. It can only be achieved if the ____ is
already engaged.
Ans: Hover coupler mode
The crew hover trim grip has a control authority of +/- ____ KGS laterally and
longitudinally about the reference values selected on the LONG VEL and LAT
VEL in addition to the speed set by the cyclic four-way TRIM switch
Ans: 5
If the ___ outer ring is reached while the dome is in the water, there is a
significantly increased risk of the dome striking the aircraft including the
aircraft rotors which may result in aircrew injury and/or death.
Ans: 8.5 degree
The potentiometers on this panel are used to bias the cable angle sensors away
from the preset manufacturer cable angle sensor calibration and should
normally not require adjustment. In most cases, these potentiometers should
be set at zero (at the ___ o'clock position) prior to flight and not adjusted:
Ans: 12
Approved By:
vPretest - Stuvia US
