NATOPS Question Bank Flashcards
The MV-22 is a multi-mission aircraft with many applications. These applications include the following:
- Medium lift assault support
- Tactical Recovery of Aircraft and Personnel (TRAP)
- Emergency Evacuation
- Fleet logistics support
- Logistics support ashore
- Long range logistics support
- Medical Evacuation
The maximum VTOL gross weight of the V-22 is ___ lbs sea level; maximum Short Takeoff (STO) gross weight is ___ lbs; and maximum alternate gross weight is ___ lbs.
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The nose to tail length of the V-22 is ___ ft ___ in.
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The ______ ______ ______ is the primary interface between the flight crew, the aircraft systems, and avionics.
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When power is applied, ______ MC is designated as ______. the other MC then operates as the ______. the ______ receives all commands and data, performs the required routines, and monitors the ______ computer.
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Each ______ controls operation of ______ MFDs, with the capability of controlling ______ ______ MFDs in the event of a ______ failure.
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There are five main Aircraft Interface Units (AIUs) on the aircraft: the Avionics Bay Interface Unit (ABIU), two ______ ______ ______, the ______ ______ ______, and the Drive Systems Interface Unit (DSIU).
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An AIU text status page does not exist for the ______.
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The DSIU, located on the midwing forward equipment shelf, monitors and controls the ______ ______ ______, and monitors for oil debris in the ______, TABGs, MWGBs, and ______ ______.
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The APN-194 radar altimeter provides aircraft altitude above ground level (AGL) from ___ to approximately ___ ft.
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The ______ ______ ______ provides pitot-static pressure data to the FCCs.
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Stall warning is provided for nacelle angles between ___° and ___°.
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The ______ ______ warning is initiated when the vertical velocity exceeds the vertical velocity limit with airspeed less than ___ kts and nacelle angle greater than ___°.
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The operator can select MFD modes by depressing the bezel key associated with the desired function or by using the ______ ______.
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______ remain displayed until the condition which caused the ______ no longer exists.
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______ and ______ are only displayed on the MFDs when the MFDs are in the CDU backup mode.
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If the aircraft was ______ ______ without a proper system log off, the MCs will attempt to restore the aircraft configuration available prior to loss of power. this is referred to as a ______ _____.
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The Aircraft Start-Up Control Layer, on MFDs, provides three options:
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______ - Situation or condition requiring immediate attention but not necessarily immediate action. Nonroutine action required to avoid or prevent equipment damage, comprise safety, or preclude a warning condition. Operator must take action to correct caution and/or land as soon as possible.
______ - System or mission limiting abnormal condition(s) exists; i.e., loss of redundancy or degradation within a redundant system, which may require operator action, but no specific crew action (e.g., HYD 1 RSVR LO).
______ - Situation or condition requiring immediate action and/or land immediately is dictated to prevent death, injury, equipment damage, or mission abort. Operator must take critical steps without reference to checklist or other aids.
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There are 17 signals that prompt a voice warning:
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______ are indicated by illumination of the ______ ______ light, a text message displayed as ______ characters in a ______ box near the top of the MFDs, and a voice alert.
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Cautions and advisories are arranged from top to bottom based upon _________________ associated with the condition being alerted.
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In the event of an EICAS failure, the ______ will be treated as ______ and displayed on all MFD layers and incorporated in the ______ summary list on the MFDs.
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______ ______ ______ provide information on data entry problems and interactive operation messages.
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______ ______ ______ are presented in the display field in the upper center of the CDU/EICAS in ______ characters.
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The Standby Flight Display, located above the CDU on the instrument panel, provides for the independent backup of ______, ______, and ______ ______ parameters exclusive of the ______.
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There are a total of ___ display layers for each pilot [on the HUD]. The display layers available are ______ and ______. The two primary layers’ corresponding de-clutter layers are identified by de-clutter markers: ___ and ___.
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Output power is transferred to the Proprotor Gearbox (PRGB) by the ______ ______, located in the center of the ______ assembly.
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The ______ also provides ______ ______ against damage due to exceedence of limits on engine gas generator (Ng), power turbine speed (Np), turbine temperature (MGT), and output shaft torque (Qe).
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The FADECs transmit information to each other through a ______ ______ ______ ______ commonly referred to as cross-talk.
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The primary mode of operation is one FADEC actively controlling each engine, while the second FADEC is in ______.
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The ______ ______ ______ ______ controls fuel flow and pressure in response to signals from the FADECs.
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The ______ ______ control is configured so that when it is in the ON position, it mechanically prohibits the ECLs from moving past the ______ position.
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Forward or aft movement of the TCL is translated by the FCCs into a ______ ______ ______ that is sent to the FADECs.
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The INTERIM POWER push button switch allows for selection of interim power at ___% mast torque and ___% Nr.
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