NATOPs Open Book Exam Questions with Detailed Verified
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The MV-22 is a multi-mission aircraft with many applications. These
applications include the following:
Ans: 1. Medium Lift Assault Support
2. Tactical Recovery of Aircraft and Personnel (TRAP)
3. Emergency Evaluation
4. Fleet Logistic Support
5. Logistics Support Ashore
6. Long Range Logistics Support
7. 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.
Ans: 52,600
57,000
60,500
The _______ _______ _______ is primary interface between the flight crew,
the aircraft systems, and avionics.
Ans: Cockpit Management System
When power is applied, _______ MC is designated as _______. Th other MC
then operate as the _______ . The _______ recieves all commands and data,
performs the required routines, and monitors the _______ computer.
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Ans: One
Master
Shadow
Shadow
Master
Each _______ controls operation of _______ MFDs, with the capability of
controlling _______ _______ MFDs in the event of a _______ failure.
Ans: DEU
Two
All Four
DEU
The APN-194 radar altimeter provides aircraft altitude above ground level
(AGL) from _______ to approximately _______ ft.
Ans: 0 - 4,500
The _______ _______ _______ provides pitot-static pressure data to the
FCCs.
Ans: Air Data System
Stall warnings are provided for nacelle angles between _______° and
_______ °
Ans: 0-35°
The _______ _______ warning is initiated when the vertical velocity exceeds
the vertical velocity limit with airspeed _______ kts and less and nacelle angle
greater than _______°.
Ans: Sink Rate
60 kts
65°
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_______ remain displayed until the condition which caused the _______ no
longer exists.
Ans: Warnings
Warning
_______ and _______ are only displayed on the MFDs when the MFDs are in
the CDU backup mode.
Ans: Cautions
Advisories
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 _______ _______ .
Ans: Shut down
Warm start
The aircraft start-up control layer, on the MFDs, provides three options:
Ans: 1. Maintainer Configuration
2. Shipboard minimum power configuration
3. Normal flight operations configuration
_______ _______ _______ are presented in the upper center of the
CDU/EICAS in _______ characters
Ans: Aircraft state indicators
Green
The Standby Flight Display (SFD) located above the CDU on instrument panel,
provides for the independent backup of _______ , _______ , and _______
_______ parameters exclusive of the _______.
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