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First Landings Crossword: Gleim Units 1&2

Across
______ altitude is the altitude above the surface.
The last word of ANDS.
Ground effect is most often recognized when the airplane is less than one _____ the wingspans length above the ground.
When turning from a north heading, a magnetic compass will _____.
The most important airspeed limitation that is not color coded is the design _____ speed.
The ____ arc is an airspeed that is safe in smooth air only.
_____ move in the opposite direction from one another to control roll about the longitudinal axis.
A one piece horizontal stabilizer and elevator that pivots from a central hinge point.
_____ are attached to the trailing edge of the wing and are used during approach and landing to increase wing lift.
His principle states in part that the internal pressure of a fluid decreases at points where the speed of the fluid increases.
Asymmetric propeller loading.
The _____ component of lift makes the airplane turn.
On ____ days, the altimeter indicates lower than actual altitude.
The _____ at which a wing stalls remains constant regardless of weight, airplane loading, airspeed, etc.
The direction of airflow relative to the wing when the wing is moving through the air.
The _____ line is an imaginary straight line from the leading edge to the trailing edge of the wing.
The standard _____ plane is 29.92 inHg.
____ changes with heading rather than with geographic location.
When the CG in an airplane is located at or rear of the _____ CG limit, the airplane the airplane becomes less stable at all airspeeds.
On warm days, the ____ indicates lower than actual altitude.
_____ is when the difference in true and magnetic north affects the compass.
The _____ effect is greatest at low airspeeds, high angles of attack, and high power.
Vne is never meant to be ______.
______ altitude is pressure altitude corrected for nonstandard temperatures.
Down
A _____ results whenever the critical angle of attack is exceeded.
______ altitude is not susceptible to variations with atmospheric conditions.
To enter a _____ an airplane must always be stalled first.
The pitot tube provides _____ pressure for the ASI only.
Yaw is rotation about the _____ axis.
_____ on wings disrupts the smooth airflow over the airfoil.
The _____ in the attitude indicator rotates in a horizontal plane and depends upon rigidity in space for its operation.
As _____ increases, the load factor increases.
The _____ static system is a source of pressure for three instruments.
The ball indicates whether the angle of bank is _____ with the rate of turn.
When the ____ vents are clogged, your altimeter, VSI, and ASI will provide inaccurate readings.
Altimeter readings are adjusted for changes in ____ pressure.
The wing will require a lower angle of attack in _____ to produce the same lift coefficient.
A magnetic compass will _____ the turn when turning from a south heading.
_____ systems are used to relieve the pilot of the need to maintain constant pressure on the flight controls.
The ten thousand foot interval on an altimeter is indicated by the _____ needle.
The _____ arc is the full flap operating range.
The rearward acting force acting on an airplane during flight.
Pressure altitude and density altitude are the same at standard _____.
VFR cruising _____ changes based on your heading.
A _____ is similar to the horizontal stabilizer but is located in front of the main wings.
The _____ on an airplane controls yaw but does not cause the airplane to turn.
The lower limit of the _____ arc is the power off stalling speed in a specified configuration.
A magnetic compass will indicate a turn toward the _____ during acceleration when on an east or west heading.