Term
| The acute angle A is the angle of... |
|
Definition
|
|
Term
| The term "angle of attack" is defined as the angle... |
|
Definition
| between the wing chord line and the relative wind. |
|
|
Term
| The angle between the chord line of an airfoil and the relative wind is known as the angle of... |
|
Definition
|
|
Term
| Angle of attack is defined as the angle between the chord line of an airfoil and the... |
|
Definition
| direction of the relative wind. |
|
|
Term
| Which statement relates to Bernoulli's principle? |
|
Definition
| Air traveling faster over the curved upper sufrace of an airfoil causes lower pressure on the top surface. |
|
|
Term
| The four forces acting on an airplane in flight are... |
|
Definition
| lift, weight, thrust, and drag. |
|
|
Term
| What is the purpose of the rudder on an airplane? |
|
Definition
| The purpose of the rudder is to control yaw. |
|
|
Term
| What is the relationship of lift, drag, thrust, and weight when the airplane is in straight-and-level flight? |
|
Definition
| lift equals weight and thrust equals drag. |
|
|
Term
| When are the four forces that act on an airplane in equilibrium? |
|
Definition
| during unaccelerated flight. |
|
|
Term
| An airplane said to be inherently stable will... |
|
Definition
| require less effort to control. |
|
|
Term
| What determines the longitudinal stability of an airplane? |
|
Definition
| The location of the CG with respect to the center of lift. |
|
|
Term
| What causes an airplane (except a T-tail) to pitch nosedown when power is reduced and controls are not adjusted? |
|
Definition
| The downwash on the elevators from the propeller slipstream is reduced and elevator effectiveness is reduced. |
|
|
Term
| An airplane has been loaded in such a maner that the CG is located aft of the aft CG limit. One undesirable flight characteristic a pilot might experience with this airplane would be... |
|
Definition
| difficulty in recovering from a stalled condition. |
|
|
Term
| Loading an airplane to the most aft CG will cause the airplane to be... |
|
Definition
| less stable at all speeds. |
|
|
Term
| Changes in the center of pressure of a wing affect the aircraft's... |
|
Definition
| aerodynamic balance and controllability. |
|
|
Term
| The amount of excess load that can be imposed on the wing of an airplane depends upon the... |
|
Definition
|
|
Term
| Which basic flight maneuver increases the load factor on an airplane as compared to straight-and-level flight? |
|
Definition
|
|
Term
| What force makes an airplane turn? |
|
Definition
| the horizontal component of lift. |
|
|
Term
| During an approach to a stall, an increased load factor will cause the airplane to... |
|
Definition
| stall at a higher airspeed. |
|
|
Term
| Select the four flight fundamentals involved in maneuvering an aircraft. |
|
Definition
| Straight-and-level flight, turns, climbs, and descents. |
|
|
Term
| If an emergency situation requires a downwind landing, pilots should expect a faster... |
|
Definition
| groundspeed at touchdown, a longer ground roll, and the likelihood of overshooting the desired touchdown point. |
|
|
Term
| As altitude increases, the indicated airspeed at which a given airplane stalls in a particular configuration will... |
|
Definition
| remain the same regardless of altitude. (true airspeed does not increase or decrease with increased altitude) |
|
|
Term
| In what flight condition must an aircraft be placed in order to spin? |
|
Definition
|
|
Term
| During a spin to the left, which wing(s) is/are stalled? |
|
Definition
| One wing is less stalled than the other, but both wings are stalled in a spin. |
|
|
Term
| The angle of attack at which an airplane wing stalls will... |
|
Definition
| remain the same regardless of gross weight. |
|
|
Term
| One of the main functions of flaps during approach and landing is to... |
|
Definition
| increase the angle of descent without increasing the airspeed. |
|
|
Term
| What is one purpose of wing flaps? |
|
Definition
| To enable the pilot to make steeper approaches to a landing without increasing the airspeed. |
|
|
Term
| Ground effect is most likely to result in which problem? |
|
Definition
| settling to the surface abruptly during landing. |
|
|
Term
|
Definition
| The result of the interference of the surface of the Earth with the airflow patterns about an airplane. |
|
|
Term
| Floating caused by the phenomenon of ground effect will be most realized during an approach to land when at... |
|
Definition
| less than the length of the wingspan above the surface. |
|
|
Term
| What must a pilot be aware of as a result of ground effect? |
|
Definition
| Induced drag decreases; therefore, any excess speed at the point of flare may cause considerable floating. |
|
|
Term
| Which is a result of the phenomenon of ground effect? |
|
Definition
| The angle of attack generating lift is increased. |
|
|
Term
| The airspeed range to avoid while flying in ground effect is... |
|
Definition
|
|
Term
| When landing behind a large aircraft, which procedure should be followed for vortex avoidance? |
|
Definition
| Stay above its final approach flightpath all the way to touchdown. |
|
|
Term
| How does the wak turbulence vortex circulate around each wingtip? |
|
Definition
| Outward, upward, and around each tip. |
|
|
Term
| When taking off or landing at an airport where heavy aircraft are operating, one should be particularly alert to the hazards of wingtip vortices because this turbulence tends to... |
|
Definition
| sink into the flightpath of aircraft operating below the aircraft generating the turbulence. |
|
|
Term
| Wingtip vortices are created only when an aircraft is... |
|
Definition
|
|
Term
| The greatest vortex strength occurs when the generating aircraft is... |
|
Definition
|
|
Term
| Wingtip vortices created by large aircraft tend to... |
|
Definition
| sink below the aircraft generating turbulence. |
|
|
Term
| The wind condition that requires maximum caution when avoiding wake turbulence on landing is a... |
|
Definition
| light, quartering tailwind. |
|
|
Term
| When landing behind a large aircraft, the pilot should avoid wake turbulence by staying... |
|
Definition
| Above the large aircraft's final approach path and landing beyond the large aircraft's touchdown point. |
|
|
Term
| When departing behind a heavy aircraft, the pilot should avoid wake turbulence by maneuvering the aircraft... |
|
Definition
| above and upwind from the heavy aircraft. |
|
|
Term
| One purpose of the dual ignition system on an aircraft engine is to provide for... |
|
Definition
| improved engine performance. |
|
|
Term
| An electrical system failure (battery and alternator) occurs during flight. In this situation, you would... |
|
Definition
| experience avionics equipment failure. |
|
|
Term
| The operating principle of float-type carburetors is based on the... |
|
Definition
| difference in air pressure at the venturi throat and the air inlet. |
|
|
Term
| The basic purpose of adjusting the fuel/air mixture at altitude is to... |
|
Definition
| decrease the fuel flow in order to compensate for decreased air density. |
|
|
Term
| While cruising at 9,500 feet MSL, the fuel/air mixture is properly adjusted. What will occur if a descent to 4,500 MSL is made without readjusting the mixture? |
|
Definition
| The fuel/air mixture may become excessively lean. |
|
|
Term
| During the run-up at a hight-elevation airport, a pilot notes a slight engine roughness that is not affected by the magneto check but grows worse during the carburetor heat check. Under these circumstances, what would be the most logical initial action? |
|
Definition
| Check the results obtained with a leaner setting of the mixture. |
|
|
Term
| If an aircraft is equipped with a fixed-pitch propeller and a float-type carburetor, the first indication of carburetor ice would most likely be... |
|
Definition
|
|
Term
| The presence of carburetor ice in an aircraft equipped with a fixed pitch propeller can be verified by applying carburetor heat and noting... |
|
Definition
| a decrease in RPM and then a gradual increase in RPM. |
|
|
Term
| Which condition is most favorable to the development of carburetor icing? |
|
Definition
| Temperature between 20 and 70 degrees Fahrenheit and hight humidity. |
|
|
Term
| The possibility of carburetor icing exists even when the ambient air temperature is as... |
|
Definition
| high as 70 degrees Fahrenheit and the relative humidity is high. |
|
|
Term
| Applying carburetor heat will... |
|
Definition
| enrich the fuel/air mixture. |
|
|
Term
| What change occurs in the fuel/air mixture when carburetor heat is applied? |
|
Definition
| The fuel/air mixture becomes more rich. |
|
|
Term
| Generally speaking, the use of carburetor heat tends to... |
|
Definition
| decrease engine performance. |
|
|
Term
| On aircraft equipped with fuel pumps, when is the auxiliary electric driven pump used? |
|
Definition
| In the event engine-driven fuel pump fails. |
|
|
Term
| Which regard to carburetor ice, float-type carburetor systems in comparison to fuel injection systems are generally considered to be... |
|
Definition
| more susceptibel to icing. |
|
|
Term
| If the grade of fuel used in an aircraft engine is lower than specified for the engine, it will most likely cause... |
|
Definition
|
|
Term
| Detonation may occur at high-power settings when... |
|
Definition
| the fuel mixture ignites instantaneously instead of burning progressively and evenly. |
|
|
Term
| Detonation occurs in a reciprocating aircraft engine when... |
|
Definition
| the unburned charge in the cylinders explodes instead of burning normally. |
|
|
Term
| The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as... |
|
Definition
|
|
Term
| What type of fuel can be substituted for an aircraft if the recommended octane is not available? |
|
Definition
| The next higher octane aviation gas. |
|
|
Term
| Filling the fuel tanks after the last flight of the day is considered a good operating procedure because this will... |
|
Definition
| prevent moisture condensation by eliminating airspace in the tanks. |
|
|
Term
| If a pilot suspects that the engine (with a fixed-pitch propeller) is detonating during a climb-out after takeoff, the initial corrective action to take would be to... |
|
Definition
| lower the nose slightly to increase the airspeed. |
|
|
Term
| Excessively high engine temperatures will... |
|
Definition
| cause loss of power, excessive oil consumption, and possible permanent internal engine damage. |
|
|
Term
| Excessively hight engine temperatures, either in the air or on the ground, will... |
|
Definition
| cause loss of power, excessive oil consumption, and possible permanent internal engine damage. |
|
|
Term
| If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, the pilot may have been operating with... |
|
Definition
| too much power and with the mixture set too lean. |
|
|
Term
| Which would most likely cause hte cylinder head temperature and engine oil temperature to exceed their normal operating ranges? |
|
Definition
| Using fuel that has a lower-than-specified fuel rating. |
|
|
Term
| For internal cooling, reciprocating aircraft engines are especially dependent on... |
|
Definition
| the circulation of lubricating oil. |
|
|
Term
| An abnormally high engine oil temperature indication may be caused by... |
|
Definition
| the oil level being too low. |
|
|
Term
| What action can a pilot take to aid in cooling an engine that is overheating during a climb? |
|
Definition
| reduce rate of climb and increase airspeed. |
|
|
Term
| What is one procedure to aid in cooling an engine that is overheating? |
|
Definition
| open the cowl flaps, increase airspeed, enrich the mixture, or reduce the power. |
|
|
Term
| How is engine operation controlled on an engine equipped with a constant-speed propeller? |
|
Definition
| The throttle controls power output as registered on the manifold pressure gauge and the propeller control regulates engine RPM. |
|
|
Term
| What is an advantage of a constant speed propeller? |
|
Definition
| Permits the pilot to select the blad angle for the most efficient performance. |
|
|
Term
| A precaution for the operation of an engine equipped with a constant-speed propeller is to... |
|
Definition
| avoid high manifold pressure settings with low RPM. |
|
|
Term
| In what flight condition is torque effect the greatest in a single-engine airplane? |
|
Definition
| low airspeed, high power, high angle of attack. |
|
|
Term
| The left turning tendency of an airplane caused by P-factor is the result of the |
|
Definition
| propeller blade descending on the right, producing more thrust than the ascending blade on the left. |
|
|
Term
| When does P-factor cause the airplane to yaw to the left? |
|
Definition
| When at high angles of attack. |
|
|
Term
| During the preflight inspection who is responsible for determining the aircraft is safe for flight? |
|
Definition
|
|
Term
| How should an aircraft preflight inspection be accomplished for the first flight of the day? |
|
Definition
| Thorough and systematic means recommended by the manufacturer. |
|
|
Term
| Who is primarily responsible for maintaining an aircraft in airworthy condition? |
|
Definition
|
|
Term
| Which instrument will become inoperative if the pitot tube becomes clogged? |
|
Definition
|
|
Term
| Which instrument(s) will become inop if the static vents become clogged? |
|
Definition
| airspeed indicator, altimeter, vertical speed indicator |
|
|
Term
| If the pitot tube and outside static become clogged, which instruments would be affected. |
|
Definition
| The altimeter, airspeed indicator, and vertical speed indicator |
|
|
Term
| The pitot system provides impact pressure for which instrument? |
|
Definition
|
|
Term
| Which V-speed represents maneuvering speed? |
|
Definition
|
|
Term
| What does the red line on an airspeed indicator represent? |
|
Definition
|
|
Term
| Which color identifies the never-exceed speed? |
|
Definition
|
|
Term
| Which color identifies the power-off stalling speed in a specified configuration |
|
Definition
| The lower limit of the green arc |
|
|
Term
| Which would provide the greatest gain in altitude in the shortest distance during climb after takeoff? |
|
Definition
|
|
Term
| After takeoff, which airspeed would the pilot use to gain the most altitude in a given period of time? |
|
Definition
|
|
Term
| What is the full flap operating range for the airplane? |
|
Definition
|
|
Term
| The maximum speed at which the airplane can be operated in smooth air? |
|
Definition
|
|
Term
| What is the max flaps extended speed? |
|
Definition
|
|
Term
| Which color identifies the normal flap operating range? |
|
Definition
|
|
Term
| Which color identifies the power-off stalling speed with wing flaps and landing gear in the landing configuration? |
|
Definition
| the upper limit of the white ark |
|
|
Term
| What is the maximum structural cruising speed? |
|
Definition
|
|
Term
| What is an important airspeed limitation that is not coded on airspeed indicators |
|
Definition
|
|
Term
| which v-speed represents maximum flap extended speed? |
|
Definition
|
|
Term
| Which v speed represents maximum landing gear extended speed? |
|
Definition
|
|
Term
|
Definition
| max structural cruising speed |
|
|
Term
|
Definition
| minmum stall speed in landing configuration |
|
|
Term
| what is the caution range of the airplane |
|
Definition
|
|
Term
| if an altimeter setting is not available before flight, to which altitude should the pilot adjust the altimeter? |
|
Definition
| the elevation of the departure area |
|
|
Term
| prior to takeoff, the altimeter should be set to which altitude or altimeter setting? |
|
Definition
| the current local altimeter setting, if available, or the departure airport elevation. |
|
|
Term
| At which altitude shall the altimeter be set to 29.92 |
|
Definition
|
|
Term
| altimeter setting is the value to which the barometric pressure scale of the altimeter is set so the altimeter indicates |
|
Definition
| true altitude at field elevation |
|
|
Term
| How do variations in the temperature affect te altimeter? |
|
Definition
| pressure levels are raised on warm days and the indicated altitude is lower than true altitude. |
|
|
Term
|
Definition
| the vertical distance of the aircraft above sea level |
|
|
Term
| under what condition will true altitude be lower than indicated altitude |
|
Definition
| in colder than standard air temperature |
|
|
Term
| what is absolute altitude |
|
Definition
| the vertical distance of the aircraft above the surface |
|
|
Term
|
Definition
| the pressure altitude corrected for nonstandard temperature |
|
|
Term
| what is pressure altitude |
|
Definition
| the altitude indicated when the barometric pressure scale is set to 29.92 |
|
|
Term
| under what condition is indicated altitude the same as true altitude? |
|
Definition
| when at sea level under standard conditions |
|
|
Term
| If it is necessary to set the altimeter from 29.15 to 29.85 what change occurs |
|
Definition
| 700 foot increase in indicated altitude |
|
|
Term
| under which condition will pressure altitude be equal to true altitude? |
|
Definition
| when standard atmospheric conditions exist |
|
|
Term
| under what condition is pressure altitude and density altitude the same value? |
|
Definition
|
|
Term
| if a flight is made from an area of low pressure into an area of high pressure without the altimeter setting being adjusted, the altimeter will indicate |
|
Definition
| lower than actual altitude aove sea level |
|
|
Term
| if a flight is made from an area of hight pressure into an area of lower pressure without the altimeter setting being adjusted, the altimeter will indicate.. |
|
Definition
| higher than actual altitude above sea level |
|
|
Term
| which condition would cause the altimeter to indicate a lower altitude than true altitude? |
|
Definition
| air temp warmer than standard |
|
|
Term
| If a pilot changes the altimeter setting from 30.11 to 29.96 what is the approximate change in indication? |
|
Definition
| altimeter will indicate 150 lower |
|
|
Term
| How should a pilot determine the direction of bank from an attitude indicator such as the one illustrated? |
|
Definition
| by the relationship of the miniature airplane to the deflection horizon bar |
|
|
Term
| the turn coordinator provides an indication of the |
|
Definition
| movement of the aircraft about the yaw and roll axis |
|
|
Term
| the proper adjustment to make on the attitude indicator during level flight is to align the |
|
Definition
| miniature airplane to the horizon bar |
|
|
Term
| to receive accurate indications during flight from a heading indicator, the instrument must be |
|
Definition
| periodically realigned with the magnetic compass as the gyro precesses |
|
|
Term
| deviation in a magnetic compass is caused by the |
|
Definition
| magnetic fields within the aircraft distorting the lines of magnetic force |
|
|
Term
| the angular difference between true north and magnetic north is |
|
Definition
|
|
Term
| In the northern hemisphere, a magnetic compass will normally indicate a turn toward the north if |
|
Definition
| an aircraft is accelerated while on an east or west heading |
|
|
Term
| in the northern hemisphere, the magnetic compass will normally indicate a turn toward the south when... |
|
Definition
| the aircraft is decelerated while on a west heading |
|
|
Term
| What should be the indication on the mag compass as you roll into a standard rate turn to the right from a south heading in the northern hemisphere? |
|
Definition
| the compass will indicate a turn to the right, but at a faster rate than is actually occurring |
|
|
Term
| in the northern hemisphere, if an aircraft is accelerated or decelerate, the mag compass will normally indicate... |
|
Definition
| correctly when on a north or south heading |
|
|
Term
| in the northern hemisphere, a mag compass will normally indicate initially a turn toward the west |
|
Definition
| if a right turn is entered from a north heading |
|
|
Term
| in the northern hemisphere, a mag compass will normally indicate initially a turn toward the east if |
|
Definition
| a left turn is entered from a north heading |
|
|
Term
| during flight, when are the indication of a magnetic compass accurate? |
|
Definition
| only in straight-and-unaccelerated flight |
|
|
Term
| in the northern hemisphere, if a glider is accelerated or decelerated, the mag compass will indicate |
|
Definition
| correctly only when on a north or south heading |
|
|
Term
| what documents must be in your personal possession or readily accessible in the aircraft while operating as pic of an aircraft? |
|
Definition
| an appropriate pilot certificate and an appropriate current medical certificate if required. |
|
|
Term
| When must a current pilot certificate be in the pilot's personal possession or readily accessible in the aircraft? |
|
Definition
| anytime when acting as pic or as a required crew member |
|
|
Term
| a rec or private pilot acting as pic or in any other capacity as a required pilot flight crew member, must have in their personal possession or realiy accessible in the aircraft a current |
|
Definition
| medical certificate if require and an appropriate pilot certifiate. |
|
|
Term
| each person who holds a pilot certificate or a medical certificate shall present if for inspection upon the freques of an administrator, the natonal transporation safety board, or any |
|
Definition
| federal, state, or local law enforcement officer |
|
|
Term
| a rec pilot acting as pic must have in his or her personal possession while aboard the aircrat |
|
Definition
| a curren logbook endorsmem that permits flight within 50nm formt eh deperature airport |
|
|
Term
| to act a pic of an aircraft carrying passengers, a pilot must show by logbook endorsement the satisfacoty ocompeltion of flight review or compleiton of pilot proficiency check within |
|
Definition
|
|
Term
| if recency of experience reqires for night flight are not met and offical sunset is 1830, the altest time passengers may be carried is |
|
Definition
|
|