Term
| Fouling of spark plugs is more apt to occur if the aircraft |
|
Definition
| gains altitude with no mixture adjustment. |
|
|
Term
| Blade angle of a propeller is defined as the angle between the |
|
Definition
| chord line and plane of rotation. |
|
|
Term
| Why should special precautions be taken when filling propane bottles? |
|
Definition
| Propane is very cold and may cause freeze burns |
|
|
Term
| The best power mixture is that fuel/air ratio at which |
|
Definition
| the most power can be obtained for any given throttle setting. |
|
|
Term
| The fuel vents on many powered parachutes and weight shift control aircraft are located |
|
Definition
|
|
Term
| The first indication of carburetor icing in an aircraft equipped with a constant-speed propeller would most likely be a |
|
Definition
| decrease in manifold pressure. |
|
|
Term
| Which statement is true about the effect of temperature changes on the indications of a sensitive altimeter? |
|
Definition
| Colder-than-standard temperatures will place the aircraft lower than the altimeter indicates. |
|
|
Term
| On a multiengine airplane, where the propellers rotate in the same direction, why is the loss of power on one engine more critical than the loss of power on the other engine? |
|
Definition
| The asymmetric propeller thrust or P-factor results in the center of thrust from one engine being farther from the airplane centerline than the center of thrust from the other engine. |
|
|
Term
| Many 4-cycle engines utilize what type of lubrication system? |
|
Definition
|
|
Term
| If a pilot suspects that the engine (with a fixed-pitch propeller) is detonating during climb-out after takeoff, the initial corrective action to take would be to |
|
Definition
| lower the nose slightly to increase airspeed. |
|
|
Term
| Prior to starting the engine, the manifold pressure gauge usually indicates approximately 29" Hg. This is because the |
|
Definition
| pressure within the manifold is the same as atmospheric pressure. |
|
|
Term
| What energy source is used to drive the turbine of a turbocharged airplane? |
|
Definition
|
|
Term
| Propane is preferred over butane for fuel in hot air balloons because |
|
Definition
| it develops higher pressure. |
|
|
Term
| Low-frequency vibrations are normally associated with the |
|
Definition
|
|
Term
| Unless adjusted, the fuel/air mixture becomes richer with an increase in altitude because the amount of fuel |
|
Definition
| remains constant while the density of air decreases. |
|
|
Term
| During preflight, the fuel vent system should always be checked |
|
Definition
| to ensure the vent is open. |
|
|
Term
| When refueling aircraft, which precaution would be adequate for eliminating the potential hazard of static electricity? |
|
Definition
| Connect a ground wire between the aircraft, fuel truck, fuel nozzle, and ground. |
|
|
Term
| Fuel enters a two-cycle engine through an |
|
Definition
| intake port and intake valve. |
|
|
Term
| Why type of oxygen should be used to replenish an aircraft oxygen system? |
|
Definition
|
|
Term
| Which airspeed is identified by color coding on an airspeed indicator? |
|
Definition
| Maximum structural cruising speed. |
|
|
Term
| What airspeed indicator marking identifies the maximum structural cruising speed of an aircraft? |
|
Definition
| Upper limit of the green arc. |
|
|
Term
| Which instrument would be affected by excessively low pressure in the airplane's vacuum system? |
|
Definition
|
|
Term
| 2-cycle engine thrust and fuel efficiency can be greatly compromised when |
|
Definition
| exhaust systems are installed that are not specifically tuned for an engine. |
|
|
Term
| The reason for variations in geometric pitch (twisting) along a propeller blade is that it |
|
Definition
| permits a relatively constant angle of attack along its length when in cruising flight. |
|
|
Term
| If the ground wire between the magneto and the ignition switch becomes disconnected, the most noticeable result will be that the engine |
|
Definition
| cannot be shut down by turning the switch to the OFF position. |
|
|
Term
| If both the ram-air input and drain hole of the pitot system are blocked, what airspeed indication can be expected? |
|
Definition
| No variation of indicated airspeed in level flight even if large power changes are made. |
|
|
Term
| Ground resonance is most likely to occur when |
|
Definition
| a series of shocks cause the rotor system to become out of balance. |
|
|
Term
| During which stroke of a reciprocating engine is the gaseous mixture expanding within the cylinder? |
|
Definition
|
|
Term
| Fuel injection systems, compared to carburetor systems, are generally considered to be |
|
Definition
| just as susceptible to impact icing. |
|
|
Term
| Detonation occurs in a reciprocating aircraft engine when |
|
Definition
| the unburned charge in the cylinders explodes instead of burning normally. |
|
|
Term
| Which statement is true concerning rotor systems? |
|
Definition
| The main rotor blades of a semirigid rotor system can flap and feather as a unit. |
|
|
Term
| Detonation occurs in a reciprocating aircraft engine when |
|
Definition
| the unburned fuel/air charge in the cylinders is subjected to instantaneous combustion. |
|
|
Term
| What effect, if any, does ambient temperature have on propane tank pressure? |
|
Definition
|
|
Term
| With regard to gyroscopic precession, when a force is applied at a point on the rim of a spinning disc, the resultant force acts in which direction and at what point? |
|
Definition
| In the same direction as the applied force, 90° ahead in the plane of rotation. |
|
|
Term
| The purpose of the preheating coil used in hot air balloons is to |
|
Definition
| vaporize the fuel for more efficient burner operation |
|
|
Term
| During power-off stalls with flaps full down, the stall occurs and the pointer on the airspeed indicator shows a speed less than the minimum limit of the white are on the indicator. This is most probably due to |
|
Definition
| installation error in the pitot-static system. |
|
|
Term
| At high altitudes, an excessively rich mixture will cause the |
|
Definition
|
|
Term
| A propeller rotating clockwise, as seen from the rear, creates a sprialing slipstream that tends to rotate the aircraft to the |
|
Definition
| right around the vertical axis, and to the right around the longitudinal axis. |
|
|
Term
| Why should methanol be added to propane fuel? |
|
Definition
| Helps prevent moisture from forming in the fuel system. |
|
|
Term
| In the Northern Hemisphere, if an aircraft is accelerated or decelerated, the magnetic compass will normally indicate |
|
Definition
| correctly when on a north or south heading while either accelerating or decelerating. |
|
|
Term
| Excessively high engine temperatures will |
|
Definition
| cause loss of power, excessive oil consumption, and possible permanent internal engine damage. |
|
|
Term
| The best way to determine burner BTU availability is the |
|
Definition
|
|
Term
| One advantage of fuel injection systems over carburetor systems is |
|
Definition
| better fuel distribution to the cylinders. |
|
|
Term
| The low temperature that causes carburetor ice in an engine equipped with a float-type carburetor is normally the result of the |
|
Definition
| vaporization of fuel and expansion of air in the carburetor. |
|
|
Term
|
Definition
| The vertical distance of the aircraft above sea level. |
|
|
Term
| Concerning the advantages of an aircraft generator or alternator, select the true statement. |
|
Definition
| An alternator provides more electrical power at lower engine RPM than a generator. |
|
|
Term
| What should be the indication on the magnetic 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
| As a result of gyroscopic precession, it can be said that any |
|
Definition
| yawing around the vertical axis results in a pitching moment. |
|
|
Term
| What does the lower limit of the white arc on an airspeed indicator represent? |
|
Definition
| Power-off stall speed in a landing configuration. |
|
|
Term
| The formation of ice in a carburetor's throat is indicated by |
|
Definition
| a drop in RPM, followed by rough engine operation. |
|
|
Term
| What should be the first action after starting an aircraft engine? |
|
Definition
| Adjust for proper RPM and check for desired indications on the engine gauges. |
|
|
Term
| During preflight in cold weather, crankcase breather lines should receive special attention because they are susceptible to being clogged by |
|
Definition
| ice from crankcase vapors that have condensed and subsequently frozen. |
|
|
Term
| The purpose of a kill switch is to |
|
Definition
| ground the lead wire to the ignition coil shutting down the powerplant. |
|
|
Term
| The pilot controls the air/fuel ratio with the |
|
Definition
|
|
Term
| For internal cooling, air cooled aircraft engines are especially dependent on |
|
Definition
| the circulation of lubricating oil. |
|
|
Term
| A typical two-cycle engine ignition coil is powered by |
|
Definition
|
|
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 the primary advantage of a constant-speed propeller? |
|
Definition
| To obtain a pitch setting that is suitable for each flight situation and power setting. |
|
|
Term
| As flight altitude increases, what will occur if no leaning is made with the mixture control? |
|
Definition
| The density of air entering the carburetor decreases and the amount of fuel remains constant. |
|
|
Term
| Leaving the carburetor heat on during takeoff |
|
Definition
| will increase the ground roll. |
|
|
Term
| Generally speaking, the use of carburetor heat tends to |
|
Definition
| decrease engine performance. |
|
|
Term
| What type of oxygen system is most commonly found in general aviation aircraft? |
|
Definition
|
|
Term
| When the pilot leans the mixture control, what is being accomplished? |
|
Definition
| The amount of fuel entering the combustion chamber is being reduced. |
|
|
Term
| Which statement is true regarding fouling of the spark plugs of an aircraft engine? |
|
Definition
| Spark plug fouling results from operating with an excessively rich mixture. |
|
|
Term
| Pitot-static system errors are generally the greatest in which range of airspeed? |
|
Definition
|
|
Term
| In addition to an added safety factor, dual ignition systems also provide |
|
Definition
|
|
Term
| Which condition is most favorable to the development of carburetor icing? |
|
Definition
| Temperature between 20 and 70°F and high humidity. |
|
|
Term
| The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as |
|
Definition
|
|
Term
| The distance a propeller actually advances in one revolution is |
|
Definition
|
|
Term
| Running a fuel tank dry before switching tanks is not a good practice because |
|
Definition
| the engine-driven fuel pump or electric fuel boost pump draw air into the fuel system and cause vapor lock. |
|
|
Term
| Under what condition is indicated altitude the same as true altitude? |
|
Definition
| When at sea level under standard conditions. |
|
|
Term
| The first indication of carburetor ice in an aircraft with a four-cycle engine and fixed-pitch propeller is |
|
Definition
|
|
Term
| In the Northern Hemisphere, which would be correction about starting the rollout form a turn using a magnetic compass? Start the rollout |
|
Definition
| after the compass indication passes south by a number of degrees approximately equal to the latitude minus the normal rollout lead. |
|
|
Term
| What is the primary purpose of the clutch? |
|
Definition
| It allows the engine to be started without driving the main rotor system. |
|
|
Term
| In most helicopters, what is one cause of in-flight medium frequency vibrations? |
|
Definition
| Improper rigging of tail rotor. |
|
|
Term
| If the static pressure tubes are broken inside a pressurized cabin during a high-altitude flight, the altimeter would probably indicate |
|
Definition
| lower than actual flight altitude. |
|
|
Term
| During climbing flight using a turbocharged airplane, the manifold pressure will remain approximately constant until the |
|
Definition
| engine's critical altitude is reached. |
|
|
Term
| Pilots should refrain from revving an engine wiht a reduction drive because |
|
Definition
| the torque exerted on the gears during excessive acceleration and deceleration can cause the gear box to self-destruct. |
|
|
Term
| Proper mixture control and better economy in the operation of a fuel injected engine can be achieved best by use of |
|
Definition
| an exhaust gas temperature indicator. |
|
|
Term
| The purpose of the fuel tank vent system is to |
|
Definition
| allow air to enter the tank as fuel is consumed. |
|
|
Term
| Which statement is true regarding propeller efficiency? Propeller efficiency is the |
|
Definition
| ratio of thrust horsepower to brake horsepower. |
|
|
Term
| In order to improve engine efficiency, two-cycle engine exhaust systems are tuned to |
|
Definition
| stop the fuel mixture from existing the cylinder before combustion. |
|
|
Term
| If the engine oil temperature and cylinder head temperature gauges have exceeded their normal operating range, you may have been |
|
Definition
| operating with too much power and with the mixture set too lean. |
|
|
Term
| Concerning carburetor icing, which statement is true? |
|
Definition
| Carburetor icing would most likely form when the air temperature is between -7°C and 21°C and visible moisture or high humidity is present. |
|
|
Term
| What is the purpose of the rebreather bag on an oxygen mask in a continuous-flow system? |
|
Definition
| Helps to conserve oxygen. |
|
|
Term
| What is the primary purpose of the freewheeling unit? |
|
Definition
| It provides disengagement of the engine from the rotor system for autorotation purposes. |
|
|
Term
| A high-frequency vibration in flight would most likely indicate potential trouble with |
|
Definition
| a piston engine malfunction. |
|
|
Term
| Detonation in an aircraft engine is most likely to occur whenever the |
|
Definition
| engine is operated under conditions which cause the fuel mixture to burn instantaneously. |
|
|
Term
| Propane is used in a balloon fuel system because it |
|
Definition
| provides natural pressure for fuel movement. |
|
|
Term
| An abnormally high engine oil temperature indication may be caused by |
|
Definition
| the oil level being too low. |
|
|
Term
| Why should propane lines be bled after each use |
|
Definition
| Heat may expand the propane and fracture the lines. |
|
|
Term
| Deviation error of the magnetic compass is caused by |
|
Definition
| certain metals and electrical systems within the aircraft. |
|
|
Term
| The operating principle of float-type carburetors is based on the |
|
Definition
| increase in air velocity in the throat of a venturi causing a decrease in air pressure. |
|
|
Term
| Which statement is true regarding preheating of an aircraft during cold weather operations? |
|
Definition
| The cockpit, as well as the engine, should be preheated. |
|
|
Term
| What is absolute altitude? |
|
Definition
| The vertical distance of the aircraft above the surface. |
|
|
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
| Prior to balloon flight on a cold, winter day, it may be necessary to preheat propane tanks because |
|
Definition
| the temperature of liquid propane controls burner pressure during combustion. |
|
|
Term
| The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as |
|
Definition
|
|
Term
| The main rotor blades of a fully articulated rotor system can |
|
Definition
| flap, drag, and feather independently. |
|
|
Term
| Adding more oil to the fuel than specified by the manufacturer of a 2-cycle engine will result in |
|
Definition
| increased carbon buildup and engine fouling. |
|
|
Term
| If a pitot tube is clogged, which instrument would be affected? |
|
Definition
|
|
Term
| Fuel/air ratio is the ratio between the |
|
Definition
| weight of fuel and weight of air entering the cylinder. |
|
|
Term
| Combusted fuel is expelled from a 2-cycle engine through an |
|
Definition
|
|
Term
| While in flight, ice begins forming on the outside of the fuel tank in use. The could indicate |
|
Definition
|
|
Term
| The pitot system provides impact pressure for which instrument? |
|
Definition
|
|
Term
| On a multiengine airplane with engines which rotate clockwise, the critical engine is the |
|
Definition
| left engine, because the right engine center of thrust is farther away from the centerline of the fuselage. |
|
|
Term
| The valve located on each tank that indicates the tank is filled to 80 percent capacity is the |
|
Definition
|
|
Term
| The amount of water absorbed in aviation fuels will |
|
Definition
| increase as the temperature of the fuel decreases. |
|
|
Term
| Detonation occurs at high power settings when the |
|
Definition
| fuel mixture explodes instead of burning progressively and evenly. |
|
|
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
| To absorb maximum engine power and to develop maximum thrust, a constant-speed propeller should be adjusted to a blade angle which will produce a |
|
Definition
| small angle of attack and high RPM |
|
|
Term
| An electrical system failure (battery and alternator) occurs during flight. In this situation, you would |
|
Definition
| experience avionics equipment failure. |
|
|
Term
| What is an important airspeed limitation not color coded on aispeed indicators? |
|
Definition
|
|
Term
| A possible result of using the emergency alternate source of static pressure inside the cabin of an unpressurized airplane is the |
|
Definition
| altimeter may indicate an altitude higher than the actual altitude being flown. |
|
|
Term
| The critical engine on most light multiengine airplanes with clockwise rotating propellers is the |
|
Definition
| left engine, because of the P-factor of the right propeller. |
|
|
Term
| How does temperature and weight affect the V(NE) of a helicopter? |
|
Definition
| V(NE) decreases as temperature and weigh increase. |
|
|
Term
| Air cooled engines dissipate heat |
|
Definition
| through cooling fins on the cylinder and head. |
|
|
Term
| Propeller slip is the difference between the |
|
Definition
| geometric pitch and the effective pitch of the propeller. |
|
|
Term
| Why is nylon line best for tethering a balloon? |
|
Definition
| It stretches under tension, but recovers to normal size when tension is removed, giving it excellent shock-absorbing qualities. |
|
|
Term
| When operating an aircraft with a constant-speed propeller, which procedure places the least stress on cylinder components? |
|
Definition
| When power settings are being decreased, reduce manifold pressure before RPM. |
|
|
Term
| A standby source of fuel to an engine in a powered parachute is typically |
|
Definition
| from an electrically powered pump. |
|
|
Term
| Coolant in a liquid cooled engine is normally circulated by |
|
Definition
|
|
Term
| What is the weight of propane? |
|
Definition
|
|
Term
| What precautions should be taken with respect to aircraft oxygen systems? |
|
Definition
| Ensure that industrial oxygen has not been used to replenish the system. |
|
|
Term
| How should a balloon fuel system be checked for leaks prior to flight? |
|
Definition
|
|
Term
| If the grade of fuel used in an aircraft engine is lower than that specified, it may cause |
|
Definition
|
|
Term
| The main purpose of the mixture control is to |
|
Definition
| adjust the fuel flow to obtain the proper air/fuel ratio. |
|
|
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
| The advantage of total energy compensators is that this system |
|
Definition
| reduces climb and dive errors on variometer indications caused by airspeed changes. |
|
|
Term
| To properly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, it is necessary to drain fuel from the |
|
Definition
| fuel strainer drain and the fuel tank sumps. |
|
|
Term
| What does the lower limit of the green arc on an airspeed indicator represent? |
|
Definition
| Power-off stall speed in a specified configuration. |
|
|
Term
| Which statement is true about magnetic deviation of a compass? |
|
Definition
| Deviation varies for different headings of the same aircraft. |
|
|
Term
| Detonation can be caused by |
|
Definition
| using a lower grade of fuel than recommended. |
|
|
Term
| The basic purpose of adjusting the fuel/air mixture control at altitude is to |
|
Definition
| decrease the fuel flow to compensate for decreased air density. |
|
|
Term
|
Definition
| when the outside air temperature is as high as 100 degrees F and the humidity is as low as 50%. |
|
|
Term
| What is the main reason fuel tank vents must be open? To allow |
|
Definition
| proper air pressure within the tanks for maintaining a steady fuel flow. |
|
|
Term
| If the ground wire between the magneto and the ignition switch becomes disconnected, the engine |
|
Definition
| could accidentally start if the propeller is moved with fuel in the cylinder. |
|
|
Term
| The first indication of carburetor ice in an aircraft with a fixed-pitch propeller is |
|
Definition
|
|
Term
| The rotor blade pitch angle is the acute angle between the blade chord line and the |
|
Definition
|
|
Term
| Which is true concerning total energy compensators? |
|
Definition
| The instrument responds only to up and down air currents. |
|
|
Term
| A high-frequency vibration that suddenly occurs during flight could be an indication of a defective |
|
Definition
|
|