Summary Checklist Flashcards
1A Summary Checklist
The Federal Aviation Administration (FAA) is the agency which governs commercial and general aviation
1A Summary Checklist
The Federal Aviation Regulations (FARs) provide rules which apply to all areas of aviation, including flight operations, the construction of aircraft, and the training requirements which must be met to obtain pilot certificates and ratings
1A Summary Checklist
Many Pilot training schools are located at airport facilities called fixed base operators (FBOs). These facilities provide a variety of services to pilots, including aircraft rental, fueling, maintenance, parking, and the sale of pilot supplies.
1A Summary Checklist
There are two types of pilot training schools; FAA-approved schools governed by FAR Part 141 and schools governed by FAR Part 61
1A Summary Checklist
A syllabus provides structure to pilot training by organizing flight and ground lessons
1A Summary Checklist
To be eligible for a student pilot certificate you must be at least 16 years of age, be able to read, speak, and understand the English language, and hold at least a third-class medical certificate
1A Summary Checklist
There are three classes of medical certificates: first-class which is designed for the airline transport pilot, second-class which is required for the commercial pilot, and third-class for student, recreational, and private pilots
1A Summary Checklist
In addition to the student pilot requirements, to be eligible for a private pilot certificate you must be at least 17 years of age, complete specific training and flight time requirements described in the FARs, pass a knowledge test, and successfully complete a practical test which consists of oral quizzing, performing pilot operations, and executing maneuvers in the airplane
1A Summary Checklist
A private pilot training program can generally be divided into three phases; pre solo, cross-country, and practical test preparation. Each phase includes both flight and ground training.
1A Summary Checklist
The pilot in command of an aircraft is directly responsible for, and is the final authority as to , the operation of that aircraft
1A Summary Checklist
For pilot certification, aircraft are organized into category, class, and type. Your private pilot certificate will state the category, class, and type (if appropriate) of aircraft which you are authorized to fly
1A Summary Checklist
For aircraft certification, category related to the intended use of an aircraft and sets strict limits on its operation
1A Summary Checklist
To act as pilot in command of an aircraft, you must satisfactorily complete a flight review every twenty-four calendar months
1A Summary Checklist
to act as pilot in command of an aircraft carrying passengers, you must have performed at least three takeoffs and landings in an aircraft of the same category and class within the preceding 90 days
1A Summary Checklist
You may not fly an aircraft unless it has received an annual inspection within the previous 12 calendar months, plus a 100-hour inspection within the previous 100 hours if the aircraft is used for rental and flight instruction
1B Summary Checklist
Frequent refresher training is essential to keep your flying skills sharp and to keep you informed on current pilot information.
1B Summary Checklist
Mountain flying requires proper training because special considerations have to be made for weather, airport operations, course selection, and aircraft performance
1B Summary Checklist
Aerobatics instruction increases your proficiency as a pilot. While there are no specific flight hour training requirements to operate an aircraft in aerobatic flight, the FARs do place certain restrictions on aerobatic maneuvers
1B Summary Checklist
Aviation organizations such as AOPA, the EAA, The Ninety-Nines Inc., and the CAP sponsor flying activities, promote safety, and furnish pilot information
1B Summary Checklist
The FARs require that you receive trying and a logbook endorsement stating competency before you can operate as pilot in command of either a high performance airplane or tailwheel airplane
1B Summary Checklist
To obtain an instrument rating, you are required to have a least 40 hours of instrument flight time as well as pass a knowledge test and practical test
1B Summary Checklist
There are no specific ground or flight instruction hours required for the addition of a multi-engine rating to your certificate, but you will have to pass a practical test
1B Summary Checklist
To obtain a seaplane rating, your pilot training will focus on the characteristics of water and its effect on the seaplane
1B Summary Checklist
To pilot aircraft such as helicopters, gliders, or hot air balloons, you will need to obtain an appropriate category and class rating
1B Summary Checklist
To apply for a commercial pilot certificate, you must accumulate a total of 190 to 250 hours of flight time (depending on the type of pilot school that you attend) which typically include a minimum of 100 hours of pilot-in-command time and 50 hours of cross-country time
1B Summary Checklist
There is no specific number of flight hours required for CFI training, but you must pass two knowledge exams and a practical test
1B Summary Checklist
To obtain an ATP certificate, you must have a total of 1,500 hours of flight time including 250 hours of pilot-in-command time, 500 hours cross-country time, 100 hours of night flight, and 75 hours of instrument experience
1B Summary Checklist
If you are seeking a position with a regional airline, you should accumulate as much total flight time, pilot-in-command time, and multi-engine time as possible
1B Summary Checklist
To obtain a position as an airline pilot, you must meet specific minimum requirements, and competitive qualifications which vary as the job market shifts
1B Summary Checklist
Typically, the minimum pilot qualifications to fly as a corporate pilot include a commercial pilot certificate with an instrument rating and a multi-engine rating
1B Summary Checklist
To become employed as an aerial applicator you must hold a commercial pilot certificate and receive additional training in agricultural aircraft operations
1B Summary Checklist
The Army, Navy, Air Force, and Marines provide extensive and demanding pilot training in some of the most technologically advanced aircraft in the world
1C Summary Checklist
When the decision-making process is applied to flight operations it is termed aeronautical decision making (ADM)
1C Summary Checklist
Your general health, level of stress or footage, attitude, knowledge, skill level, and recency of experience are several factors which affect your performance as pilot in command
1C Summary Checklist
Communication is the exchange of ideas, information, or instruction
1C Summary Checklist
Since useful tools and sources of information may not always be readily apparent, learning to recognize and utilize the resources available to you is an essential part of human factors training
1C Summary Checklist
Effective workload management ensures that essential operations are accomplished by planning, prioritizing, and sequencing tasks to avoid work overload
1C Summary Checklist
Situational awareness is the accurate perception of the operational and environmental factors which affect the aircraft, pilot and passengers during a specific period of time
1C Summary Checklist
Ear pain is normally the result of a difference between air pressure in the middle ear and outside air pressure
1C Summary Checklist
Slow descent rates can help prevent or reduce the severity of ear problems and to equalize pressure, the eustachian tube can sometimes be opened by yawning, swallowing, chewing, or employing the Valsalva maneuver
1C Summary Checklist
The reduction of atmospheric pressure during flight can cause scuba divers to experience decompression sickness. Recommended waiting periods are specified before ascending to 8,000 feet MSL or above after diving
1C Summary Checklist
Motion sickness is caused by the brain receiving conflicting messages about the state of the body
1C Summary Checklist
Stress can be defined as the body’s response to physical and psychological demands placed upon it
1C Summary Checklist
Some of the effects of fatigue include degradation of attention and concentration, impaired coordination, and decreased ability to communicate
1C Summary Checklist
Cockpit noise can contribute to excessive fatigue, stress, and airsickness, as well as severely impede the understanding of speech
1C Summary Checklist
Pilots who fly frequently may experience serious hearing loss over a period of time unless ear protection is used
1C Summary Checklist
Depressants are drugs which reduce the body’s functioning in many areas. The most common depressant is alcohol
1C Summary Checklist
Intoxication is determined by the amount of alcohol in the bloodstream which is usually measured as a percentage by weight in the blood. The FARs require that your blood alcohol level be less than .04 percent and that 8 hours pass between drinking alcohol and piloting an aircraft
1C Summary Checklist
Stimulants are drugs which excite the central nervous system and produce an increase in alertness and activity. Amphetamines, caffeine, and nicotine are all forms of stimulants
1C Summary Checklist
Your ability to assess your mental and physical fitness for flight, and your skill at making effective decisions are essential to flight safety
2A Summary Checklist
The fuselage houses the cabin, or cockpit, and serves as the attachment point for the other major airplane components
2A Summary Checklist
Wings may be attached at the top, middle, or lower portion of the fuselage and are contoured to take maximum advantage of the lifting force created by the passing airflow
2A Summary Checklist
The empennage typically consists of the vertical stabilizer, rudder, horizontal stabilizer, and elevator, which act to steady the airplane and maintain a straight path through the air.
2A Summary Checklist
Trim devices are used to help minimize your workload by aerodynamically helping you move a control surface, or maintain the surface in a desired position
2A Summary Checklist
Landing gear employing a rear-mounted wheel is called conventional landing gear
2A Summary Checklist
When the third wheel is located on the nose, the design is referred to as tricycle gear
2A Summary Checklist
Brake pressure may be applied equally or to varying degrees by pressing on the top of each rudder pedal
2A Summary Checklist
The engine works to turn the propeller, generate electrical energy, create vacuum source for some flight instruments, and, in most single-engine airplanes, provide a source of heat for the pilot and passengers
2A Summary Checklist
The propeller translates the rotating force of the engine into a forward-acting force called thrust that helps to move the airplane through the air
2A Summary Checklist
Most of the pertinent information about particular make and model of airplane, including operating limits, can be found in the pilot’s operating handbook (POH) and FAA approved airplane flight manual (AFM)
2B Summary Checklist
The continuos energy-creating process in typical reciprocating airplane engine is referred to as the four-stroke operating cycle. The steps in this cycle are: the intake of the fuel/air mixture, the compression by the piston, the ignition and expansion of the uses, and the venting of the burned gases
2B Summary Checklist
Engine speed for aircraft equipped with a fixed-pitch propeller is displayed on a tachometer in revolutions per minute (r.p.m.)
2B Summary Checklist
A constant-speed propeller is adjustable from the cockpit. A manifold pressure gauge is used on these types of airplanes to monitor engine output by displaying the pressure inside the engine in inches of mercury (in.Hg.)
2B Summary Checklist
The carburetor mixes incoming air with fuel and delivers it to the combustion chamber
2B Summary Checklist
The operating principle of float-type carburetors is based on the difference in pressure at the venturi throat and the air inlet
2B Summary Checklist
The fuel/air mixture can be adjusted from the cockpit with the mixture control
2B Summary Checklist
Carburetor ice may be caused by fuel vaporization and decreasing air pressure in the venturi, which causes a sharp temperature drop in the carburetor
2B Summary Checklist
Carburetor ice is more likely to occur when temperatures are below 21C (70F) and relative humidity is above 80%. To combat the effects of carburetor ice, engines with float-type carburetors employ a carburetor heat system that is designed to eliminate ice by routing air across a heat source before it enters the carburetor
2B Summary Checklist
One of the most significant advantages of the fuel injection system is the relative freedom from the formation of induction icing
2B Summary Checklist
Sea-level performance can be obtained even at high altitudes using either a supercharging or turbocharging system
2B Summary Checklist
The ignition system is made up of magnetos, spark plugs, interconnecting wires, and the ignition switch
2B Summary Checklist
Detonation occurs when fuel in the cylinders explodes instead of burning smoothly
2B Summary Checklist
Preignition is a result of the fuel/air mixture being ignited in advance of the normal timed ignition
2B Summary Checklist
Fuel-pump and gravity-feed systems are similar, except the gravity system does not include engine-driven or electric boost pumps or fuel gauges
2B Summary Checklist
To help prevent moisture buildup it is a good practice to ensure that an airplane’s tanks are refueled following the last flight of the day
2B Summary Checklist
A wet-sump system uses an oil pump to draw oil from the sump and route it to the engine. Oil system operation can be monitored by referring to the oil pressure and temperature gauges
2B Summary Checklist
Cooling air enters the engine compartment through an inlet behind the propeller hub where it is further directed to the hottest part of the engine by baffles
2B Summary Checklist
Exhaust is normally directed out below the engine compartment through a muffler and tailpipe. Metal shrouds around the muffler capture heat that is used to defrost the windscreen and heat the cabin.
2B Summary Checklist
A fixed-pitch propeller uses a single blade that is selected on the basis of what is best for the primary function of the airplane
2B Summary Checklist
A constant-speed propeller control permits you to select a blade angle that is the most appropriate for the flight operation being conducted. The propeller control regulates engine r.p.m. as shown on the tachometer, while the throttle controls engine power output, as indicated on the manifold pressure gauge
2B Summary Checklist
With a constant-speed propeller, you should avoid low r.p.m. settings with high manifold pressure
2B Summary Checklist
When hand-propping an airplane, always ensure that you have received instruction in the correct procedure, and a qualified pilot is at the controls
2B Summary Checklist
Alternators produce alternating current (AC) first, and then convert it to direct current (DC) for use in the airplane electrical system
2B Summary Checklist
One type of ammeter reflects current flowing to or from the battery while the other type, called a load meter, simply displays the load placed on the alternator
2C Summary Checklist
The airspeed indicator, altimeter, and vertical speed indicator all use static pressure. The airspeed indicator is the only instrument which uses pitot pressure
2C Summary Checklist
At sea level, the standard atmosphere consists of a barometric pressure of 29.92 in. Hg. (1013.2 millibars) and a temperature of 15C (59F)
2C Summary Checklist
In the lower atmosphere (below 36,000 feet), the standard pressure lapse rate for each 1,000 feet of altitude is approximately 1.00 in. Hg., and the standard temperature lapse rate is 2C (3.5F)
2C Summary Checklist
The airspeed indicator is divided into color-coded arcs which define speed ranges for different phases of flight. The upper and lower limits of the arcs correspond to specific airspeed limitations, called V-speeds
2C Summary Checklist
VA or maneuvering speed, is the maximum speed at which you may apply full and abrupt control movement without the possibility of causing structural damage. Since VA changes with aircraft weight, it is not depicted on the airspeed indicator
2C Summary Checklist
Regardless of altitude, the indicated airspeed at which a particular airplane stalls in a specific canfiguration remains the same
2C Summary Checklist
Indicated altitude is the altitude measured, and displayed, by your altimeter. Pressure altitude is the verticle distance above the standard datum plane, while density altitude corrects pressure altitude for nonstandard temperature. True altitude is the actual height af an object above mean sea level. Absolute altitude is the actual height of the airplane above the earth’s surface over which it is flying
2C Summary Checklist
If you fly from an area of high pressure to an area of lower pressure without resetting your altimeter, the altimeter will indicate higher than the true altitude. True altitude will be higher than indicated altitude if you do not reset your altimeter when flying from a low pressure area to an area of high pressure
2C Summary Checklist
A one inch change in teh altimeter setting equals 1,000 feet of indicated altitude change in the same direction
2C Summary Checklist
If atmospheric temperature is higher than standard, true altitude will be higher than your indicated altitude. In colder than standard temperatures, true altitude will be lower than indicated altitude
2C Summary Checklist
Trend information shows an immediate indication of an increase or decrease in the airplane’s rate of climb of descent, while rate information shows you a stabilized rate of change
2C Summary Checklist
Blockage of the pitot tube only affects teh airspeed indicator, but a clogged static system affects all three pitot-static instruments
2C Summary Checklist
Rigidity in space refers to the principle that a wheel spun rapidly tends to remain fixed in teh plane in which it is spinning
2C Summary Checklist
Precession causes slow drifting and minor erroneous indications in teh gyroscopic instruments
2C Summary Checklist
The turn coordinator typically uses electrical power while an engine-driven vacuum pump is used to power the attitude and heading indicators
2C Summary Checklist
The turn coordinator provides an indication of turn direction and quality as well as a backup source of bank information in the event of attitude indicator failure
2C Summary Checklist
The attitude indicator uses an artificial horizon and miniature airplane to depict the position of your airplane in relation to the true horizon
2C Summary Checklist
Due to precession, the heading indicator must be aligned periodically with the magnetic compass. When aligning the heading indicator, be certain you are in straight-and-level, unaccelerated flight with the magnetic compass showing a steady indication.
2C Summary Checklist
The magnetic compass shows a turn to the north if you accelerate an airplane in the northern hemisphere; if you decelerate, it indicates a turn to the south. The error doesn’t occur when you are flying on a north or south heading
2C Summary Checklist
Turning error causes the magnetic compass to lead or lag the actual magnetic heading of the airplane during turns
3A
Summary Checklist
During flight, the four forces acting on the airplane are lift, weight, thrust, and drag
3A
Summary Checklist
The four forces are in equilibrium during unaccelerated flight
3A
Summary Checklist
Lift is the upward force created by the effect of airflow as it passes over and under the wing
3A
Summary Checklist
The airplane wing’s shape is designed to take advantage of both Newton’s laws and Bernoulli’s principle
3A
Summary Checklist
According to Bernoulli’s principle, the increase in speed of air on the top of an airfoil produces a drop in pressure and this lowered pressure is an component of total lift. The decrease in speed of air on the bottom of an airfoil produces an increase in pressure, providing the other main component of total lift
3A
Summary Checklist
The reaction to downwash causes an upward reaction according to Newton’s third law of motion
3A
Summary Checklist
Planform, camber, aspect ratio. and wing area are some of the design factors which affect a wing’s lifting capability
3A
Summary Checklist
A stall is caused by the seperation of airflow from the wing’s upper surface. For a given airplane, a stall always occurs at the critical angle of attack, regardless of airspeed, flight attitude, or weight
3A
Summary Checklist
Total lift depends on the combined effects of airspeed and angle of attack. When speed decreases, you must increase the angle of attack to maintain the same amount of lift
3A
Summary Checklist
Flaps increase lift (and drag) by increasing the wing’s effective camber and changeing the chord line which increases the angle of attack. Flap types include plain, split, slotted, and Fowler
3A
Summary Checklist
Weight is the force of gravity which acts vertically through the center of gravity of the airplane toward the center of the earth
3A
Summary Checklist
Thrust is the forward-acting force which opposes drag and propels the airplane
3A
Summary Checklist
Drag acts in opposition to the direction of flight, opposes the forward-acting force of thrust, and limits the forward speed of the airplane
3A
Summary Checklist
Parasite drag is caused by any aircraft surface which deflects or interferes with the smooth airflow around the airplane. Parasite drag normally is divided into three types: form drag, interference drag, and skin friction drag. If airspeed is doubled, parasite drag increases fourfold
3A
Summary Checklist
Induced drag is generated by airflow circulation around the wing as it creates lift. Induced drag increases with flight at slow airspeeds as the angle of attack increases
3A
Summary Checklist
The phenomenon of ground effect occurs close to the ground where the earth’s surface restricts the downward deflection of the airstream from the wing, decreasing induced drag
3B
Summary Checklist
Most training aircraft are designed to display both positive static and positive dynamic stability
3B
Summary Checklist
All aircraft movement takes place around the longitudinal, lateral, and vertical axes, all of which pass through the center of gravity
3B
Summary Checklist
Longitudinal stability relates to movement about the airplane’s lateral axis. Longitudinal stability is influenced by the relationship between the center of pressure and the center of gravity as well as the effects of power changes and the design of the horizontal stabalizer
3B
Summary Checklist
Stability around the aircraft’s longitudinal axis is reffered to as lateral stability, Wing dihedral, sweepback, keel effect, and weight destribution are design features that affect an airplane’s lateral stability
3B
Summary Checklist
Directional stability, or stability about the vertical axis, of most aircraft is maintained by the vertical tail
3B
Summary Checklist
Dutch roll is most likely to occur on aircraft with weak directional stability and strong lateral stability
3B
Summary Checklist
Aircraft with strong directional stability and weak lateral stability are susceptible to spiral instability
3B
Summary Checklist
A stall will always occur when the critical angle of attack, or CLmax, is exceeded. This can occur at any airspeed and in any configuration or attitude
3B
Summary Checklist
A spin will not develop unless both wings are stalled. A normal, erect spin results in the airplane entering a nose-low autorotative descent with one wing stalled more than the other
3C
Summary Checklist
In climbing flight, one component of weight acts perpendicular to the flight path, and another component of weight acts rearward, in hte same direction as drag
3C
Summary Checklist
Four left-turning tendencies associated with propeller-driven airplanes are torque, gyroscopic precession, asymmetrical thrust, and spiraling slipstream
3C
Summary Checklist
During descending flight, one component of weight acts forward along the flight path, while another component acts perpendicular to the flight path
3C
Summary Checklist
The least drag, best glide angle, and maximum gliding distance can be obtained by maintaining the angle of attack that corresponds to L/Dmax
3C
Summary Checklist
Changes in aircraft weight will not affect glide ratio, but a higher airspeed will have to be maintained in a heavier aircraft in order to cover the same distance over the ground
3C
Summary Checklist
Centripetal force, which is created by the horizontal component of lift, is the center-seeking force that acts on a turning airplane
3C
Summary Checklist
The effects of adverse yaw can be counted by maintaining a coordinated turn using rudder
3C
Summary Checklist
Rate of turn increases and radius of turn decreases as angle of bank is increased in a constant airspeed turn, If angle of bank is held constant and airspeed is increased, turn rate will decrease and turn radius will increase
3C
Summary Checklist
The ratio of the weight that the wings must support to the actual weight of the aircraft is termed load factor
3C
Summary Checklist
Accelerated stalls occur when the critical angle of attack is exceeded at an airspeed higher than the one-G stall speed
3C
Summary Checklist
The V-g diagram defines the airplane’s envelope, which is bounded by the stall region, limit load factor, and VNE
4A
Summary Checklist
The majority of midair collisions occur during daylight hours, in VFR conditions, and within five miles of an airport
4A
Summary Checklist
During daylight hours, the most effective way to scan is through a series of short, regularly-spaced eye movements in 100 sectors.
4A
Summary Checklist
You may not notice objects in your peripheral vision unless there is some relative motion
4A
Summary Checklist
If there is no apperent relative motion between another aircraft and yours, you are probably on a collision course
4A
Summary Checklist
Empty field myopia occurs when you are looking at a featureless sky that is devoid of objects, contrasting colors, or patterns and your eyes tend to focus at only 10 to 30 feet
4A
Summary Checklist
Blind spots make it difficult to see conflicting traffic. In both high-wind and low-wing designs, portions of your view are blocked by the fuselage and wings
4A
Summary Checklist
Operation lights On encourages you to use your landing lights during departures and approaches, both day and night, especially when operating within 10 miles of an airport, or in conditions of reduced visibility
4A
Summary Checklist
Clearing turns allow you to see areas blocked by blind spots and make it easier to maintain visual contact with other aircraft in the practice area
4A
Summary Checklist
An aircraft in distress has the right-of-way over all other aircraft
4A
Summary Checklist
Primarily, there are three situations where right-of-way rules apply; converging with another aircraft, approaching another aircraft head-on, or overtaking another aircraft
4A
Summary Checklist
You must maintain minimum safe altitudes at all times except during takeoffs and landings
4A
Summary Checklist
Mountain flying and flight over open water require specialized training from experienced instructors who are familiar with the area over which the flights will be conducted
4A
Summary Checklist
While taxing in wind, proper use of the aileron and elevator controls will help you maintain control of the airplane
4A
Summary Checklist
To ensure that it is clear as to who has control of the aircraft, the FAA strongly recommends the use of a three-step process when exchanging the flight controls
4B
Summary Checklist
A two-way radio is required for you to operate in the controlled airport environment since all aircraft in the vicinity, as well as those on the ground, are subject to instructions issued from the control tower
4B
Summary Checklist
Control of VFR traffic is not exercised at an uncontrolled airport
4B
Summary Checklist
The number at the end of the runway corresponds to the magnetic direction that you are heading when taking off or landing on that runway
4B
Summary Checklist
A standard rectangular pattern with five named legs is used at most airports to ensure that air traffic flows in an orderly manner
4B
Summary Checklist
The most common wind direction indicator is the wind sock, which is used at both controlled and uncontrolled airports. It provides you with the present wind conditions near the touchdown zone of the runway
4B
Summary Checklist
A tetrahedron is a landing direction indicator which may swing around with the small end pointing into the wind, or may be manually positioned to show landing direction
4B
Summary Checklist
The segmented circle helps to identify the location of the wind direction indicator and employs landing strip indicators in conjunction with traffic pattern indicators to show traffic pattern turn direction for a given runway
4B
Summary Checklist
Adhering to noise abatement procedures reduces the level of noise over neighborhoods that are near airports
4B
Summary Checklist
A visual runway normally is marked only with the runway number and a dashed white centerline. When flying instrument approaches, pilots can use the additional markings on IFR runways, such as threshold markings, touchdown zone markings, and aiming point markings
4B
Summary Checklist
Usually, a runway has a displaced threshold because of an obstruction off the end of the runway which might prohibit a normal descent and landing on the beginning portion of the pavement
4B
Summary Checklist
A blast/stopway area is an area where propeller or jet blast can dissipate without creating a hazard to others
4B
Summary Checklist
Taxiways normally have yellow centerline markings, and hold lines wherever they intersect with a runway
4B
Summary Checklist
There are six basic types of airport signs - mandatory, location, direction, destination, information, and runway distance remaining
4B
Summary Checklist
Airport beacons are used to guide pilots to lighted airports at night and may indicate when weather conditions are below VFR minimums during the day
4B
Summary Checklist
The two-bar visual approach slope indicator (VASI) shows whether or not you are on a glide path that will take you safely to the touchdown zone of the runway
4B
Summary Checklist
A variety of lighting systems, including approach light systems, runway edge lights, runway end identifier lights (REILs), in-runway lighting, and taxiway lighting are used at airports to aid pilots in identifying the airport environment at night and in low visibility conditions
4B
Summary Checklist
Pilot-controlled lighting is the term used to describe systems that you can activate by keying the aircraft’s microphone on a specified radio frequency
4C
Summary Checklist
Aeronautical charts are maps that provide a detailed portrayal of an area’s topography and include aeronautical and navigational information
4C
Summary Checklist
Reference lines based on great and small circles are used to define locations on the earth’s surface
4C
Summary Checklist
You can locate a position on an aeronautical chart by knowing its coordinates of latitude and longitude
4C
Summary Checklist
Each sectional chart covers 60 to 80 of longitude and approximately 40 of latitude and is given the name of a primary city within its coverage
4C
Summary Checklist
Maximum elevation figures (MEFs) are based on the highest known feature within a quadrangle bounded by lines of latitude and longitude
4C
Summary Checklist
You should fly no lower than 2,000 feet AGL over a special conservation area, such as a national park or wildlife refuge
4C
Summary Checklist
World aeornautical charts (WACs) use a scale of 1:1,000,000 and are commonly used by pilots of high performance aircraft
4C
Summary Checklist
Divided into seven categories, the chart legend describes symbology for airports, airport data, radio aids to navigation and communication boxes, airport traffic service and airspace information, obstructions, topographic information, and miscellaneous data
4C
Summary Checklist
Since there is a wide variety of airport types, shapes, and sizes, several types of airport diagrams are shown on sectional charts to help you picture the actual airport being illustrated
4C
Summary Checklist
Tick marks extending from an airport diagram indicate that fuel is available and that the field is attended, at least during normal working hours
4C
Summary Checklist
A star above the airport diagram indicates an airport beacon normally operates from sunset to sunrise
4C
Summary Checklist
Airports with control towers are shown in blue, while all others are identified by a magenta color
4C
Summary Checklist
By referring to the airport data on sectional charts, you can determine what radio frequencies to use for communication at a particular airport. In addition, information such as longest runway length, airport lighting, and field elevation can be determined
4C
Summary Checklist
For cross-country planning and flight, refer to navigation and communication boxes for information concerning navaids and fligth service stations (FSSs) in the area
4C
Summary Checklist
Boxes placed near the appropriate navaid, include the name, frequency, and Morse code identifier of the navaid, FSS frequencies are printed above the boxes