Book - FAA Questions Flashcards

1
Q

1A FAA Questions

A

A class of aircraft, with respect to the certification of airmen, means a classification of aircraft within a category having similar operating characteristics, such as single engine, multi-engine, land, water,gyroplane, and Helicopter. With respect to the certification of aircraft, class means a broad grouping of aircraft having similar characteristics of propulsion, flight, or landing, such as airplane, rotorcraft, glider, ballon, landplane, and seaplane

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2
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1A FAA Questions

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An aircraft with an experimental certificate may not be operated for compensation or hire or for any purpose other than the purpose for which the certificate was issued

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3
Q

1A FAA Questions

A

If the aircraft logbook shows that the last annual inspection and transponder inspection were completed on November 1, then the next annual inspection is due November 30 of the following year. The transponder inspection is due November 30, two years later

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4
Q

1A FAA Questions

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An aircraft may be flown beyond a 100-hour inspection expiration to a place where the service can be completed. However, the next inspection is due 100 hours from the original expiration time.

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5
Q

1A FAA Questions

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If an aircraft is altered in a way that could appreciably change its flight characteristics, it must be flight tested by a person who is rated in that aircraft and who holds at least a private pilot certificate

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6
Q

1A FAA Questions

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Preventive maintenance must be entered in aircraft maintenance record; including the signature, certificate number, and kind of certificate held by the person approving the work and a description of the work performed

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7
Q

1A FAA Questions

A

You must complete a flight review every 24 calendar months to continue exercising your pilot certificate privileges. To carry passengers, you must complete three takeoffs and landings in the same category and class of aircraft. To carry passengers at night, those takeoffs and landings must be to a full stop and between one hour after sunset and one hour before sunrise

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8
Q

1B FAA Questions

A

A parachute that is carried in an aircraft for emergency use must have been packed by a certificated and appropriately-rated parachute rigger: If constructed of natural materials - within the preceding 60 days If constructed of synthetic materials - within the preceding 180 days

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9
Q

2A FAA Questions

A

Aircraft operating limitations may be found in the approved flight manual, markings, placards, or a combination of these

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10
Q

2A FAA Questions

A

An experimental or light-sport aircraft’s operating limitations are part of Form 8130-7, which is the special airworthiness certificate, This must be carried in the aircraft

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11
Q

2B FAA Questions

A

The operating principle of float-type carburetors is based on the difference in pressure at the venturi throat and the air inlet

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12
Q

2B FAA Questions

A

When you lean the mixture, you decrease the fuel flow to compensate for decreased air density. Leaning the mixture may eliminate engine roughness during sunup at high-elevation airports

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13
Q

2B FAA Questions

A

If you do not adjust the mixture control during descents from high to low altitudes, the fuel/air mixture will be too lean

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14
Q

2B FAA Questions

A

You should expect carburetor ice when temperatures are at or below 210C (700F) and the relative humidity is high

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15
Q

2B FAA Questions

A

The first indication of carburetor ice in an airplane equipped with a fixed-pitch propeller is a loss of r.p.m. The decrease in r.p.m. casued by the enriched mixture will be followed by an increase in r.p.m. as the ice melts

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16
Q

2B FAA Questions

A

The use of carburetor heat generally decreases engine performance

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17
Q

2B FAA Questions

A

Fuel injection systems are generally less susceptible to icing than float-type carburetors

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18
Q

2B FAA Questions

A

The dual ignition system on an airplane engine provides improved engine performance

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19
Q

2B FAA Questions

A

Detonation occurs when fuel in the cylinders explodes instead of burning smoothly

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20
Q

2B FAA Questions

A

Detonation may result if you allow the engine to overheat or if you use an improper grade of fuel. If you suspect the engine is detonating on climbout, you can lower the nose to increase airspeed and the cooling airflow around the engine

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21
Q

2B FAA Questions

A

Preignition is the uncontrolled combustion of fuel in advance of normal ignition

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22
Q

2B FAA Questions

A

On aircraft equiped with electric fuel pumps, the auxillary electric driven pump is used in the event the engine-driven fuel pump fails

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23
Q

2B FAA Questions

A

To porperly purge water from the fuel system of an aircraft equipped with fuel tank sumps and a fuel strainer quick drain, drain fuel from both the fuel strainer drain and teh fuel sumps

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24
Q

2B FAA Questions

A

Filling fuel tanks after the last flight of the day prevents moisture from condensing by eliminating air from the tanks

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25
2B FAA Questions
Using a fuel grade lower than specified can cause cylinder head and engine temperatures to exceed normal operating limits. If the recommended fuel grade is not available, you may substitute the next higher grade, if approvedby the manufacturer
26
2B FAA Questions
Airplane engines depend on circulation of oil for lubrication of internal parts and cooling
27
2B FAA Questions
Immediately after starting the engine, adjust r.p.m. and check engine instruments for the proper indications
28
2B FAA Questions
High engine oil temperature may be caused by an oil level that is too low
29
2B FAA Questions
Excessive engine temperatures can result in loss of power, high oil consumption, and possible engine damage
30
2B FAA Questions
Engine temperature may be reduced by enriching the mixture, reducing the rate of climb, increasing airspeed, or reducing power
31
2B FAA Questions
If oil and cylinder head temperatures are above normal, you may be using too much power with an overly lean mixture
32
2B FAA Questions
With a constant-speed propeller, the throttle controls engine power output, as indicated on the manifold pressure gauge, while the propeller control regulates engine r.p.m.
33
2B FAA Questions
A constant-speed propeller allows you to select the blade angle that provides the most efficient performance
34
2B FAA Questions
With a constat-speed propeller, you should avoid low r.p.m. settings with high manifold pressure to prevent internal engine stress
35
2B FAA Questions
When hand-starting an airplane, a competent pilot must be at the controls
36
2C FAA Questions
The instruments required for day VFR flight in a single-engine airplane are: airspeedindicator, altimeter, magnetic compass, tachometer, oil pressure gauge, oil temperature gauge, manifold pressure gauge (for constant-speed propeller), fuel gauge for each tank, and landing gear position indicator (for retractable landing gear)
37
2B FAA Questions
ISA at sea level equals 29.92 in. Hg., or 1013.2 millibars, and has a temperature of 15C. Temperature decreases approximately 2C for each 1,000-foot increase in altitude
38
2C FAA Questions
The pitot-static system provides impact, or ram, air pressure to the airspeed indicator
39
2C FAA Questions
Airspeed ranges are shown by color-coded arcs on the airspeed indicator. The white arc is the flap operating range, the green arc is for normal operations, the yellow arc is the caution range, and the red line marks the never exceed speed. Important airspeeds are also marked by the boundaries of the color-coded arcs
40
2C FAA Questions
Since Va changes with aircraft weight, it is not marked on the airspeed indicator
41
2C FAA Questions
As altitude increases, the indicated airspeed at whcih a given airplane stalls in a specific configuration remains the same
42
2C FAA Questions
The longest pointer of the altimeter shows hundreds of feet, the middle-sized pointer indicates thousands of feet, and the shortest pointer shows tens of thousands of feet
43
2C FAA Questions
Pressure altitude is the height above the standard datum plane when 29.92 is set in the altimeter scale
44
2C FAA Questions
Density altitude is the pressure altitude corrected for nonstandard temperature. Density altitude increases as ambient temperature increases
45
2C FAA Questions
True altitude is the actual vertical distance above mean sea level, and is equal to pressure altitude and indicated altitude when standard atmospheric conditions exist. True altitude is equal to field elevation when the altimeter is set to the local pressure setting.
46
2C FAA Questions
Absolute altitude is the height, or vertical distance, above the surface
47
2C FAA Questions
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 actual (true) altitude. If you do not reset your altimeter when flying from a low pressure area to an area of high pressure, your altimeter will indicate lower than actual (true) attitude
48
2C FAA Questions
A one inch change in the altimeter setting equals 1,000 feet of indicated altitude change in the same direction
49
2C FAA Questions
When atmospheric temperature is higher than standard, pressure levels are raised, and your true altitude is higher than your indicated altitude. When temperature is colder than standard, pressure levels are lowered, and your true altitude is lower than your indicated altitude
50
2C FAA Questions
Blockage of the pitot tube affects only the airspeed indicator, but a clogged static system affects all three pitot-static instruments, the airspeed inicator, altimeter, and VSI
51
2C FAA Questions
The turn coordinator shows aircraft yaw and roll movement
52
2C FAA Questions
As the airplane banks, the relationship between the minature airplane and the horizon bar depicts the direction of turn
53
2C FAA Questions
The miniature airplane is adjustable and should be set to match the level flight indication of the horizon bar
54
2C FAA Questions
Due to precession, the heading indicator must be aligned periodically with the magnetic compass
55
2C FAA Questions
Deviation is the error caused by the magnetic fields of the airplane and its electronic equipment
56
2C FAA Questions
If you accelerate an airplane in the northern hemisphere, the compass shows a turn to the north; if you decelerate, it indicates a turn to the north; if you decelerate, it indicates a turn to the south. The error is most pronounced when flying on headings of east of west; it doesn't occur when flying directly on a north or south heading
57
2C FAA Questions
In the northern hemisphere, a magnetic compass will initially indicate a turn to the west if a right turn is entered from a heading of north. A left turn under the same circumstances will cause a magnetic compass to initially indicate a turn toward the east
58
2C FAA Questions
Turning error causes the magnetic compass to lead or lag the actual magnetic headings of the airplane during turns
59
2C FAA Questions
The magnetic compass provides accurate indicators only when you are flying in smooth air and in straight-and-level, unaccelerated flight
60
3A FAA Questions
The four forces acting on an airplane in flight are lift, weight, thrust, and drag. These forces are in equilibrium during unaccelerated flight.
61
3A FAA Questions
In straight-and-level, unaccelerated flight, lift equals weight and thrust equals drag.
62
3A FAA Questions
The angle formed by the wing chord line and relative wind is called the angle of attack
63
3A FAA Questions
An airplane always stalls when the critical angle of attack is exceeded regardless of airspeed, flight attitude, or weight
64
3A FAA Questions
Flaps allow you to steepen the angle of descent on an approach without increasing airspeed
65
3A FAA Questions
Ground effect is the result of the earth's surface altering the airflow patterns about the airplane. In ground effect, an airplane may become airborne before it reaches its recommended takeoff speed
66
3A FAA Questions
In ground effect, induced drag decreases and excess speed in the flare may cause floating when the aircraft is within one wingspan above the surface
67
3B FAA Questions
An airplane said to be inherently stable will require less effort to control
68
3B FAA Questions
Yaw movement about the vertical axis is produced by the rudder
69
3B FAA Questions
The longitudinal stability of an airplane is determined primarily by the location of the center of gravity in relation to the center of pressure (lift)
70
3B FAA Questions
An Airplane loaded to its aft CG limit will be less stable at all speeds
71
3B FAA Questions
An airplane becomes progressively more difficult to control as the CG moves aft. If the CG is beyond the aft limit, it will be difficult to lower the nose to recover from a stall or spin
72
3B FAA Questions
A power reduction in airplanes, other than T-tails, will decrease the downwash on the horizontal stabilizer from the wings and propeller slipstream. This is what causes the nose to pitch down after a power reduction
73
3B FAA Questions
To enter a spin, an airplane must first be stalled. Although both wings are in stalled condition during a spin, one wing is stalled more than the other
74
3C FAA Questions
The four flight fundamentals involved in maneuvering an aircraft are: straight-and-level flight, turns, climbs, and descents
75
3C FAA Questions
Torque effect is greatest at low airspeeds, high power settings, and high angles of attack
76
3C FAA Questions
P-factor causes an airplane to yaw to the left when it is at high angles of attack. P-factor results from the descending propeller blade on the right producing more thrust than the ascending blade on the left.
77
3C FAA Questions
If a power failure occurs after takeoff, immediately establish the proper gliding attitude and airspeed
78
3C FAA Questions
The horizontal component of lift causes an airplane to turn
79
3C FAA Questions
The load factor imposed on an airplane will increase as the angle of bank is increased
80
3C FAA Questions
Increasing the load factor will cause an airplane to stall at a higher speed
81
3C FAA Questions
VA is defined as the design maneuvering speed
82
3C FAA Questions
The amount of excess load that can be imposed on an airframe depends on the aircraft's speed
83
4A FAA Questions
The most effective way to scan during daylight is through a series of short, regularly-spaced eye movements in 100 sectors
84
4A FAA Questions
If there is no apparent relative motion between another aircraft and yours, you are probably on a collision course
85
4A FAA Questions
In haze, air traffic and terrain features appear to be farther away than they actually are
86
4A FAA Questions
Prior to starting any maneuvers, make clearing turns and carefully scan the area for other aircraft.
87
4A FAA Questions
An aircraft in distress has the right-of-way over all other aircraft
88
4A FAA Questions
When two aircraft of the same category are converging, but not head-on, the aircraft to the left shall give way. If the aircraft are on a head-on collision course, both aircraft should give way to the right.
89
4A FAA Questions
The least maneuverable aircraft normally has the right-of-way. For example, a glider has the right-of-way over an airship and an airship has the right-of-way over an airplane
90
4A FAA Questions
When two or more aircraft are approaching an airport for the purpose of landing, the right-of-way belongs to the aircraft at the lower altitude
91
4A FAA Questions
The minimum safe altitude anywhere must allow an emergency landing, following an engine failure, without undue hazard to persons of property on the surface
92
4A FAA Questions
Over a congested area, you are required to fly 1,000 feet above any obstacle within a horizontal radius of 2,000 feet of your aircraft
93
4A FAA Questions
When flying over an uncongested area, you must fly at least 500 feet above the surface. Over sparsely populated or open water areas you cannont fly within 500 feet of any person, vessel, vehicle, or structure
94
4A FAA Questions
When taxing in strong winds, proper use of the sileron and elevator controls of your airplane. For example, when taxiing in a quartering headwind, hold the aileron up on the side from which the wind is blowing. In a quatering tailwind, position the aileron down on the side from which the wind is blowing
95
4A FAA Questions
Generally, the most critical wind condition when taxiing a high-wing, tricycle-gear airplane is a quartering tailwind
96
4A FAA Questions
When taxiing a tailwheel airplane, you should position the ailerons the same as you do for a tricycle-gear airplane. However, you should hold the elevator control aft (elevator up) in a headwind, and hold the elevator control forward (elevator down) in a tailwind
97
4B FAA Questions
The runway's magnetic direction is rounded off to the nearest 100, with the last zero omitted. For example, runways oriented approximately 0900 and 2700 magnetic are designated by the numbers 9 and 27
98
4B FAA Questions
At an uncontrolled airport, you can determine landing direction by observing the wind direction indicator. The extensions on the segmented circle indicate whether a lefthand of righthand pattern should be used for a given runway.
99
4B FAA Questions
On runways with a displaced threshold, the beginning portion of the landing zone is marked with a solid white line with white arrows leading up to it. Although the pavement leading up to a displaced threshold may not be used for landing, it may be available for taxiing, the landing rollout, and takeoffs.
100
4B FAA Questions
A blast pad/stopway area cannot be used for taxiing, takeoff, or landing. A yellow demarcation bar delineates a displaced threshold area where taxi is permitted from a blast pad or stopway that precedes the area
101
4B FAA Questions
A closed runway or taxiway is marked by a yellow X
102
4B FAA Questions
ATC should issue a LAHSO clearance only when the visibility is at least three miles and the cealing is at least 1,000 feet
103
4B FAA Questions
An airport's rotating beacon operated during daylight hours normally indicates that weather at the airport is below basic VFR minimums
104
4B FAA Questions
A militrary airport is identified by a rotating beacon which emits two quick, white flashes between green flashes
105
4B FAA Questions
If you are landing at a controlled airport served by a VASI, regulations require that you maintain an altitude at or above the glide slope until a lower altitude is necessary for a safe landing
106
4B FAA Questions
You will see white over white lights on the VASI if you are too high. Red over white indicates that you are on teh glide path, and you are too low if the VASI shows red over red
107
4B FAA Questions
An above glide slope indication from a tri-color VASI is an amber light. If you see a green light, you are on glide path, and a red light indicates that you are too low
108
4B FAA Questions
A below glide path indication from a pulsating approach slope indicator is a pulsating red light
109
4B FAA Questions
A slightly high glide slope indication from a PAPI is three white lights and one red light
110
4B FAA Questions
Blue omnidirectional lights identify the edge of the taxiway at night
111
4B FAA Questions
To operate pilot-controlled lighting, key your mike seven times on the specified frequency to turn all the lights on at maximum intensity. Key the mike fice times for medium-intensity lighting and three times for the lowest intensity
112
4C FAA Questions
You can locate a position on an aeronautical chart by knowing its coordinates of latitude and longitude
113
4C FAA Questions
The terrain height is portrayed on sectional charts by contour lines and spot elevations
114
4C FAA Questions
You should fly no lower than 2,000 feet AGL over a national park or wildlife refuge
115
4C FAA Questions
Tick marks extending from an airport symbol indicate that fuel is available and that the field is attended, at least during normal working hours. A star above the airport symbol indicates an airport beacon normally operates from sunset to sunrise
116
4C FAA Questions
By referring to the airport data on sectional charts, you can determine what radio frequencies to use for communication at that airport. In addition, information such as longest runway length, airport lighting, and field elevation can be determined
117
4C FAA Questions
A VORTAC navigational facility is depicted by a blue triangular symbol on aeronautical charts
118
4C FAA Questions
A circle H located in the top right corner of a communication box indicates that the weather service HIWAS is transmitted over the navaid frequency
119
4C FAA Questions
The height of an obstruction is located next to the symbol and may be indicated by both an MSL and AGL altitude. By referring to terrain and obstruction heights, you can determine a safe cruising altitude
120
4C FAA Questions
At times, a caution box may alert you to a specific hazard depicted on a sectional chart
121
4D FAA Questions
Specific VFR weather minimums apply in Class G airspace below 1,200 feet AGL, between 1,200 feet AGL and 10,000 feet MSL, and above 10,000 feet MSL. The minimums which you must maintain in Class G airspace depend on whether you are operating during the day or at night
122
4D FAA Questions
Class G airspace typically extends from the surface to 700 or 1,200 feet AGL. In some areas, Class G may extend from the surface to 14,500 feet MSL
123
4D FAA Questions
An operable 4,096-code transponder with Mode C capability is required while operating within Class A airspace, Class B airspace, within 30 nautical miles of Class B primary airports, and Class C airspace
124
4D FAA Questions
Class E airspace segments include Federal, or Victor, airways which usually extend to 4 nautical miles on each side of the airway centerline and from 1,200 feet AGL up to 17,999 feet MSL
125
4D FAA Questions
When climbing or descending VFR along an airway, execute gentle banks left and right for continuous scanning of the airspace
126
4D FAA Questions
Class E airspace consists of several different segments. The weather minimums that you must maintain while in each of these segments depend on whether you are operating at an altitude below 10,000 feet MSL, or at or above 10,000 feet MSL
127
4D FAA Questions
Airspace at an airport with a part-time control tower is classified as Class D airspace only when the associated tower is in operation
128
4D FAA Questions
The lateral dimensions of Class D airspace are based on the instrument procedures for which the controlled airspace is established. Class D airspace is depicted on a sectional chart by a blue segmented circle
129
4D FAA Questions
When operating at a nontower satelite airport within Class D airspace, you must establish contact with the primary airport's control tower
130
4D FAA Questions
Unless otherwise authorized, you must establish two-way radio communication with the control tower prior to entering Class D airspace. In addition, while operating within Class D airspace, you must maintain at least 3 statute miles visibility and a distance 500 feet below, 1,000 feet above, and 2,000 feet horizontally from clouds
131
4D FAA Questions
Class C airspace usually has similar dimensions from one airport to another although some areas may be modified to fit unique aspects of a specific airport environment
132
4D FAA Quesions
The normal radius of the outer area of Class C airspace is 20 nautical miles from the primary airport
133
4D FAA Questions
You must establish two-way radio communication with the ATC facility having jurisdiction over the area prior to entering Class C airspace
134
4D FAA Questions
While operating in Class C airspace, you must maintain at least 3 statute miles visibility and remain at least 500 feet below, 1,000 feet above, and 2,000 feet horizontally from clouds
135
4D FAA Questions
If you are operating out of a satelite airport within Class C airspace you should contact ATC as soon as practicable after takeoff
136
4D FAA Questions
To operate within Class B airspace, your aircraft must have two-way radio communication capability and a Mode C transponder
137
4D FAA Questions
To operate in Class B airspace, you must be at least a private pilot or a student pilot with the appropriate logbook endorsement
138
4D FAA Questions
The floor and ceiling of each layer of Class B airspace are denoted on a sectional chart by MSL altitude
139
4D FAA Questions
Class A airspace extends from 18,000 feet MSL up to and including FL600. You must be instrument rated and be on an IFR flight plan to operate in Class A airspace
140
4D FAA Questions
Within Class A airspace, you are required to set your altimeter to the standard settting of 29.92 in. Hg.
141
4D FAA Questions
A special VFR clearance allows you to operate within the surface areas of Class B, C, D, or E airspace if the visibility is at least 1 statute mile and you can remain clear of clouds
142
4D FAA Questions
You may not operate under a special VFR clearance at night unless you are instrument rated and your aircraft is instrument equipped
143
4D FAA Questions
The phrase NO SVFR included with the airport data on a sectional chart indicates that special VFR clearances are not issued to fixed-wing aircraft
144
4D FAA Questions
Scud running is an operational pitfall in which a pilot pushes his or her capabilities and the aircraft's limits by trying to maintain visual contact with the terrain in low visibility and ceiling
145
4D FAA Questions
Responsibiilty for collision avoidance in an alert area rests with all pilots
146
4D FAA Questions
While operating under VFR in an MOA, you should exercise extreme caution when military training activity is being conducted
147
4D FAA Questions
Warning areas often contain hazards such as aerial gunnery or guided missiles
148
4D FAA Questions
You must have the controlling agency's permission to fly through a restricred area
149
4D FAA Questions
Milirtary aircraft are normally operating at speeds in excess of 250 knots along MTRs
150
4D FAA Questions
MTRs are classified as VR or IR and are identified with a three or four number designation based on the type and altitude of the operations conducted on the specific route
151
5A FAA Questions
You may not use a transponder for operations in controlled airspace unless it has been tested and inspected within at least the preceding 24 calandar months
152
5A FAA Questions
When making routine transponder code changes, you should avoid inadvertent selection of 7500, 7600, 7700
153
5A FAA Questions
The standard transponder code for VFR operations is 1200
154
5A FAA Questions
Controllers reference traffic from your airplane as if it were a clock
155
5A FAA Questions
Basic radar service in the terminal radar program includes traffic advisories and limited vectoring to VFR aircraft
156
5A FAA Questions
Pilots of departing VFR aircraft requestion radar traffic information should notify ground control on initial contact with their request and proposed direction of flight
157
5A FAA Questions
Automatic terminal information service (ATIS) is the continuous broadcast of noncontrol airport information at selected high activity terminal areas
158
5A FAA Questions
The letters VHF/DF appearing in an *Airport/Facility Directory airport listing indicate that the FSS has direction finding equipment*
159
5A FAA Questions
To use VHF/DF facilities for assistance in locating your aircraft's position, you must have a VHF transmitter and receiver
160
5B FAA Questions
The correct method of stating 4,500 feet MSL is "four thousand five hundred"
161
5B FAA Questions
In the United States, you add hours to convert local time to Zulu time. For example, if you depart an airport in the eastern daylight time zone at 0945 EDT for a 2 hour flight to an airport located in the central daylight time zone, you will land at approximately 1545 Zulu time (0945 EDT + 4:00 = 1345Z + 2:00 (flight time) = 1545Z
162
5B FAA Questions
Prior to entering an airport advisory area, you should contact the local FSS for airport and traffic advisories
163
5B FAA Questions
When you are landing at an airport with a part-time tower and the tower is not in operation, you should monitor airport traffic and announce your position and intentions on the designated
164
5B FAA Questions
The recommended communication procedure when using a CTAF is to transmit your intentions when you are 10 miles out and give position reports in the traffic pattern
165
5B FAA Questions
Pilots should state their position on the airport when calling the tower for takeoff
166
5B FAA Questions
An air traffic clearance is an authorization by ATC for you to proceed under specified traffic conditions within controlled airspace
167
5B FAA Questions
After landing at a controlled airport, you should contact ground control when advised to do so by the tower
168
5B FAA Questions
If your aircraft radio fails when landing at a controlled airport, you should observe the traffic flow, enter the pattern, and look for a light signal from the control tower
169
5B FAA Questions
Each color or color combination of light signal has a specific meaning for an aircraft in flight or on the airport surface. For example, after a communication failure, a steady green light signal from the control tower indicates that you are cleared to land
170
5B FAA Questions
You may not operate an aircraft in formation flight except by prior arrangement with the pilot in command of each aircraft
171
5B FAA Questions
When activated, an emergency locator transmitter (ELT) transmits on designated emergency frequencies
172
5B FAA Questions
ELT false alarms can be minimized by monitoring 121.5 MHz during flight, prior to engine shut down, and after maintenance
173
5B FAA Questions
The battery in an emergency locator transmitter (ELT) must be replaced, or recharged if the battery is rechargeable, after one-half of its useful life. An ELT may be tested during the first five minutes after the hour
174
5C FAA Questions
Airport listings in the *Airport/Facility Directory* (A/FD) include the airport location, availability and type of radar services, as well as communication and navigation frequencies. The designation "Rgt tfc." indicates that the runway has right-hand traffic
175
5C FAA Questions
You can refer to the *Airport/Facility Directory* (A/FD) for information regarding parachute jumping and glider operations
176
5C FAA Questions
Advisory circulars are divided into a variety of subjects, and are identified by numbers corresponding to the different Part numbers of the FARs. For example, ACs specifically related to airmen are issued under 60. Airspace information is contained in ACs issued under 70, while air traffic control and general operations can be found under 90.
177
5C FAA Questions
FAA advisory circulars (some free, others at cost) are available to all pilots and can be ordered from the U.S. Government Printing Office
178
6A FAA Questions
Variations in altimeter settings between weather reporting points are primarily caused by the unequal heating of the earth's surface
179
6A FAA Questions
Friction causes wind to shift directions when near the earth's surface
180
6A FAA Questions
Convective circulation patterns associated with sea breezes are caused by the temperature differences between land and sea. The result is cool, dense air moving inland from over the water
181
6B FAA Questions
Stability of an airmass is decreased by warming from below
182
6B FAA Questions
The actual lapse rate can be used to determine the stability of the atmosphere
183
6B FAA Questions
A smooth, stable layer of air and a temperature increase with altitude are features of a temperature inversion. Visibility in an inversion is usually poor due to trapped pollutants. In addition, high humidity beneath a low-level temperature inversion can contribute to the formation of fog, haze, or low clouds
184
6B FAA Questions
A surface-based temperature inversion is often produced by terrestrial radiation on clear, cool nights when the air is relatively calm
185
6B FAA Questions
Every physical process of weather is accompanied by a heat exchange
186
6B FAA Questions
Water vapor is added to the atmosphere by evaporation and sublimation
187
6B FAA Questions
The amount of moisture in the air depends on air temperature
188
6B FAA Questions
Dewpoint is the temperature to which air must be cooled to become saturated
189
6B FAA Questions
You can calculate cloud bases by using the following formula: _Temperature (_0F_) - Dewpoint_ (0F) X 1,000 4.4(F0)
190
6B FAA Questions
Frost forms when the temperature of the collecting surface is at or below the dewpoint of the surrounding air and the dewpoint is below freezing
191
6B FAA Questions
If frost is not removed from the wings before flight, it may spoil the smooth airflow over the wings, decrease lift, and increase drag, preventing the aircraft from becoming airborne at normal takeoff speed
192
6B FAA Questions
Clouds, fog, or dew always form when water vapor condenses
193
6B FAA Questions
A small and decreasing temperature/dewpoint spread indicates conditions are favorable for the formation of fog
194
6B FAA Questions
Clouds are grouped by families according to their altitudes (height range)
195
6B FAA Questions
The term *nimbus* describes clouds which produce rain
196
6B FAA Questions
When moist air flows upslope and cools to its saturation point, it produces: * Stratus clouds if the air is stable * Cumulus clouds if the air is unstable
197
6B FAA Questions
Radiation fog forms in moist air over low, flat areas on clear, calm nights
198
6B FAA Questions
Advection and upslope fog require wind for formation. Both types of fog commonly occur along coastlines where sea breezes transport air from warm water to the cooler land surfaces
199
6B FAA Questions
Low-level turbulence and aircraft icing are associated with steam fog
200
6B FAA Questions
Vertical cloud development and turbulence result from the lifting of unstable air
201
6B FAA Questions
Ice pellets at the surface are an indication of a temperature inversion and freezing rain at a higher altitude
202
6B FAA Questions
Stable air is generally smooth with layered or stratiform clouds. Visibility is usually restricted, with widespread areas of clouds and steady rain or drizzle
203
6B FAA Questions
Moist unstable air causes the formation of cumuliform clouds, showers, turbulence, and good surface visibility
204
6B FAA Quesitons
Fronts are boundaries between airmasses
205
6B FAA Questions
One of the most easily recognized discontinuities across a front is the change in temperature
206
6B FAA Questions
When you are flying across a front, you will notice a change in wind direction. Wind speed may also change
207
6B FAA Questions
Steady precipitation with little turbulence usually precedes a warm front
208
6C FAA Questions
Thunderstorm formation requires unstable conditions, a lifting force, and high moisture levels
209
6C FAA Questions
A squall line is a non-frontal band of thunderstorms that often produces the most intense weather hazards for aircraft
210
6C FAA Questions
The cumulus stage is characterized by continuous updrafts
211
6C FAA Questions
Thunderstorms reach the greatest intensity during the mature stage which is signaled by the beginning of precipitation
212
6C FAA Questions
A dissipating thunderstorm is characterized by downdrafts
213
6C FAA Questions
Severe turbulence often exists in a cumulonimbus cloud, the most turbulent of all clouds
214
6C FAA Questions
Lightning is always associated with thunderstorms
215
6C FAA Questions
If you encounter severe turbulence during flight, set the power for turbulence penetration airspeed, maintain a level flight attitude, and accept variations in airspeed and altitude
216
6C FAA Questions
When sufficient moisture is present, towering cumulus clouds indicate the presence of convective turbulence
217
6C FAA Questions
Wingtip vortices are creted when an airplane generates lift
218
6C FAA Questions
The greatest vortex strength occurs when the generating aircraft is heavy, slow, and in a clean configuration
219
6C FAA Questions
Wingtip vortices tend to sink below the flight path of the aircraft which generated them. They are most hazardous during light, quartering tailwind conditions
220
6C FAA Questions
Mountain wave turbulence can be anticipated when the winds across a ridge are 40 knots or more, and the air is stable
221
6C FAA Questions
The crests of mountain waves may be marked by lens-shaped, or lenticular, clouds
222
6C FAA Questions
Although they may appear stationary, standing lenticular clouds may contain winds of 50 knots of more
223
6C FAA Questions
Wind shear often exists near the surface when there is a frontal system, thunderstorm, or temperature inversion with strong upper-level winds in the area. Wind shear is also associated with clear air turbulence
224
6C FAA Questions
Wind shear may occur during a low-level temperature inversion when cold, still surface air is covered by warmer air which contains winds of 25 knots or more at 2,000 to 4,000 feet above the surface
225
6C FAA Questions
Wind shear can exist at any altitude and may occur in all directions
226
6C FAA Questions
Visible moisture is necessary for structural icing to form. Freezing rain usually produces the highest rate of ice accumulation
227
7B FAA Questions
Winds are reported in reference to true north
228
7B FAA Questions
Wind gusts are reported using a G followed by the highest gust
229
7B FAA Questions
Precailing visibility is reported in statute miles, as indicated by the abbreviation SM
230
7B FAA Questions
A ceiling is the lowest broken or overcast layer, or vertical visibility into an obstruction
231
7B FAA Questions
In controlled airspace, VFR conditions exist with a visibility of at least 3 statute miles and a ceiling of 1,000 feet or more
232
7B FAA Questions
Cloud heights of the vertical visibility into an obscuration are reported with three digits in hundreds of feet
233
7B FAA Questions
The beginning of the remarks section is indicated by the code RMK. The remarks section reports weather considered significant to aircraft operations
234
7B FAA Questions
PIREPs use a standard format. Note that altitudes are given in hundreds of feet above mean sea level (MSL)
235
7B FAA Questions
TAF's (Terminal Aerodrome Forcast) usually are valid for a 24-hour period and are similar to those used in METARs.
236
7B FAA Questions
Cumulonimbus (CB) is the only type of cloud included in the TAF
237
7B FAA Questions
You should refer to the area forcast to determine forecast weather conditions between reporting stations and over several states. The area forecast is helpful in determining weather at airports which do not have TAFs
238
7B FAA Questions
In a winds and temperatures aloft forecast, winds are given in true direction and speed is shown in knots
239
7B FAA Questions
Wind direction and speed information on an FD is shown by a four-digit code. The first two digits are the wind direction in tens of degrees. Wind speed is shown by the second two digits. The last two digits indicate the temperature in degrees Celsius. All temperatures above 24,000 feet are negative
240
7B FAA Questions
To decode a forecast of winds between 100 and 199 knots, subtract 50 from the two-digit direction code and multiply by 10. Then, add 100 to the two-digit wind speed code. If the code 9900 is used, it means the winds are light and variable
241
7B FAA Questions
AIRMETs warn of weather conditions which are particularly hazardous to small, single-engine aircraft
242
7B FAA Questions
SIGMETs warn of weather hazards, such as severe icing, which concern all aircraft
243
7B FAA Questions
Convective SIGMETs warn of weather hazards including tornadoes, embedded thunderstorms, and hail 3/4 inch or greater in diameter
244
7C FAA Questions
A stationary front is depicted with rounded warm front symbols on one side and triangular cold front symbols on the opposite side
245
7C FAA Questions
A station circle on a weather depiction chart shows the visibility, cloud height or ceiling, and weather and/or obstructions to vision
246
7C FAA Questions
For flight planning, the weather depiction chart is most useful for determing general weather conditions and quickly locating areas of adverse weather
247
7C FAA Questions
Radar summary charts depict the location of precipitation along with the type, intensity, and cell movement
248
7C FAA Questions
Individual thunderstorm cells as well as lines of thunderstorms are depicted on radar summary charts. Since radar only reflects precipitation, it does not detect cloud formations
249
7C FAA Questions
In addition to helping you avoid areas of significant turbulence, the information contained on the low-level significant weather prog chart helps you avoid areas where temperatures are conductive to aircraft icing
250
7C FAA Questions
Symbols used to define areas of IFR, MVFR, VFR, and moderate or greater turbulence, as well as the forcast altitude of the freezing level, are depicted in the legend between the two upper panels of the low-level significant weather prog chart
251
7C FAA Questions
On the low-level significant weather prog chart, solid lines enclose areas of precipitation. Shading is used to describe the precipitation conditions and coverage. Continuous precipitation covering more than half of the area is shaded. Intermittent precipitation covering half or less of the area is unshaded
252
7C FAA Questions
Turbulence is depicted on the low-level significant weather prog chart with a peaked symbol. Underneath the symbol, figures indicate the top and base of the turbulence
253
7D FAA Questions
When you contact a weather briefer, identify yourself as a pilot flying VFR and provide the briefer with your aircraft number of your name, type of aircraft, intended route, destination, and other relevant background data for the flight
254
7D FAA Quesitons
The standard briefing provides the most complete information concerning weather for your flight. When you request a standard briefing, the weather briefer assumes you have not received any preliminary information
255
7D FAA Questions
Request an abbreviated briefing to update weather information from mass dissemination sources. e.g. telephone information briefing service, or an earlier briefing
256
7D FAA Questions
You should request an outlook briefing when your proposed departure is six or more hours in the future
257
7D FAA Questions
EFAS facilities provide actual weather information, including any thunderstorm activity which might affect your route
258
7D FAA Questions
The frequency for EFAS (Flight Watch) below 18,000 feet MSL is 122.0 MHz
259
7D FAA Questions
TWEB recordings are broadcast over selected NDBs and/or VORs. The recorded messages typically provide a variety of information including specific route forecasts and winds aloft information
260
8A FAA Questions
Low atmospheric pressure, high temperature, and high humidity all result in decreased air density and a corresponding increase in density altitude
261
8A FAA Quesitons
Pressure altitude and density altitude are equal only at standard temperature
262
8A FAA Questions
As density altitude increases, engine power output, propeller efficiency, and aerodynamic lift all decrease
263
8A FAA Questions
Both density altitude and pressure altitude calculations may be solved using a density altitude chart
264
8A FAA Questions
High density altitude will reduce aircraft takeoff performance
265
8A FAA Questions
Headwind and crosswind components are computed by using a crosswind component graph
266
8A FAA Questions
Takeoff performance charts show the total distance required to clear a 50-foot obstacle. In addition, some provide estimates of ground roll distance prior to liftoff
267
8A FAA Questions
Total distance required to land and approximate ground roll distance after landing can be determined by using a landing distance graph or table
268
8A FAA Questions
The best angle-of-climb airspeed (Vx) provides the greatest gain in altitude in the shortest distance during climb after takeoff
269
8A FAA Questions
The best rate-of-climb airspeed (Vy) provides the greatest gain in altitude over a period of time
270
8A FAA Questions
A high density altitude decreases engine performance, aerodynamic lift, and propeller efficiency with a resulting reduction in climb performance
271
8A FAA Questions
Cruise performance tables are used to calculate manifold pressure, fuel flow, fuel consumption, and true airspeed.
272
8B FAA Questions
Basic empty weight includes the weight of the standard airplane, optional equipment, unusable fuel, and full operating fluids including full engine oil
273
8B FAA Questions
The standard weight of gasoline is 6 pounds per gallon. To convert gallons to pounds, multiply by 6 (20 fallons times 6 equals 120 pounds). To convert pounds to gallons, divide by 6 (30 pounds divided by 6 equals 5 gallons)
274
8B FAA Questions
To find the CG location, divide the total moment by the total weight
275
8B FAA Questions
If the total moment falls between the fore and aft moment limits given in the table for that total weight, then the aircraft is within CG limits
276
8B FAA Questions
The weight shift formula can be used to calculate the amount of weight that must be moved a specific distance or to determine the distance a specific weight would need to move to bring the CG within approved limits. The formula is: _Weight Moved_ = _Distance CG Moves_ Aircraft Weight = Distance Between Arm Locations
277
8C FAA Questions
To find an estimated time enroute (ETE), first calculate groundspeed, then compute the time to cover the remaining distance. To compute an estimated time of arrival (ETA), add the estimated time enroute to the time over the last checkpoint
278
9A FAA Questions
Magnetic course is true course corrected for local magnetic variation
279
9A FAA Questions
Magnetic heading is magnetic course corrected for the effects of wind
280
9A FAA Questions
Compass heading is magnetic heading corrected for compass deviation
281
9A FAA Questions
On magnetic courses from 00 to 1790 above 3,000 feet AGL, VFR cruising altitudes are odd thousands plus 500 feet. On magnetic courses from 1800 to 3590 above 3,000 feet AGL, VFR cruising altitudes are even thousands plus 500 feet
282
9A FAA Questions
Day VFR flights must carry enough fuel to fly to the first point of intended landing, and to fly after that for an additional 30 minutes. A reserve of 45 minutes is required for night VFR flights
283
9A FAA Questions
The initial cruising altitude should be entered on the flight plan, even if an altitude change is anticipated later in the flight
284
9A FAA Questions
The fuel on board is the total amount of usable fuel in hours and minutes
285
9A FAA Questions
If no stopover or more than one hour is expected, the name of the destination airport should be entered on the flight plan
286
9A FAA Questions
VFR flight plans must be closed with the nearest FSS or other FAA facility upon landing
287
9B FAA Questions
When the CDI needle is centered with a TO indication, the radial you are on is the reciprocal of the course set by the OBS. To determine which course takes you to a VOR from a specific location on a sectional chart, plot the course and note where it intersects the VOR compass rose
288
9B FAA Questions
The CDI indicates whether the aircraft is left or right of the station on the selected course
289
9B FAA Questions
The standard VOR indicator displays course information independent of aircraft heading
290
9B FAA Questions
When the VOR indicator displays an OFF flag (or similar indication), the aircraft is either directly over the station or 900 to either side of the course set in your VOR indicator. An OFF flag (or similar indication) also can mean that the tuned VOR station's signal is unreliable
291
9B FAA Questions
You can determine your position on a chart by platting the intersection of LOPs from two or more VORs
292
9C FAA Questions
The needle on a fixed-card ADF points to the relative bearing
293
9C FAA Questions
Magnetic heading (MH) + relative bearing (RB) = magnetic bearing (MB) to the station
294
9C FAA Questions
Once you are established on an inbound course with the proper wind correction, the head of the ADF needle indicates the wind correction angle and points in the opposite direction as the correction
295
9C FAA Questions
When the magnetic heading is set on a movable-card ADF indicator, the head of the needle points to the magnetic bearing to the station and the tail of the needle points to the magnetic bearing from the station. To determine relative bearing, turn the knob so 00 is at the top, or subtract the magnetic heading from the magnetic bearing to the station
296
10A FAA Questions
During night flight, the most effective method of looking for other aircraft is to scan small sectors slowly and to use off-center viewing
297
10A FAA Questions
To adapt the eyes for night flying, avoid bright white lights at least 30 minutes before your flight
298
10A FAA Questions
Lighted position lights must be displayed on an aircraft from sunset to sunrise
299
10A FAA Questions
Night is the time between the the end of evening civil twilight and the beginning of morning civil twilight
300
10A FAA Questions
Interpreting the position lights of other aircraft can help you determine their direction of movement. For example, if you see a red position light to the right of a green light, the aircraft is flying toward you. A steady red and flashing red light indicate the aircraft is crossing to your left and a steady white light combined with a flashing red light identify an aircraft flying away from you
301
10A FAA Questions
Your landing approaches at night should be made the same as during the daytime to reduce the effects of landing illusions
302
10A FAA Questions
A state of temporary confusion resulting from misleading information being sent to the brain by various sensory organs is defined as disorientation
303
10A FAA Questions
Relying on the instruments and believing their indications, regardless of how your body feels, are the keys to maintaining orientation during flight at night or in marginal weather conditions
304
10A FAA Questions
You are more susceptible to disorientation if you use body signals to interpret flight attitudes
305
10A FAA Questions
Hypoxia is a state of oxygen deficiency in the body
306
10A FAA Questions
Large accumulations of C in the body can result in symptoms such as a loss of muscular power
307
10A FAA Questions
Between cabin pressure altitudes of 12,500 feet MSL and 14,000 feet MSL, the flight crew is required to use supplemental oxygen after 30 minutes. Above 14,000 feet MSL, the crew is required to use supplemental oxygen for the entire duration of the flight and above 15,000 feet MSL, each aircraft occupant must be provided with it
308
10A FAA Questions
Hyperventilation is rapid or deep breathing which can be caused by emotional tension, anxiety, or fear. Hyperventilation can occur while breathing supplemental oxygen
309
10A FAA Questions
You should be able to overcome the symptoms, or avoid the occurrence of hyperventilation by slowing the breathing rate, breathing into a bag, or talking aloud.
310
10B FAA Questions
The pilot in command of an aircraft is directly responsible for, and is the final authority as to, the operation of that aircraft. In an in-flight emergency requiring immediate action, the pilot in command may deviate from any rule to the extent required to meet that emergency
311
10B FAA Questions
The pilot in command is responsible for ensuring that the pre-takeoff breifing of passengers is completed
312
11A FAA Questions
An airworthiness certificate is valid when the aircraft is maintained according to FARs. A special flight permit may allow an aircraft to be relocated, tested, or demonstrated, if it is capable of safe flight within the limits of the flight permit
313
11A FAA Questions
The owner of operator is primarily responsible for maintaining an aircraft in an airworthy condition
314
11A FAA Questions
The pilot in command is responsible for determining that an aircraft is safe for flight
315
11A FAA Questions
Some aircraft include a minimum equipment list (MEL), which lists the equipment that may be inoperatice based on the flight conditions. A pilot may fly an airplane with inoperative instruments or equipment only if that equipment is not required by the FARs or by the MEL. The inoperative equipment must not constitute a hazard to the aircraft, and the inoperative equipment must be removed or deactivated and placarded as inoperative
316
11A FAA Questions
An aircraft preflight inspection for the first flight of the day, should be accomplished by a thorough and systematic means recommended by the manufacturer
317
11A FAA Questions
Always perform a walkaround inspection prior to every flight. During your preflight, you should use a written checklist to ensure that all necessary items are checked in a logical sequence