Progress Relearn Flashcards

(50 cards)

1
Q

Medical classes and privileges

A

First-Class Medical: Required for Airline Transport Pilots (ATP).
Validity: 12 months (under 40), 6 months (40 or older).

Second-Class Medical: Required for Commercial Pilots (carry persons or property for compensation).
Validity: 12 months, regardless of age.

Third-Class Medical: Required for Student, Recreational, and Private Pilots.
Validity: 60 months (under 40), 24 months (40 or older).

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2
Q

Student pilot certificate and temporary certificate expiration

A

temporary expires after 120 days, regular student pilot cert does not expire

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3
Q

currency vs proficiency

A

Currency is the legal, regulatory minimum required to act as pilot in command ensuring you are legal to fly. Proficiency is the measure of your actual skill, confidence, and ability to handle various conditions and emergencies safely. While currency makes you legal, proficiency keeps you safe.

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4
Q

What is a private pilot flight review

A

required by the FAA every 24 calendar months to act as pilot in command, is a minimum 2-hour proficiency check (1 hour ground, 1 hour flight) with a CFI to ensure safety
Passenger currency requires 3 day takeoff and landings and 3 night takeoff and landings as PIC

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5
Q

AV1ATES

A

For airframe, engine, and prop -

> Annual Inspection - by IA-certified mechanic
VOR Check - test navigation equipment every 30 days (IFR only)
100 hours inspection - full inspection of aircraft used for commercial use
Airworthiness Directives - FAA issued mandatory actions to be taken
Transponder check - test to ensure accurate data transmission to ATC every 24 months
ELT inspection - check every 12 months, replace after 1 hour continuous use or 50% battery life
Static system and altimeter - every 24 months

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6
Q

How is lift created

A

> Pressure Differential (Bernoulli’s Principle): Air travels faster over the curved top surface of a wing, creating lower pressure (a partial vacuum effect) compared to the higher pressure on the bottom, which pushes the wing up.
Action and Reaction (Newton’s Third Law): The wing is designed to deflect oncoming air downwards. According to Newton’s law, this downward acceleration of air produces an equal and opposite upward force on the wing.
Angle of Attack: Tilting the wing upward increases the amount of air deflected downwards, generating more lift.
Factors Affecting Lift: Lift depends on air density, velocity (speed), surface area of the wing, and the airfoil’s shape.

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7
Q

Factors Affecting Air Density

A

> Altitude: Air becomes less dense as altitude increases because pressure drops.
Temperature: Warmer air is less dense because molecules spread out.
Pressure: Higher pressure forces air molecules closer together, increasing density.
Humidity: Humid air is less dense than dry air because water molecules are lighter than nitrogen/oxygen molecules.

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8
Q

How does headwind affect an aircraft

A

A headwind blows directly against an aircraft’s direction of travel, increasing airspeed relative to the ground. This enhances lift for shorter, safer takeoffs and landings. During cruise, it reduces ground speed, leading to longer flight times and increased fuel consumption.

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9
Q

What is a METAR

A

a standardized hourly report of current ground-level weather conditions at an airport as a live snapshot reported in AGL in relation to the airport

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10
Q

What is an AIRMET

A

routinely issued every 6 hours by the Aviation Weather Center (AWC), with valid periods of 6 hours. Unscheduled amendments are issued as necessary. these are forecasts delivered in MSL

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11
Q

What is a TAF

A

Terminal Area Forecast Issued four times daily at 0000Z, 0600Z, 1200Z, and 1800Z, covering a 24-hour or 30-hour period. They are valid from the time of issuance and updated every 6 hours, though they may be amended (TAF AMD) more frequently to reflect changing, severe, or unforecasted weather conditions reported in AGL

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12
Q

What types of ceilings are presented in a weather report

A

BKN - Broken
OVC - Overcast
VV - Vertical visibility

Few (FEW) and Scattered (SCT) are not ceilings

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13
Q

What factors affect stall speed

A

> Weight: A heavier aircraft requires a higher angle of attack to produce sufficient lift, increasing the stall speed.
Load Factor (G-force): Increased load factor (e.g., in a turn or pull-up) increases stall speed. A 60° bank turn, for example, increases stall speed by approximately 40%.
Configuration: Extending flaps or landing gear changes the lift characteristics. While flaps generally lower the stall speed, they also increase drag.
Air Density/Altitude: As air density decreases with altitude, the true airspeed (TAS) at which a plane stalls increases, though indicated airspeed (IAS) remains relatively constant.
Wing Contamination: Ice, frost, or snow disrupts airflow, reducing lift and increasing stall speed by up to 30%.
Center of Gravity: A more forward CG typically increases the required tail-down force, forcing a higher angle of attack and increasing stall speed.
Power Setting: Higher thrust can reduce stall speed by providing a vertical component of lift.

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14
Q

What type of engine is found in our aircraft

A

Textron Lycoming IO-360-L2A
180hp @ 2700 RPMs
>Normally Aspirated - draws in air using only atmospheric pressure, no turbo or supercharger
>Direct Drive - motor is coupled directly to the load without intermediate gears, belts, or chains
>Air-Cooled - dissipates heat directly from the cylinder barrels and heads, often using metal fins to increase surface area, without requiring radiators, water pumps, or coolant
>Horizontally Opposed - more compact and superior balance
>Fuel Injected - use a pump to inject pressurized fuel directly into the intake manifold or cylinder, offering improved efficiency, better fuel distribution, and increased power compared to carburetors
>Four Cylinders

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15
Q

What is AHRS and how does it work (solid state laser system, accelerometers, tilt and rate sensors, microprocessors)

A

Attitude and Heading Reference System is a modern, solid-state avionics unit that replaces traditional mechanical gyroscopic instruments to provide precise, real-time 3D orientation data (pitch, roll, yaw) and heading

Solid state Laser systems: Measure the rate of rotation (angular velocity) around the roll, pitch, and yaw axes to detect changes in orientation.
Accelerometers: Measure linear acceleration, including gravity, to establish pitch and roll angles relative to the Earth.
Magnetometers: Measure the Earth’s magnetic field to provide a stable, consistent heading (yaw) reference.
Microprocessors: Process this sensor data through complex algorithms to deliver accurate, 3D orientation data to the pilot.

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16
Q

Class A airspace

A

Vertical Limits: 18,000 ft MSL to FL 600.
IFR only
Not depicted on charts

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17
Q

Class B airspace

A

Surface to 10,000’ MSL surrounding nations busiest airports with 30 NM mode C veil
3 SM clear of clouds
Solid dark blue lines

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18
Q

Class C airspace

A

5 NM radius from surface to 1,200’ MSL, then 10 NM radius up to 4,000’ MSL
3 NM, 1,5,2
Solid magenta circles

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19
Q

Class D airspace

A

Surface to 2,500’ AGL
3 NM, 1,5,2
Dashed blue circles

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20
Q

Class E Airspace

A

Controlled airspace not classified as A, B, C, or D
Depicted on charts when below 14,500’ MSL but extends up to 18,000’ MSL and all airspace above FL 600
Within shaded magenta lines, begins at 700 AGL
Dashed magenta line indicates starts at surface
Fuzzy blue or no color indicates starts at 1,200’ AGL
Above 10,000’ MSL - 5 SM 1,1,1SM
Below 10,000’MSL - 3 SM 1,5,2

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21
Q

Class G airspace

A

UNCONTROLLED AIRSPACE Surface to the base of overlying Class E airspace
Day Below 1,200’ AGL - 1 SM clear of clouds
Night Below 1,200’ AGL - 3 SM 1,5,2
Day above 1,200’ AGL but below 10,000’ MSL - 1 SM 1,5,2
Night above 1,200’ AGL but below 10,000’ MSL - 3 SM 1,5,2
Above 1,200’ AGL AND at or above 10,000’ MSL - 5 SM 1,1,1 SM

22
Q

What is Special Use Airspace

A

Designation for airspace in which certain activities
must be confined, or where limitations may be imposed
on aircraft operations that are not part of those activities.
* Prohibited areas
* Restricted areas
* Warning areas
* Military operation areas (MOAs)
* Alert areas
* Controlled firing areas (CFAs)

23
Q

Prohibited areas

A

depicted on sectional charts as blue-hatched outlined areas labeled with the letter “P” followed by a number (e.g., P-49). These areas, which indicate where flight is permanently forbidden for national security or welfare reasons

24
Q

Restricted Areas

A

depicted on sectional charts as blue, hatched-bordered, enclosed areas labeled with the letter “R” followed by a unique number (e.g., R-4401). These areas indicate hazards like artillery firing or guided missiles, requiring pilot authorization from the controlling agency to enter when active.

25
Warning Areas
depicted on sectional charts as blue hatched lines, similar to restricted areas, and are identified by the letters "W-" followed by a number (e.g., W-110). They are located in international airspace, starting at least 3 NM from the U.S. coast, and indicate potential hazards to non-participating aircraft.
26
Military operation areas (MOAs)
depicted on VFR sectional charts with solid magenta lines featuring short, perpendicular hash marks. These areas are clearly labeled with their names (e.g., “MOA NAME”) and often include, or refer to a tab on the side of the chart for, details on vertical limits, times of use, and controlling agency frequencies.
27
Alert areas
depicted by a dashed or hashed magenta line boundary and labeled with the letter "A" followed by a hyphen and a three-digit number (e.g., A-211). These areas indicate high-volume pilot training or unusual aerial activity, requiring, but not restricting, caution by nonparticipating pilots.
28
Controlled firing areas (CFAs)
not depicted on aeronautical sectional charts. Because hazardous activities, such as ordnance disposal or rocket testing, are immediately suspended upon the spotting of an aircraft, they do not require charting or a change in flight path for non-participating aircraft.
29
National Wildlife Area
depicted on sectional charts by a blue line with a single line of dots on the inside of the boundary. These areas often have associated voluntary or mandatory noise-sensitive altitude restrictions, with pilots requested to maintain at least 2,000 feet AGL above them.
30
Yellow Areas on sectional chart
areas of high population but not necessarily a congested area. intense city lighting is likely to be visible at night to aid in navigation at night.
31
Magenta Flags on sectional chart
represent Visual Flight Rules (VFR) checkpoints or waypoints. They are used to help pilots identify, report, or navigate to specific, easily recognizable landmarks, aiding in situational awareness. They are sometimes associated with specific reporting points, such as near mountain passes.
32
AIRGUS
Advection: Warm, moist air moves over a cold surface. Ice: Water vapor forms directly into ice crystals in arctic regions bellow freezing. Radiation: Forms overnight as ground cools, common in valleys. Ground/Ground-based: Often used to describe radiation fog less than 20 feet thick. Upslope: Moist air is pushed up sloping terrain by wind. Steam: Cold air moves over warmer water.
33
How a thunderstorm forms
when warm, moist air rises rapidly into colder, dry air, fueled by three main ingredients: moisture, instability, and lift.
34
Three stages of thunderstorm
Developing stage, a cumulus cloud is being pushed upward by a rising column of air forming a towering cumulous cloud. Mature stage, updraft continues to feed the storm but precipitation starts to fall creating a downdraft. This is the most dangerous stage and the most likely time for hail, heavy rain, lightning, strong wind, and tornadoes. Dissipating stage, a large amount of precipitation is produced and the updraft is overcome by the downdraft ultimately leaving a remnant anvil shaped cloud.
35
Types of lifting action
Orographic Lifting: Occurs when air is forced upward by terrain, such as mountains, often creating clouds on the windward side and dry, warm conditions on the leeward side. Convective Lifting (Thermal): Caused by intense solar heating of the Earth's surface, which warms the air above it, making the air buoyant and causing it to rise. Frontal Lifting (Wedging): Happens when a cold air mass (dense) pushes a warm air mass (less dense) upward, creating extensive clouds, stratus, and potential thunderstorms. Convergence: Develops when horizontal winds blow inward from different directions into a common area, forcing the air to rise vertically because it has nowhere else to go.
36
How to navigate a thunderstorm
Proceed at maneuvering speed, keep wings level, avoid tight turns, activate icing equipment if available, do not fly underneath the storm, do not turn around in the storm, and do not rely on VFR alone
37
Category class and type
Category is type of aircraft: airplane, glider, rotorcraft, etc. Class specifies design and performance: single-engine land, MEL, SES, MES Type refers to specific make and model, IE: B737
38
Left turning tendancies
Torque Effect: Newton's third law, the clockwise rotation of the propeller (from cockpit) causes a counter-clockwise reaction, rolling the aircraft to the left. Spiraling Slipstream: The propeller creates a corkscrewing slipstream that wraps around the fuselage and strikes the left side of the vertical fin, turning the plane to the left. P-Factor (Asymmetric Loading): At high angles of attack, the descending propeller blade on the right produces more thrust than the ascending blade on the left, causing a yaw to the left. Gyroscopic Precession: When a force is applied to a spinning disc (propeller), the result is felt ahead in the direction of rotation, causing a left yawing motion when the tail rises during takeoff.
39
Micro bursts
Indicators include rapidly descending rain or, in dry areas, a ring of blowing dust/debris beneath virga. Apply maximum available power, pitch for a high angle of attack to maximize climb performance without stalling, and fly straight ahead to exit the area.
40
TFRs
Temporary Flight Restrictions (TFRs) are FAA-issued, short-term limitations on airspace usage to ensure safety or security, covering specific areas for limited times such as VIP movements, natural disasters, and sporting events.
41
ADC computer flight controls
Air Data Computer (ADC) is a critical avionics component that processes pitot-static and temperature inputs to calculate real-time flight data—such as airspeed, altitude, Mach number, and angle of attack—for aircraft displays, autopilot, and flight control systems. It acts as the "digital brain" for these parameters, ensuring precise, automated navigation and control.
42
Use and function of alternator
primary engine-driven electrical power source, converting mechanical energy into direct current (DC) to power avionics, lights, and instruments while recharging the battery in-flight. The primary indicator is a, "low voltage" or "alternator out" annunciator light, or an ammeter showing a negative reading (discharge). Upon failure electrical systems will run off battery for approximately 30min.
43
What standby battery powers
Primary Flight Display, ADC and AHRS, NAV 1, COMM 1, Standby Indicator Lights (illuminate the backup flight instruments—attitude indicator, airspeed indicator, and altimeter)
44
What are magnetos and what does the test in run up show
self-contained, engine-driven electrical generators that produce high-voltage current to fire spark plugs independently of the aircraft's battery/alternator system. As the engine spins, a permanent magnet rotor inside the magneto rotates, inducing a magnetic field in a coil that collapses when breaker points open, creating a high-voltage surge sent to the spark plugs. No RPM Drop: Suggests a broken P-lead (magneto not grounding). Excessive RPM Drop: Suggests a bad plug or faulty magneto. Engine Roughness: Indicates a cylinder is not firing correctly.
45
Engine failure in flight
Airspeed - 68 KIAS Fuel Selector - BOTH Fuel Shutoff Valve - ON (IN) Auxiliary Fuel Pump - ON ---if restart has not occurred--- Mixture - RICH Magnetos - BOTH (START if prop is stopped)
46
Emergency landing during flight
Landing Area - SELECT & INSPECT Airspeed - 68 KIAS ---on final approach--- Mixture - IDLE CUTOFF Fuel Shutoff Valve - OFF (OUT) Flaps - AS REQUIRED Radio/Transponder - 121.5 / 7700 Standby Battery Switch - OFF ---landing assured--- Master Switch (ALT & BAT) - OFF Doors - Unlatch prior to touchdown
47
Charting headwind
Angle difference between wind direction and runway heading, charting a line to the arc representing wind velocity and then horizontally to the left to get the headwind component.
48
What is Hypoxia
Oxygen deficiency in body's tissues. Primarily caused by flying unpressurized aircraft above 10,000 ft without supplemental oxygen, rapid decompression, or oxygen system failure. Symptoms: Include euphoria, headache, impaired judgment, dizziness, fatigue, blurred vision, numbness, and cyanosis (blue lips/fingernails).
49
Types of Hypoxia
Hypoxic Hypoxia: Insufficient oxygen reaching the blood (e.g., high altitude). Hypemic Hypoxia: Blood cannot transport oxygen (e.g., carbon monoxide poisoning). Stagnant Hypoxia: Blood flow is insufficient. Histotoxic Hypoxia: Cells cannot use oxygen (e.g., alcohol/drug impairment).
50
How to determine if inop equipment is required for flight RAKETS
>Reg - 91.205 ATOMATOFLAMES >Airworthiness Directives - FAA website >Kinds of Operation Equipment List-POH >Equipment List - POH >Type Certificate Data Sheet - FAA website >Safety of flight