Aircraft Instruments Overview
73 Questions
0 Views

Aircraft Instruments Overview

Created by
@LighterErhu

Podcast Beta

Play an AI-generated podcast conversation about this lesson

Questions and Answers

What does variation refer to in the context of compass errors?

  • The angular difference between true north and magnetic north. (correct)
  • Indicates a turn to the south under deceleration in the northern hemisphere.
  • The tendency of the compass needle to point down towards the magnetic pole.
  • Difference between indicated and actual magnetic heading due to other magnetic fields.

    • Which of the following best describes deviation in compass errors?

  • The angular difference between true north and magnetic north.
  • The compass needle oscillation caused by turbulence.
  • Indicates a turn to the north during acceleration.
  • Difference between the indicated magnetic heading and the actual heading. (correct)

    • What does the acronym 'ANDS' relate to in the context of acceleration errors?

  • Refers to the oscillation of the compass card during turbulence.
  • Describes how acceleration and deceleration affect compass readings. (correct)
  • Indicates the angular difference between true north and magnetic north.
  • Shows how the compass behaves when turning from east to west.

    • Which statement accurately reflects the turning errors in compass readings?

    <p>Compass readings will lag the actual heading during a left turn.</p> Signup and view all the answers

    What is magnetic dip in relation to compass errors?

    <p>The tendency of the compass needle to point down towards the magnetic pole.</p> Signup and view all the answers

    What describes calibrated airspeed (CAS)?

    <p>Indicated airspeed corrected for installation and instrument errors.</p> Signup and view all the answers

    What is the purpose of the static port in the pitot-static system?

    <p>To allow static pressure to enter the system.</p> Signup and view all the answers

    Which of the following correctly defines the stalling speed in landing configuration?

    <p>V<del>SO</del></p> Signup and view all the answers

    What does the VNE speed represent?

    <p>Never exceed speed.</p> Signup and view all the answers

    How does the airspeed indicator (ASI) determine the speed of the aircraft?

    <p>By comparing ram air with static air pressure.</p> Signup and view all the answers

    Which type of airspeed reflects the actual speed reading of the aircraft?

    <p>Indicated airspeed (IAS)</p> Signup and view all the answers

    What information does a Vertical Speed Indicator (VSI) provide to the pilot?

    <p>Rate of climb or descent.</p> Signup and view all the answers

    What is indicated by VLE?

    <p>Maximum speed for landing gear extended.</p> Signup and view all the answers

    What is the purpose of maneuvering speed (VA)?

    <p>Maximum speed for abrupt control without structural damage</p> Signup and view all the answers

    How is the indicated altitude determined?

    <p>By reading the altitude directly from the altimeter</p> Signup and view all the answers

    What does a Vertical Speed Indicator (VSI) measure?

    <p>Rate of climb or descent in feet per minute</p> Signup and view all the answers

    What characteristic of a gyroscope allows it to maintain its position in space?

    <p>Rigidity in space</p> Signup and view all the answers

    What happens to the altimeter if the static port is blocked?

    <p>The altimeter reads low in climb and high in descent</p> Signup and view all the answers

    What does the attitude indicator display?

    <p>Actual attitude of the aircraft relative to the earth's horizon</p> Signup and view all the answers

    Which type of altitude represents the actual height of an aircraft above mean sea level?

    <p>True altitude</p> Signup and view all the answers

    How does a blocked pitot tube affect the airspeed indicator (ASI)?

    <p>Reads high in climb and low in descent</p> Signup and view all the answers

    What is the primary function of the Turn Coordinator (TC) in an aircraft?

    <p>The Turn Coordinator indicates the rate and quality of turn and serves as an emergency bank indicator if the Attitude Indicator fails.</p> Signup and view all the answers

    How does the Heading Indicator (HI) relate to the aircraft's movement?

    <p>The Heading Indicator senses the airplane's movement and displays its heading based on a 360-degree azimuth.</p> Signup and view all the answers

    What are the meanings of 'Skid' and 'Slip' in relation to the Turn Coordinator?

    <p>'Skid' means the rate of turn is too high for the angle of bank, while 'Slip' indicates the rate of turn is too slow for the angle of bank.</p> Signup and view all the answers

    What unique characteristic does the Magnetic Compass have compared to other aircraft instruments?

    <p>The Magnetic Compass is the only direction-seeking instrument in the airplane.</p> Signup and view all the answers

    How often should the Heading Indicator be aligned with the magnetic compass and why?

    <p>The Heading Indicator should be aligned with the magnetic compass every 15 minutes due to precession.</p> Signup and view all the answers

    What is the significance of maneuvering speed (VA) in aviation?

    <p>Maneuvering speed (V<del>A</del>) is the maximum speed at which abrupt control movements can be made without causing structural damage to the aircraft.</p> Signup and view all the answers

    Describe the process by which an altimeter measures altitude.

    <p>An altimeter measures altitude by sensing pressure changes through aneroid wafers that expand and contract, converting these changes into pointer movements.</p> Signup and view all the answers

    What type of altitude is used to assess airplane performance when non-standard temperatures are accounted for?

    <p>Density altitude is used to assess airplane performance after correcting for non-standard temperature.</p> Signup and view all the answers

    Explain the effect of a blocked static port on the altimeter and VSI readings.

    <p>If the static port is blocked, the altimeter freezes at its last indicated altitude and the VSI reads zero, thus providing incorrect altitude and rate of climb/descent information.</p> Signup and view all the answers

    What characteristic of gyroscopic instruments allows them to remain fixed in space?

    <p>Rigidity in space allows gyroscopic instruments to maintain a fixed position in their plane of rotation.</p> Signup and view all the answers

    How does precession affect the functioning of a gyroscope in aviation instruments?

    <p>Precession causes a gyroscope to react at a 90-degree angle to an applied force, which can affect the accuracy of readings in instruments like the attitude indicator.</p> Signup and view all the answers

    What indication does the altimeter provide when it is set to a standard pressure of 29.92 inHg?

    <p>When set to 29.92 inHg, the altimeter shows pressure altitude, which indicates altitude relative to a standard atmospheric pressure.</p> Signup and view all the answers

    What is the function of a suction gauge in a vacuum system for gyroscopic instruments?

    <p>A suction gauge monitors the available vacuum pressure in the system, ensuring that enough vacuum is present to operate the gyroscopic instruments effectively.</p> Signup and view all the answers

    What is the primary function of the Pitot tube in the pitot-static system?

    <p>The Pitot tube supplies ram air pressure, measuring the dynamic pressure of the air for the airspeed indicator.</p> Signup and view all the answers

    How does the speed indicated on the Airspeed Indicator (ASI) differ from True Airspeed (TAS)?

    <p>Indicated Airspeed (IAS) is the actual reading displayed, while True Airspeed (TAS) is IAS corrected for non-standard pressure and temperature.</p> Signup and view all the answers

    What are the four types of airspeed defined in aviation?

    <p>The four types are Indicated Airspeed (IAS), Calibrated Airspeed (CAS), True Airspeed (TAS), and Groundspeed.</p> Signup and view all the answers

    Describe the significance of the different colored arcs on the ASI.

    <p>The colored arcs represent various speed ranges essential for safe flight operations: green for normal, white for flaps, yellow for caution, and red for never exceed.</p> Signup and view all the answers

    What does VSO represent in aircraft performance metrics?

    <p>V<del>SO</del> is the stalling speed or minimum flight speed in the landing configuration with flaps and gear down.</p> Signup and view all the answers

    Explain the role of the static port in the pitot-static system.

    <p>The static port allows static pressure to enter the system, which is critical for altitude measurements and determining airspeed.</p> Signup and view all the answers

    What does VFE indicate regarding aircraft operation?

    <p>V<del>FE</del> indicates the maximum speed with flaps extended, which is essential for safe operation during landing and takeoff.</p> Signup and view all the answers

    What happens to the airspeed indication if the pitot tube becomes blocked?

    <p>If the pitot tube is blocked, the ASI will indicate a false reading, typically showing a decrease in airspeed as the aircraft climbs.</p> Signup and view all the answers

    Explain the impact of magnetic dip on compass accuracy, especially at the poles.

    <p>Magnetic dip causes the compass needle to point downward towards the magnetic pole, leading to increased error at the poles and zero error at the magnetic equator.</p> Signup and view all the answers

    Describe the significance of the acronym 'UNOS' in understanding compass turning errors.

    <p>'UNOS' stands for undershoot north, overshoot south, indicating that during turns from a north or south heading, the compass will lead or lag the actual heading.</p> Signup and view all the answers

    How does acceleration affect compass readings in the northern hemisphere?

    <p>In the northern hemisphere, acceleration causes the compass to indicate a turn to the north, while deceleration indicates a turn to the south, particularly when flying east or west.</p> Signup and view all the answers

    What can cause compass card oscillation, and how does it affect navigation?

    <p>Compass card oscillation can be caused by turbulence or rough control techniques, resulting in erratic compass readings that complicate navigation.</p> Signup and view all the answers

    Discuss how deviation errors are introduced in compass readings.

    <p>Deviation errors occur due to the influence of other magnetic fields in the airplane, causing a difference between the indicated magnetic heading and the actual heading.</p> Signup and view all the answers

    How does the Turn Coordinator (TC) assist pilots in maintaining turns during flight?

    <p>The Turn Coordinator helps pilots establish and maintain constant rate turns by indicating the rate and quality of the turn using a miniature airplane and an inclinometer.</p> Signup and view all the answers

    What is the primary function of the Heading Indicator (HI) in an aircraft?

    <p>The Heading Indicator provides the primary source of heading information by sensing airplane movement and displaying it in a 360-degree azimuth format.</p> Signup and view all the answers

    Explain the meanings of 'Skid' and 'Slip' indicated by the Turn Coordinator.

    <p>'Skid' indicates excessive rudder pressure with a rate of turn too great for the bank angle, while 'Slip' signifies insufficient rudder pressure with a rate of turn too slow for the bank angle.</p> Signup and view all the answers

    Describe the role of the magnetic compass in an aircraft's instrumentation.

    <p>The magnetic compass is the only direction-seeking instrument, used to set the Heading Indicator and verify its accuracy during flight when flying straight and level.</p> Signup and view all the answers

    Why must pilots align the Heading Indicator with the magnetic compass every 15 minutes?

    <p>Pilots must align the Heading Indicator with the magnetic compass every 15 minutes to correct for precession, which can cause inaccurate heading information.</p> Signup and view all the answers

    How does magnetic dip influence compass readings, and where is this effect most pronounced?

    <p>Magnetic dip causes the compass needle to point down towards the magnetic pole, resulting in inaccuracies. This effect is most pronounced at the poles.</p> Signup and view all the answers

    Explain how acceleration and deceleration affect compass readings in the northern hemisphere.

    <p>In the northern hemisphere, acceleration causes the compass to indicate a turn to the north, while deceleration indicates a turn to the south.</p> Signup and view all the answers

    What is the 'UNOS' acronym, and how does it relate to turning errors in compass navigation?

    <p>'UNOS' stands for 'undershoot north, overshoot south,' indicating how the compass can lag or lead during turns, particularly when turning from north or south headings.</p> Signup and view all the answers

    Describe the cause and impact of compass card oscillation on navigation.

    <p>Compass card oscillation occurs due to turbulence or rough control techniques, leading to erratic movements that can mislead the pilot's directional readings.</p> Signup and view all the answers

    How does deviation impact the indicated magnetic heading of an airplane?

    <p>Deviation is the difference between the indicated magnetic heading and the actual heading caused by other magnetic fields in the airplane.</p> Signup and view all the answers

    Define the term 'Indicated altitude' as it relates to aircraft measurement.

    <p>Indicated altitude is the altitude read directly from the altimeter.</p> Signup and view all the answers

    What are the two primary effects of a blocked static port on altitude and vertical speed indicators?

    <p>If the static port is blocked, the altitude indicator freezes, and the vertical speed indicator reads zero.</p> Signup and view all the answers

    Explain the concept of 'Precession' in gyroscopic instruments.

    <p>Precession is the tilting or turning of a gyro in response to applied force, acting 90 degrees in the direction of rotation from where the force was applied.</p> Signup and view all the answers

    What does the term 'Absolute altitude' mean in aviation?

    <p>Absolute altitude refers to the actual height of an aircraft above the earth's surface.</p> Signup and view all the answers

    How does the maneuvering speed (VA) protect aircraft structure?

    <p>Maneuvering speed (V<del>A</del>) is the maximum speed at which abrupt control movements can be applied without causing structural damage.</p> Signup and view all the answers

    What is the function of the altimeter's aneroid wafers?

    <p>Aneroid wafers expand and contract with pressure changes, translating these movements into altitude readings on the altimeter.</p> Signup and view all the answers

    What information does a Vertical Speed Indicator (VSI) provide, and why can it be unreliable in turbulence?

    <p>The VSI displays the aircraft's rate of climb or descent in feet per minute, but its readings can be delayed by 6-9 seconds in turbulence.</p> Signup and view all the answers

    Describe the role of a suction gauge in the vacuum system of gyroscopic instruments.

    <p>The suction gauge monitors the available vacuum pressure, ensuring the system has enough suction to spin the gyros.</p> Signup and view all the answers

    What is the primary difference between indicated airspeed (IAS) and true airspeed (TAS)?

    <p>IAS is the actual airspeed reading from the airspeed indicator, while TAS is IAS corrected for non-standard pressure and temperature.</p> Signup and view all the answers

    Explain the function of the pitot tube in the pitot-static system.

    <p>The pitot tube measures ram air pressure, which is essential for determining airspeed by comparing it with static pressure.</p> Signup and view all the answers

    Describe the relationship between static pressure and the functioning of the airspeed indicator.

    <p>The airspeed indicator compares ram air pressure from the pitot tube with static pressure to determine the aircraft's speed.</p> Signup and view all the answers

    What do the colored arcs on the airspeed indicator (ASI) represent?

    <p>The colored arcs indicate different speed ranges: green for normal operating range, white for flap-operating range, yellow for caution, and red for never exceed speed.</p> Signup and view all the answers

    What is VNO and its significance in aviation?

    <p>V<del>NO</del> is the maximum structural cruising speed; flying above this speed could potentially exceed structural limits.</p> Signup and view all the answers

    How does calibrated airspeed (CAS) differ from indicated airspeed (IAS)?

    <p>CAS is the IAS corrected for installation and instrument errors, providing a more accurate representation of airspeed.</p> Signup and view all the answers

    What effect does icing have on the pitot tube, and how do pilots mitigate this?

    <p>Icing can block the pitot tube, leading to inaccurate airspeed readings; pilots use a pitot heater to prevent this issue.</p> Signup and view all the answers

    Define VSO and explain its importance for landing.

    <p>V<del>SO</del> is the stalling speed in the landing configuration (flaps and gear down); knowing this speed helps prevent stalling during approach.</p> Signup and view all the answers

    Study Notes

    Aircraft Instruments

    • Aircraft instruments aid pilots to operate the aircraft more precisely, enhancing performance and safety.

    Pressure Instruments (Pitot-Static System)

    • Instruments rely on air pressure differences to measure speed and altitude.
    • Pitot tube provides impact (ram) air pressure.
      • Mounted on the wing or nose section, exposed to the relative wind.
      • Higher airspeed leads to increased ram air pressure.
      • Equipped with a pitot heater to prevent icing.
    • Static port allows static pressure from undisturbed air into the system.
      • Located on the side of the fuselage.

    Airspeed Indicator (ASI)

    • Indicates airspeed.
    • Uses both pitot and static pressure.
    • Speed is determined by the differential between ram and static air pressure.
    • Divided into color-coded arcs for different phases of flight:
      • Green arc - normal operating range
      • White arc - flap-operating range
      • Yellow arc - caution range (smooth air only)
      • Red line - never-exceed speed

    Types of Airspeed

    • Indicated airspeed (IAS) - direct reading.
    • Calibrated airspeed (CAS) - IAS corrected for installation and instrument errors.
    • True airspeed (TAS) - CAS corrected for non-standard pressure and temperature.
    • Groundspeed - aircraft speed relative to the earth's surface.

    V-Speeds (Speed Limitations)

    • VSO - stalling speed in the landing configuration (flaps and gear down).
    • VS1 - stalling speed in specific configuration ("clean").
    • VFE - maximum speed with flaps extended.
    • VNO - maximum structural cruising speed.
    • VNE - never exceed speed.
    • VLO - maximum speed for raising or lowering landing gear.
    • VLE - maximum speed with landing gear extended.
    • VA - maneuvering speed (no indication in the ASI).

    Altimeter

    • Measures vertical elevation.
    • Senses pressure changes.
    • Displays altitude in feet.
    • Has three pointers indicating hundreds, thousands, and tens of thousands of feet.
    • Aneroid wafers expand/contract with pressure changes, driving the pointer movement.

    Types of Altitude

    • Indicated altitude - direct reading.
    • Pressure altitude - altitude adjusted to 29.92 inHg.
    • True altitude - actual height above mean sea level.
    • Density altitude - pressure altitude corrected for temperature, used for performance calculations.
    • Absolute altitude - actual height above the earth's surface.

    Vertical Speed Indicator (VSI)

    • Displays rate of climb/descent in feet per minute (fpm).
    • Significant lag (6-9 seconds), making it unreliable in turbulence.

    Pitot-Static System Blockage

    • Blocked pitot tube - ASI reads high in climb, low in descent.
    • Blocked static port - ASI reads low in climb, high in descent; altimeter freezes; VSI reads zero.

    Gyroscopic Instruments

    • Utilize a rapidly spinning wheel (gyroscope) with concentrated weight around its rim.

    Characteristics of Gyroscopes

    • Rigidity in space - the spinning wheel remains fixed in its plane of rotation.
    • Precession - a gyro reacts to a force as if it were applied 90 degrees in the direction of rotation.

    Vacuum (Suction) System

    • Engine-driven or electrically driven.
    • Creates a partial vacuum to spin the gyros.

    Suction Gauge

    • Monitors vacuum pressure in the system.

    Attitude Indicator (AI)

    • Displays aircraft attitude relative to the horizon.

    Compass Errors

    • Variation- difference between true and magnetic north.
    • Deviation - difference between indicated magnetic heading and actual heading, caused by magnetic fields within the aircraft.
    • Magnetic dip - compass needle points downwards, greatest at the poles.
    • Acceleration errors - compass indicates a turn to the north during acceleration, and to the south during deceleration, most noticeable on east and west headings.
    • Turning errors - causes the compass to lead or lag the actual magnetic heading during turns.
    • Compass card oscillation - erratic movement of the compass card due to turbulence or control technique.

    Engine Instruments

    • Tachometer - engine speed in rpm.
    • Oil temperature gauge - engine oil temperature (°C).
    • Oil pressure gauge - pressure in the oil system (psi).
    • Fuel quantity gauge - remaining fuel quantity (gallons).
    • Fuel flow indicator - rate of fuel consumption (gph).
    • Exhaust gas temperature gauge - exhaust gas temperature (°C).
    • Manifold pressure gauge - pressure in the intake manifold (inHg).
    • Cylinder head temperature gauge - temperature of the cylinder heads (°C).

    Aircraft Instruments: Flight Guidance Tools

    • Pilots rely on aircraft instruments for precise control, optimal performance, and enhanced safety.
    • Instruments provide essential information about the aircraft’s position, attitude, speed, and engine operation.

    Pressure Instruments: Pitot-Static System

    • The Pitot-Static system uses air pressure differences to measure speed and altitude.
    • It relies on ram air pressure from the pitot tube and static pressure from the static port.
    • Pitot tubes are vulnerable to icing, requiring a pitot heater for reliable operation.

    Airspeed Indicator (ASI)

    • Displays the aircraft's speed relative to the airmass.
    • Utilizes both pitot and static pressure, measuring the difference between them.
    • Features color-coded arcs indicating speed ranges for different flight phases:
      • Green arc: Normal operating range
      • White arc: Flap-operating range
      • Yellow arc: Caution range (for smooth air conditions)
      • Red line: Never-exceed speed

    Types of Airspeed

    • Indicated airspeed (IAS): The direct reading from the ASI.
    • Calibrated airspeed (CAS): IAS corrected for instrument and installation errors.
    • True airspeed (TAS): CAS corrected for non-standard pressure and temperature.
    • Groundspeed: The aircraft's speed relative to the Earth's surface.

    V-Speeds: Airspeed Limitations

    • VSO: Stalling speed in the landing configuration (flaps and gear down).
    • VS1: Stalling speed in a “clean” configuration (flaps and gear up).
    • VFE: Maximum speed with flaps extended.
    • VNO: Maximum structural cruising speed.
    • VNE: Never exceed speed.
    • VLO: Maximum speed for extending or retracting landing gear.
    • VLE: Maximum speed with landing gear extended.
    • VA: Maneuvering speed, the maximum speed for abrupt control movements without structural damage (not indicated on ASI).

    Altimeter

    • Measures the aircraft's altitude above a reference point.
    • Senses pressure changes and displays altitude in feet.
    • Consists of three pointers indicating hundreds, thousands, and tens of thousands of feet.
    • Employs aneroid wafers, sensitive to pressure changes, which mechanically move the pointers.

    Types of Altitude

    • Indicated altitude: Directly read from the altimeter.
    • Pressure altitude: Altitude corrected to a standard pressure (29.92 inHg).
    • True altitude: Actual height above mean sea level.
    • Density altitude: Pressure altitude corrected for non-standard temperature, used for performance calculations.
    • Absolute altitude: Actual height above the Earth's surface.

    QNH, QNE, and QFE

    • QNH: Local or station pressure.
    • QNE: Standard pressure (29.92 inHg).
    • QFE: Field elevation (airport's pressure altitude).

    Vertical Speed Indicator (VSI)

    • Displays the rate of climb or descent in feet per minute (fpm).
    • Lags in response to turbulence, with a delay of 6-9 seconds.

    Pitot-Static System Blockages

    • Blocked pitot tube: ASI readings are high in climbs and low in descents.
    • Blocked static port: ASI readings are low in climbs and high in descents; the altimeter freezes; and the VSI reads zero.

    Gyroscopic Instruments: Principles

    • Gyroscope: A rapidly spinning wheel with concentrated weight at its rim.

    Gyroscope Properties

    • Rigidity in space: Maintains a fixed position in its spinning plane.
    • Precession: Tilts or turns in response to force, acting at 90 degrees to the force direction and the rotation axis.

    Vacuum System

    • Provides the suction required to spin the gyroscopes.
    • Powered by an engine-driven or electric-driven vacuum pump.
    • Monitored by a suction gauge, indicating the available vacuum pressure.

    Attitude Indicator (AI)

    • Displays the aircraft's attitude relative to the horizon.
    • Also known as the “master instrument.”

    Turn Coordinator (TC)

    • Indicates the rate and quality (skid or slip) of turns.
    • Provides an emergency source of bank information if the AI fails.
    • Consists of a miniature airplane and an inclinometer (ball).
    • Enables maintaining constant rate turns (standard rate: 3 degrees per second).
    • Skid: Excessive rudder pressure, ball is outside the turn.
    • Slip: Insufficient rudder pressure, ball is inside the turn.
    • Correction: Apply rudder pressure towards the ball (“step on the ball”).

    Heading Indicator (HI)

    • Displays heading based on a 360-degree azimuth without the final zero.
    • Primary source of heading information when set.
    • Provides indirect information about bank.
    • Lacks an automatic north-seeking system.
    • Requires alignment with the Compass every 15 minutes due to precession (during straight and level, unaccelerated flight).

    Magnetic Instruments: Magnetic Compass

    • The only direction-seeking instrument in the aircraft.
    • Used to set the HI before flight and verify its accuracy during flight.
    • Accurate readings only during straight and level, unaccelerated flight.
    • Compass needle aligns with Earth's magnetic fields.

    Compass Errors

    • Variation: The angular difference between true north and magnetic north.
    • Deviation: The difference between indicated magnetic heading and actual heading caused by magnetic fields in the aircraft.
    • Magnetic dip: The compass needle's tendency to dip towards the magnetic pole (greatest at poles, zero at equator).

    Acceleration and Turning Errors

    • Acceleration errors: In the Northern Hemisphere, acceleration indicates a turn toward north, deceleration indicates a turn toward south; more pronounced on east and west headings ("ANDS: accelerate north, decelerate south").
    • Turning errors: Cause the compass to lead or lag during turns; in the Northern Hemisphere, it indicates a turn westward from a heading of north, and eastward from a heading of south ("UNOS: undershoot north, overshoot south").
    • Compass card oscillation: Erratic movement of the compass card due to turbulence or rough control.

    Engine Instruments

    • These instruments monitor engine performance:
      • Tachometer: Engine speed (RPM).
      • Oil temperature gauge.
      • Oil pressure gauge.
      • Fuel quantity gauge.
      • Fuel flow indicator.
      • Exhaust gas temperature gauge.
      • Manifold pressure gauge.
      • Cylinder head temperature gauge.

    Aircraft Instruments

    • Aircraft instruments are used for precise aircraft operation, maximum performance, and enhanced safety.

    Pitot-Static System

    • Pitot-static instruments rely on air pressure differences to measure speed and altitude.
    • The system uses a combination of impact/ram air pressure and static pressure.
    • The pitot tube supplies ram air pressure, and is mounted on the wing or nose section to be exposed to relative wind.
    • Increased airspeed directly equates to increased ram air pressure.
    • Pitot tubes are susceptible to icing and most aircraft are equipped with a pitot heater.
    • The static port allows static pressure to enter the system, and is mounted on the side of the fuselage in an area of relatively undisturbed air.

    Airspeed Indicator

    • Indicates the speed at which the aircraft is moving through the air.
    • This instrument operates using both pitot and static pressure.
    • Speed is determined by comparing ram air to static air pressure: the greater the differential, the greater the speed.
    • The indicator features:
      • Green arc: normal operating range
      • White arc: flap-operating range
      • Yellow arc: caution range, only in smooth air and with caution
      • Red line: never-exceed speed

    Types of Airspeed

    • Indicated airspeed (IAS): Actual airspeed reading.
    • Calibrated airspeed (CAS): IAS corrected for installation and instrument errors.
    • True airspeed (TAS): Airspeed corrected for non-standard pressure and temperature.
    • Groundspeed: Speed of aircraft relative to the earth's surface.

    V-Speeds

    • VSO: Stalling speed or minimum flight speed in the landing configuration (flaps and gear down).
    • VS1: Stalling speed or minimum steady flight speed in a clean configuration.
    • VFE: Maximum speed with flaps extended.
    • VNO: Maximum structural cruising speed.
    • VNE: Never exceed speed.
    • VLO: Maximum speed at which you can safely lower or extend/raise landing gear.
    • VLE: Maximum speed with landing gear extended.
    • VA: Maneuvering speed; maximum speed at which you can apply abrupt control movement without causing structural damage.

    Altimeter

    • Measures vertical elevation above a given reference point.
    • Senses pressure changes and displays altitude in feet.
    • Features 3 pointers/hands to indicate altitude: longest = hundreds of feet; middle = thousands of feet; shortest = tens of thousands of feet.
    • Contains aneroid wafers that expand and contract as atmospheric pressure from the static source changes. This mechanical linkage translates the changes into pointer movements on the indicator.

    Types of Altitude

    • Indicated altitude: Altitude read directly from the altimeter.
    • Pressure altitude: Altitude when the barometric scale is adjusted to 29.92 inHg.
    • True altitude: Actual height above mean sea level.
    • Density Altitude: Pressure altitude corrected for non-standard temperature; determines airplane performance.
    • Absolute altitude: Actual height of an aircraft above the earth's surface.

    QNH, QNE, QFE

    • QNH: Local/station pressure.
    • QNE: Standard pressure.
    • QFE: Field elevation.

    Vertical Speed Indicator (VSI)

    • Indicates the rate at which the aircraft is climbing or descending in fpm.
    • Almost useless in turbulent conditions due to a lag of 6-9 seconds.

    Pitot-Static System Blockage

    • If the pitot tube is blocked: ASI reads high in a climb, low in a descent.
    • If the static port is blocked: ASI reads low in a climb, high in a descent; ALT freezes; VSI reads zero.

    Gyroscope

    • A rapidly spinning wheel with its weight concentrated about its rim.
    • Key characteristics:
      • Rigidity in space: The spinning wheel remains in a fixed position in the plane in which it is spinning.
      • Precession: Tilting or turning of a gyro in response to pressure; the gyro reacts to an applied force as though it was applied 90 degrees from the point of application in the direction of rotation.

    Vacuum (Suction) System

    • Engine-driven or electrically driven.
    • Controls a vacuum pump to create a partial vacuum in the system to supply rapid air to spin the gyros.
    • Monitored by the suction gauge.

    Attitude Indicator (AI)

    • Displays the actual attitude of the aircraft relative to the earth's horizon.
    • Often referred to as the "master instrument".

    Turn Coordinator (TC)

    • Indicates the rate and quality of a turn, and serves as an emergency source of bank information if the Attitude Indicator fails.
    • Combines 2 instruments: a miniature airplane and an inclinometer (ball).
    • Allows the pilot to maintain constant rate turns (standard rate turn: 3 degrees per second).
    • Provides no pitch information.
    • Modern version of the Turn and Slip Indicator.

    Skid and Slip

    • Skid: Rate of turn is too great for the angle of bank; ball is outside the turn; excessive rudder pressure.
    • Slip: Rate of turn is too slow for the angle of bank; ball is inside the turn; insufficient rudder pressure.

    Heading Indicator (HI)

    • Senses airplane movement and displays heading based on a 360-degree azimuth.
    • The final zero is omitted (e.g., 9 = 90 degrees; 27 = 270 degrees).
    • The HI can be set as the primary source of heading information.
    • Indirectly indicates bank.
    • Has no automatic north-seeking system.
    • Must be aligned with the magnetic compass every 15 minutes due to precession, during straight and level unaccelerated flight.

    Magnetic Compass

    • The only direction-seeking instrument in the airplane.
    • Primarily used to set the Heading Indicator before flight and to verify its continued accuracy during flight.
    • Readings are accurate only when the aircraft is in straight and level, unaccelerated flight.
    • The magnet on the compass aligns itself with the earth's magnetic fields.

    Compass Errors

    • Variation: Angular difference between the true and magnetic north.
    • Deviation: Difference between the indicated magnetic heading and the actual heading, due to other magnetic fields in the airplane.
    • Magnetic dip: Compass needle points down towards the magnetic pole (greatest at the poles, zero at the magnetic equator).
    • Acceleration errors: In the Northern Hemisphere, acceleration shows a turn to the north, deceleration shows a turn to the south. More pronounced on headings of east and west; no error when flying directly north or south. (ANDS - accelerate north, decelerate south)
    • Turning errors: Compass leads or lags the actual magnetic heading of the airplane during turns. In the Northern Hemisphere, a right turn from a heading of north will indicate a turn to the west, a left turn will indicate a turn to the east. Most pronounced when turning from headings of north or south. (UNOS - undershoot north, overshoot south)
    • Compass card oscillation: Erratic movement of the compass card caused by turbulence or rough control technique.

    Engine Instruments

    • Tachometer
    • Oil temperature gauge
    • Oil pressure gauge
    • Fuel quantity gauge
    • Fuel flow indicator
    • Exhaust gas temperature gauge
    • Manifold pressure gauge
    • Cylinder head temperature gauge

    Studying That Suits You

    Use AI to generate personalized quizzes and flashcards to suit your learning preferences.

    Quiz Team

    Related Documents

    Aircraft General Knowledge (Basic Aircraft Instruments) PDF

    Description

    This quiz covers the essential aircraft instruments, focusing on the Pitot-Static System and the Airspeed Indicator (ASI). Learn how these instruments enhance pilot performance and safety by utilizing air pressure differences to measure speed and altitude. Test your knowledge of how each instrument operates and its significance during flight.

    More Like This

    Use Quizgecko on...
    Browser
    Open
    Browser
    Browser