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Questions and Answers
What are the knowledge level indicators defined as in the context of Category A, B1, B2, and C Aircraft Maintenance Licence?
LEVEL 1, LEVEL 2, LEVEL 3
What is the main objective of LEVEL 1 knowledge?
In LEVEL 2 knowledge, applicants should be able to give a detailed description of the subject.
False
The applicant should understand and be able to use _ formulae related to the subject in LEVEL 3 knowledge.
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What are the four regions the atmosphere is classified into based on temperature variation with altitude?
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Which layer of the atmosphere contains all of the world's weather?
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The weight of the atmosphere on Earth's surface causes an air pressure of about _____ psi.
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Atmospheric pressure decreases with height above the Earth's surface.
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What does the International Standard Atmosphere (ISA) provide for aircraft and engine performance calculations?
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What are the main components of a pitot static system?
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Which instruments are part of the pitot static system?
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The pitot static system is used to measure only static pressure.
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What type of bellows is used in a manifold pressure gauge to reference measured pressure to a vacuum?
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Instrument sensing elements are not affected by temperature changes.
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What metals are bonded together in a bimetallic strip?
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The system of ports and tubing on the aircraft which supplies pitot and static pressure for the instruments is called the __________ system.
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What is the purpose of an altimeter in an aircraft?
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Which barometric code is used to set the altimeter reading to zero feet on landing and take-off?
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Airspeed equals ground speed in all flight conditions.
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An airspeed indicator provides information displayed in ________.
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Match the following airspeed indicator elements with their descriptions:
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What is the ratio of the aircraft's true airspeed (V) to the speed of sound (α) known as?
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What is the Mach number at which supersonic airflow first occurs on an aircraft?
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Maximum Operating Mach Number (Mmo) value is determined to avoid potential loss of control of a _____ aircraft.
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Match the following indicators with their correct descriptions:
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What will a partial blockage in the static line cause?
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What effect does a pitot tube blockage have on the airspeed indicator?
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Pitot line blockages have no effect on the altimeter or vertical speed indicator.
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In an unpressurised aircraft, a static leak may cause a standing error on the altimeter and airspeed indicator and has a minimal effect on the __________ indicator.
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Match the precautionary measure with its description:
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What are the three knowledge levels defined for Category A, B1, B2, and C Aircraft Maintenance Licence?
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What is the main objective of Level 1 knowledge?
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What is the main objective of Level 2 knowledge?
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What is the main objective of Level 3 knowledge?
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What are the three main instruments in a pitot static instrument system?
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Which component of the pitot static system measures the aircraft's speed through the air?
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The pitot tube measures static pressure.
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What are the regions of Earth's atmosphere classified based on?
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In which layer of the atmosphere do virtually all weather phenomena take place?
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The standard set of conditions used in aviation for performance calculations is known as the International Standard Atmosphere.
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The amount of pressure change the pitot static instruments are required to measure is in the region of only around _ psi overall.
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Match the pressure sensing device with its description:
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What type of bellows is a manifold pressure gauge typically using?
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What is the purpose of using bimetallic strips?
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A cold climate affects the malleability of an aneroid capsule used in instruments.
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The pressure-sensing element of an altimeter compensates for changes in ambient temperature with a bimetallic ______ bracket.
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Match the following atmospheric pressure measuring elements with their functions:
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What are the effects of a partial blockage in the static line?
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How does a pitot line blockage affect the airspeed indicator?
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A static line leak has no effect on the altimeter in a pressurized aircraft.
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How does reduced pressure in the altimeter case affect the aneroid capsules?
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Altimeters are calibrated to the standard atmosphere.
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What does the QFE code refer to?
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Indicated airspeed is measured in ______________.
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What is the Mach number defined as?
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What is the Critical Mach Number (Mcrit)?
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A Machmeter displays the Mach number indicated by the ratio V/α, where V is the aircraft's true airspeed and α is the speed of __________ at the aircraft's altitude.
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Vertical Speed Indicators (VSI) are designed to measure variations in static pressure to indicate the rate of altitude change.
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Study Notes
Category B1 Licence
- Relates to CASA B1-11f, covering Aeroplane Systems, including Instruments and Avionics
Knowledge Levels for Category A, B1, B2, and C Aircraft Maintenance Licences
- Knowledge levels are indicated by numbers (1, 2, or 3) against each applicable subject for categories A, B1, and B2
- Category C applicants must meet either the category B1 or category B2 basic knowledge levels
Level 1 Knowledge
- Familiarity with basic elements of the subject
- Ability to give a simple description of the subject using common words and examples
- Ability to use typical terms
Level 2 Knowledge
- General knowledge of theoretical and practical aspects of the subject
- Ability to apply knowledge
- Objectives:
- Understand theoretical fundamentals of the subject
- Give a general description of the subject using typical examples
- Use mathematical formulae in conjunction with physical laws
- Read and understand sketches, drawings, and schematics
- Apply knowledge in a practical manner using detailed procedures
Level 3 Knowledge
- Detailed knowledge of theoretical and practical aspects of the subject
- Capacity to combine and apply separate elements of knowledge in a logical and comprehensive manner
- Objectives:
- Know the theory of the subject and interrelationships with other subjects
- Give a detailed description of the subject using theoretical fundamentals and specific examples
- Understand and use mathematical formulae related to the subject
- Read, understand, and prepare sketches, simple drawings, and schematics
- Apply knowledge in a practical manner using manufacturer's instructions
- Interpret results from various sources and measurements, and apply corrective action where appropriate### Instrument Systems Pitot Static
- Pitot static systems measure air pressure to provide altitude, airspeed, and vertical speed data to pilots.
The Atmosphere and Atmospheric Standards
- The atmosphere is a layer of gases surrounding the Earth.
- Atmospheric pressure decreases with altitude.
- The atmosphere is divided into regions: troposphere, stratosphere, mesosphere, thermosphere, and exosphere.
- The standard atmosphere is a model used to standardize pressure, temperature, and density.
Pressure Sensing Devices
- Aneroid capsules and bellows are used to measure pressure changes.
- Bellows are flexible tubes that expand or contract with pressure changes.
- Temperature compensation is necessary to ensure accurate pressure readings.
- Bimetallic strips and temperature compensating U-shaped brackets are used for temperature compensation.
Pitot Static Systems
- Pitot probes measure impact pressure.
- Static ports measure static pressure.
- The difference between impact and static pressures gives airspeed.
- Pitot static systems are used in aircraft to provide altitude and airspeed data.
Altimeters
- Altimeters measure aircraft altitude.
- Non-sensitive altimeters measure altitude directly from static pressure.
- Sensitive altimeters measure altitude using a pressure-sensitive diaphragm.
- Barometric adjustment knobs are used to adjust for changes in atmospheric pressure.
Airspeed Indicator
- Airspeed indicators measure airspeed using pitot static pressure.
- Airspeed indicators have a pitot pressure inlet and a static pressure port.
- Maximum allowable airspeed indicators have a red line to indicate maximum safe speed.
Effects of System Blockages
- Static line blockage causes incorrect altitude readings.
- Pitot line blockage causes incorrect airspeed readings.
- System leaks can cause incorrect readings and instrument failure.
Pitot Static System Precautions
- Pitot probes must be kept clean and free of debris.
- Static ports must be kept clean and free of debris.
- System leaks must be checked regularly.
- Drain holes and water traps are used to prevent water from entering the system.### The Atmosphere and Atmospheric Standards
- Air is a mixture of gases in the following proportions:
- Nitrogen (78.08% by volume)
- Oxygen (20.95% by volume)
- Argon (0.93% by volume)
- Carbon dioxide (0.03% by volume)
- Other gases (0.01% by volume)
- The atmosphere consists of a layer of air many kilometers thick, with a weight that causes air pressure of about 14.7 psi at the earth's surface.
- Atmospheric pressure progressively reduces with height (altitude) above the earth.
Regions of the Atmosphere
- The atmosphere is classified into four regions based on the variation of temperature with altitude:
- Troposphere
- Stratosphere
- Mesosphere
- Thermosphere
- Aircraft fly only in the troposphere and the lowest part of the stratosphere.
Troposphere
- The troposphere is the lowest layer of the atmosphere, extending from sea level to the tropopause.
- All of the world's weather is contained in the troposphere.
- The temperature in the troposphere decreases rapidly with altitude, clouds form, and there may be much turbulence.
The Standard Atmosphere
- The standard atmosphere is a set of standard conditions with which observed readings can be compared.
- The standard atmosphere is also known as the International Standard Atmosphere (ISA) or ICAO Standard Atmosphere.
Pressure Sensing Devices
- Aneroid capsules:
- Measure very small changes in pressure with reference to a vacuum.
- Maximum operating range is 0 psia or a vacuum up to about 17 psia.
- Used to measure absolute pressure.
- Bellows:
- Operate similar to an aneroid capsule, but are generally not evacuated and are made of more rugged material.
- Used to measure high, low, or differential pressure.
Pitot Static Systems
- The pitot static system is a system of ports and tubing on the aircraft that supplies pitot and static pressure for the instruments.
- The pitot tube measures the ram pressure of the airstream.
- Static ports measure static pressure and are not affected by the speed of the aircraft.
Altimeters
- An altimeter measures the prevailing atmospheric pressure, which surrounds the aircraft, and displays this pressure in units of feet above sea level.
- Elements of an altimeter:
- Aneroid capsules or bellows
- Linkages and gears
- Instrument pointer
- Temperature compensation mechanisms
Category B1 Licence
- Relates to CASA B1-11f, covering Aeroplane Systems, including Instruments and Avionics
Knowledge Levels for Category A, B1, B2, and C Aircraft Maintenance Licences
- Knowledge levels are indicated by numbers (1, 2, or 3) against each applicable subject for categories A, B1, and B2
- Category C applicants must meet either the category B1 or category B2 basic knowledge levels
Level 1 Knowledge
- Familiarity with basic elements of the subject
- Ability to give a simple description of the subject using common words and examples
- Ability to use typical terms
Level 2 Knowledge
- General knowledge of theoretical and practical aspects of the subject
- Ability to apply knowledge
- Objectives:
- Understand theoretical fundamentals of the subject
- Give a general description of the subject using typical examples
- Use mathematical formulae in conjunction with physical laws
- Read and understand sketches, drawings, and schematics
- Apply knowledge in a practical manner using detailed procedures
Level 3 Knowledge
- Detailed knowledge of theoretical and practical aspects of the subject
- Capacity to combine and apply separate elements of knowledge in a logical and comprehensive manner
- Objectives:
- Know the theory of the subject and interrelationships with other subjects
- Give a detailed description of the subject using theoretical fundamentals and specific examples
- Understand and use mathematical formulae related to the subject
- Read, understand, and prepare sketches, simple drawings, and schematics
- Apply knowledge in a practical manner using manufacturer's instructions
- Interpret results from various sources and measurements, and apply corrective action where appropriate### Instrument Systems Pitot Static
- Pitot static systems measure air pressure to provide altitude, airspeed, and vertical speed data to pilots.
The Atmosphere and Atmospheric Standards
- The atmosphere is a layer of gases surrounding the Earth.
- Atmospheric pressure decreases with altitude.
- The atmosphere is divided into regions: troposphere, stratosphere, mesosphere, thermosphere, and exosphere.
- The standard atmosphere is a model used to standardize pressure, temperature, and density.
Pressure Sensing Devices
- Aneroid capsules and bellows are used to measure pressure changes.
- Bellows are flexible tubes that expand or contract with pressure changes.
- Temperature compensation is necessary to ensure accurate pressure readings.
- Bimetallic strips and temperature compensating U-shaped brackets are used for temperature compensation.
Pitot Static Systems
- Pitot probes measure impact pressure.
- Static ports measure static pressure.
- The difference between impact and static pressures gives airspeed.
- Pitot static systems are used in aircraft to provide altitude and airspeed data.
Altimeters
- Altimeters measure aircraft altitude.
- Non-sensitive altimeters measure altitude directly from static pressure.
- Sensitive altimeters measure altitude using a pressure-sensitive diaphragm.
- Barometric adjustment knobs are used to adjust for changes in atmospheric pressure.
Airspeed Indicator
- Airspeed indicators measure airspeed using pitot static pressure.
- Airspeed indicators have a pitot pressure inlet and a static pressure port.
- Maximum allowable airspeed indicators have a red line to indicate maximum safe speed.
Effects of System Blockages
- Static line blockage causes incorrect altitude readings.
- Pitot line blockage causes incorrect airspeed readings.
- System leaks can cause incorrect readings and instrument failure.
Pitot Static System Precautions
- Pitot probes must be kept clean and free of debris.
- Static ports must be kept clean and free of debris.
- System leaks must be checked regularly.
- Drain holes and water traps are used to prevent water from entering the system.### The Atmosphere and Atmospheric Standards
- Air is a mixture of gases in the following proportions:
- Nitrogen (78.08% by volume)
- Oxygen (20.95% by volume)
- Argon (0.93% by volume)
- Carbon dioxide (0.03% by volume)
- Other gases (0.01% by volume)
- The atmosphere consists of a layer of air many kilometers thick, with a weight that causes air pressure of about 14.7 psi at the earth's surface.
- Atmospheric pressure progressively reduces with height (altitude) above the earth.
Regions of the Atmosphere
- The atmosphere is classified into four regions based on the variation of temperature with altitude:
- Troposphere
- Stratosphere
- Mesosphere
- Thermosphere
- Aircraft fly only in the troposphere and the lowest part of the stratosphere.
Troposphere
- The troposphere is the lowest layer of the atmosphere, extending from sea level to the tropopause.
- All of the world's weather is contained in the troposphere.
- The temperature in the troposphere decreases rapidly with altitude, clouds form, and there may be much turbulence.
The Standard Atmosphere
- The standard atmosphere is a set of standard conditions with which observed readings can be compared.
- The standard atmosphere is also known as the International Standard Atmosphere (ISA) or ICAO Standard Atmosphere.
Pressure Sensing Devices
- Aneroid capsules:
- Measure very small changes in pressure with reference to a vacuum.
- Maximum operating range is 0 psia or a vacuum up to about 17 psia.
- Used to measure absolute pressure.
- Bellows:
- Operate similar to an aneroid capsule, but are generally not evacuated and are made of more rugged material.
- Used to measure high, low, or differential pressure.
Pitot Static Systems
- The pitot static system is a system of ports and tubing on the aircraft that supplies pitot and static pressure for the instruments.
- The pitot tube measures the ram pressure of the airstream.
- Static ports measure static pressure and are not affected by the speed of the aircraft.
Altimeters
- An altimeter measures the prevailing atmospheric pressure, which surrounds the aircraft, and displays this pressure in units of feet above sea level.
- Elements of an altimeter:
- Aneroid capsules or bellows
- Linkages and gears
- Instrument pointer
- Temperature compensation mechanisms
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Description
This quiz covers the aeroplane systems, including instruments and avionics, as part of the CASA Category B1 Licence. It's a comprehensive assessment of turbine aeroplane aerodynamics, structures, and systems.