ATPL(H): Understanding theory.

Your learning goal

Welcome to the subject Air Law of ATPL Helicopter Theory. You arrange legal sources, responsibilities, air spaces and clearances. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Correctly assigning sources of law

For a legal issue, you first need the right rule area. Part F C L deals with licenses and permissions. SERA contains common rules of the air. The operating rules depend, among other things, on whether a commercial or another company is present. The A I P publishes permanent aeronautical information, NOTAM report temporary changes. A textbook therefore does not replace the examination of the current publication. In exam tasks, you first clarify the state, type of operation, flight rules and aircraft category.

Licence, type and instrument flight

A passed ATPL theory exam is not yet an ATPL license. The exercise of an activity shall include the licence issued, appropriate ratings, the required medical certificate and other applicable requirements. For helicopters, type rating plays a central role. Instrument flight requires the necessary authorization. In addition, the curriculum versions ATPL H for visual flight and ATPL H with instrument flight differ. Which learning goals apply to your course, you clarify with your A T O.

Airspace and release

The airspace class, together with the flight rules, determines which services and requirements apply. A release is not a blanket permit for every maneuver. It shall have a content and, where appropriate, a limit. A radio contact alone does not yet mean an entry clearance. If you are uncertain, ask before crossing a border. Weather limits, obstacles, flight performance and responsibility do not disappear even with a release. Read tasks as a concrete situation, not as a collection of individual keywords.

Flight preparation as a legal application

Imagine a helicopter flight to an unknown landing site. A line on the map is not enough for preparation. Check the permitted use of the space, airspace restrictions, operating hours and current reports. Combine this information with weather, fuel planning and performance. Additional rules may apply to special types of operation. When you ask a question about minimum levels or reserves, you check the exact applicable rule instead of transferring a number from another operating area.

Case in point: Controlled airspace

You are approaching an airspace whose entry requires clearance. The pilot has confirmed your call sign, but has not yet given clearance. Are you allowed to fly in? This authorization does not follow from the mere radio contact. Keep a suitable, safe alternative outside and clarify the release in time. The learning principle is: actively test prerequisites. An expected radio message, an earlier flight and a navigation display do not replace the currently required clearance.

Learning Check and Next Step

Check your understanding. Is a passing theory exam already the license? No. Further requirements and the granting of the licence are required. Is radio contact automatically an entry clearance? No. The required release content must be available. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Is a passing theory exam already the license?

2. Is radio contact automatically an entry clearance?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• EASA: Standardised European Rules of the Air (SERA)
• EASA: Air Operations

Your learning goal

Welcome to the subject of helicopter science and systems of ATPL helicopter theory. You track the path from engine power via gearbox and rotor to the supporting systems. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Transmission and freewheeling

The engine delivers power, the transmission adapts speed and torque to the rotor system. In a conventional main rotor tail rotor configuration, the drive train drives both rotors. A freewheel makes it possible, under the conditions provided, for the rotor to rotate further without dragging along a failed engine. It does not produce energy itself. When learning, always check the relationship between power source, transmission, display and possible interference. Construction and boundaries are pattern-specific.

Rotor control

With the Collective you change the angle of adjustment of the main rotor blades together. This changes the power requirement. With the cyclic, the blade angle changes depending on the position in circulation; this controls the rotor force. Pedals affect yaw control, in many patterns via the tail rotor. The functions are coupled: a change to the collective may therefore require further corrections. Do not confuse blade angle, angle of attack and position of the rotor disk. They describe different sizes.

Turbine and engine control

In a shaft engine, the compressor compresses the air. Energy is supplied in the combustion chamber, and the turbines take work from the gas stream. In a free-turbine design, the gas generator and the power turbine are mechanically separated. Electronic control can monitor and control engine functions. This does not mean that every limit value is automatically adhered to under all conditions. Speeds, temperature and torque must be interpreted correctly. Start and fault procedure you learn from the concrete sample manual.

Hydraulics, Electrics and Fuel

The hydraulics can support control forces. A failure has a different effect depending on the pattern. In electrical systems, normal supply, replacement supply and their time limits differ. In the case of fuel systems, sufficient fuel in the tank is not equivalent to an undisturbed supply to the engine. Pumps, valves, ventilation and pipes are part of the functional chain. When learning, draw the energy source, the consumer and the replacement path. So you understand a fault better than with isolated component names.

Case study: indication and cause

An oil pressure warning device shall appear. You cannot readily infer a single mechanical defect. Sensor, supply, display and actual system state form a chain. At the same time, you must not dismiss a warning as a sensor error without proof. The correct procedure depends on the flight manual and the checklist. For theory tasks, you first assign the affected function and check which other information supports an explanation. A diagnosis does not replace a prescribed action.

Learning Check and Next Step

Check your understanding. Does the freewheel generate drive power? No. It enables decoupling in the drive train. What is changing the collective together? The angle of adjustment of the main rotor blades. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Does the freewheel generate drive power?

2. What is changing the collective together?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• FAA: Helicopter Flying Handbook – technical addition, no EU legal reference

Your learning goal

Welcome to instrumentation of ATPL helicopter theory. You differentiate between metric, display, source of error and automation mode. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Static pressure and total pressure

The barometric altimeter uses static pressure. The tachometer derives its indication from the difference between total pressure and static pressure. The classic variometer responds to changes in static pressure over time. A blocked connection therefore affects several displays in different ways. The exact malfunction depends on which connection is blocked and whether enclosed pressure is maintained. Learn the measurement chain, instead of claiming that every instrument shows the same error when blocked.

IAS, TAS and Height terms

The displayed speed is not equal to the true speed through the air under all conditions. Instrument and installation errors, compressibility and air density play different roles in the conversions. The speed above ground additionally depends on the wind. In the altimeter, the pressure setting changes the reference value. Pressure altitude, indicated altitude and true altitude must therefore be distinguished. Cold air can lead to a lower true altitude than a simplified view of the display would suggest.

Gyroscopes and electronic sensors

Mechanical gyros and electronic inertial sensors provide information about movement and position. However, a situational picture is only as reliable as its database and processing. Check alignment, supply, validation indicators and compliance with independent information. A conclusive-looking screen is not yet proof of correct values. In addition, distinguish the displayed attitude from the flight path: a helicopter can climb, sink or move in different directions if the fuselage is similar.

Autopilot and Flight Director

The flight director shows control commands; an autopilot can perform corresponding control tasks. The decisive factor is which mode is actually active and which goals are preselected. A preselected value is not automatically a captured mode. After input, check the mode display, response and trajectory. In the case of helicopters, stabilization and flight guidance functions may be differently designed. A general description therefore does not provide an operating sequence for a particular pattern.

Case in point: wind instead of instrument error

A learning example: The true speed is one hundred twenty knots. A direct headwind of twenty knots acts along the flight direction. Under these simplified conditions, the velocity over ground is one hundred knots. A difference between air speed and satellite display is expected here. It does not prove instrumental error. In crosswind, you have to consider the wind triangle. In each task, first identify the speed and its reference before comparing readings.

Learning Check and Next Step

Check your understanding. Does the Flight Director alone display automatic control? No. It can display control commands without automatically executing them. Is the velocity over ground equal to the TA? Only under suitable conditions; wind can clearly distinguish both. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Does the Flight Director alone display automatic control?

2. Is the velocity over ground equal to the TA?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• FAA: Instrument Flying Handbook – Technical Supplement

Your learning goal

Welcome to the subject mass and focus of ATPL helicopter theory. You calculate moments and center of gravity and check the load over the entire flight. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Mass, Arm and Moment

The mass moment of a charge is its mass times lever arm to a fixed reference point. This reference point is the date of the model. All values must relate to this. Arms can be positive or negative, depending on the definition. Kilogram times meter is a different number than kilogram times centimeter. Confusion generates a large computation error. If the manual uses a moment index, you need the scaling factor set there. Only then do you compare results.

Calculate the total centre of gravity

The total center of gravity is the sum of the moments divided by the total mass. It is a weighted average, not a simple average of all seating positions. A heavy charge is stronger than a light one. You then check whether the mass and center of gravity are within the allowed range. In the case of a helicopter, in addition to the longitudinal direction, the lateral loading can also be significant. Boundaries can change with mass and configuration. The valid loading plan is therefore part of the task.

Fuel and phases

During the flight, the fuel mass decreases. If the tanks are not exactly in the overall center of gravity, this also changes the center of gravity. Additional changes occur due to movement of persons or the settling of a load. Therefore, a permissible take-off load does not automatically guarantee a permissible condition on landing. Calculate the required flight phases individually. Differentiate dry matter, dry operating mass and other terms based on their definition in the task; names from different documents are not arbitrarily interchangeable.

Why the border is important

An impermissible center of gravity position may exceed required control paths and control reserves. The fact that a helicopter remains below the maximum mass is therefore not sufficient. Conversely, a permissible center of gravity does not make an excessively high mass permissible. The available flight performance can also limit the usable mass more than the maximum structural mass. Check the conditions separately and then link them to a decision. A positive response in one of the exams does not compensate for a negative response in the other.

Calculating Example: Weighted Average

A simplified example contains a basic mass of one thousand kilograms on the arm two meters and a payload of two hundred kilograms on the arm three meters. The moments are two thousand and six hundred kilogram meters. Together, twelve hundred kilograms and two thousand six hundred kilometres result. The center of gravity is thus around two comma one six seven meters. This is a calculation result, not yet a release. Only the comparison with the valid center of gravity diagram shows whether the state would be permissible.

Learning Check and Next Step

Check your understanding. How do you calculate the focus? Total torque divided by total mass. Does the take-off load prove a landing load? No. Fuel consumption or load changes can change the center of gravity. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. How do you calculate the focus?

2. Does the take-off load prove a landing load?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• FAA: Helicopter Flying Handbook – technical addition, no EU legal reference

Your learning goal

Welcome to the subject of flight planning and flight monitoring of ATPL helicopter theory. You connect route, time, fuel, weather and ongoing air traffic control. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

From task to flight plan

A flight planning starts with the assignment and the available possibilities. Route, weather, airspace and landing opportunities affect each other. A short path is not automatically the best route. Check obstacles, achievable alternatives and helicopter performance. Planning does not end with the entry of a flight plan. It shall demonstrate that the flight remains feasible under the applicable conditions. Therefore, set verifiable decision points before time pressure and workload increase in the cockpit.

Time from distance and speed

The flight time of a section is derived from distance divided by speed over ground. At nautical miles and knots, you get hours. Multiply by sixty when minutes are asked. Do not use unchecked the indicated or true air speed. Climbing, descent, wind changes and additional routes can change the actual time. In a multi-part route, you calculate the sections according to their conditions and then add the times. A single average number can mask important differences.

Sensibly divide fuel

The fuel needed for the route is only part of the planning. In addition, there are the components required according to the operating mode and regulation and, if necessary, further surcharges. Therefore, do not use a universal reserve number for each helicopter flight. Quantity, mass and volume are also different: the appropriate density is required for a conversion. Non-usable fuel is not an available reserve. Specify the minimum quantity at a checkpoint and the decision that follows if it is undershot.

Examine the assumptions on the way

Air traffic control means comparing the original planning with the actual development. Check position, past time, weather, consumption and remaining fuel. A longer flight time may necessitate an earlier evasion decision. A new arrival time alone does not solve the fuel problem. Use reliable measurements and operationally prescribed procedures. Good planning already contains criteria for continuing, rescheduling or cancelling. So you do not have to invent a fundamental decision first under unfavorable conditions.

Calculating example: section and consumption

A distance is sixty nautical miles long, the speed above ground is one hundred and twenty knots. This is followed by half an hour or thirty minutes. With an assumed constant consumption of two hundred and forty kilograms per hour, this section requires one hundred and twenty kilograms. This value does not include any additional planning elements. If the speed drops above ground, time and section consumption increase with unchanged hourly consumption. Therefore, always separate the calculation task for a section from the complete fuel proof for the flight.

Learning Check and Next Step

Check your understanding. What speed is included in the route timetable? The speed over ground. Is the calculated trip demand already the total fuel required? No. The applicable additional components must be added. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. What speed is included in the route timetable?

2. Is the calculated trip demand already the total fuel required?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• EASA: Air Operations

Your learning goal

Welcome to the subject of flight performance helicopters of ATPL helicopter theory. You differentiate between power requirements, available power and the performance limits when hovering and starting. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Performance needs and supply

For a flight condition, the helicopter needs a certain performance. The amount of power available depends, among other things, on the engine, environmental conditions and permissible limits. A surplus can be used for acceleration or rising. Nominal engine power is not automatically usable in every state: transmission, temperature or torque limits can be reached earlier. Power curves must therefore be read under the correct conditions. Always check mass, pressure altitude, temperature and the configuration mentioned in the diagram.

Floating inside and outside the ground effect

Ground proximity changes the rotor flow field. Under suitable conditions, floating in the ground effect requires less induced power than outside. Therefore, proof of floating in the ground effect does not prove sufficient performance outside. The actual effect depends on the ground, height and other conditions. Use the expressly appropriate table. A seemingly successful short hover sequence at the starting point is no substitute for a performance calculation at the later location.

Density height and mass

Low air density typically deteriorates the rotor power and can also affect the available engine power. High temperature and low air density are therefore particularly important for helicopter operations. A higher mass increases the required rotor thrust and the power requirement. The combination can limit the levitation. Do not confuse pressure altitude and density altitude: The diagram may require pressure altitude and temperature separately. Enter exactly the required input variables and do not extrapolate outside the permitted range.

Take-off, obstacles and engine failure

A secure proof of performance takes more into account than the withdrawal. This includes take-off distance, obstacles and applicable engine failure requirements. In the case of multi-engine helicopters, the single-engine case describes its own performance consideration. The categories of the approved type and the operational performance classes are different terms. They must not be equated. Whether a take-off profile is permissible and suitable follows from the specific flight manual and the operating rules. This schematic video does not provide a general starting technique for this.

Calculating Example: Recognizing Reserve

Suppose under a defined condition five hundred kilowatts are available and the considered flight state requires four hundred and sixty kilowatts. The difference is forty kilowatts. This is only a computational power difference for this condition. It proves neither a concrete climb rate nor a permissible start. If the mass, temperature, rotor condition or a limiting component change, the calculation does not continue unchanged. For the conversion into flight performance you need the appropriate approved data.

Learning Check and Next Step

Check your understanding. Does IGE hoverability prove OGE hoverability? No. Outside of the ground effect, more power may be needed. Can you extrapolate a performance diagram as you wish? No. Use the permitted data within their premises. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Does IGE hoverability prove OGE hoverability?

2. Can you extrapolate a performance diagram as you wish?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• EASA: Air Operations
• FAA: Helicopter Flying Handbook – technical addition, no EU legal reference

Your learning goal

Welcome to the Human Performance of ATPL Helicopter Theory. You learn limits of perception and strategies for attention, collaboration and decision-making. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Perception and spatial orientation

The equilibrium organ does not recognize every movement as an instrument describes it. Especially without good external vision, accelerations and rotations can create misleading impressions. A strong feeling is then not a reliable proof of the situation. The approved instrument flight procedures and the training required for them provide a systematic reference. Even in visual flight, uniform surfaces, water or darkness can make orientation difficult. Therefore, plan the flight so that the necessary visual or instrumental references are actually available.

Attention and workload

Perceiving multiple ads at the same time does not mean completely processing all information at the same time. High workload can narrow the eye and displace important clues. If the crew distributes tasks clearly, the available attention can be used better. Standardized processes and timely preparation reduce search work. As the burden increases, priorities must be actively redefined. A complicated side problem must not replace the control of the flight path. Agreed distribution of tasks and mutual monitoring therefore belong in the briefing.

Fatigue and performance

Fatigue can interfere with response, attention and judgment. The subjective assessment of one’s own performance is not always reliable. Caffeine does not replace adequate recovery. Working hours, sleep quality and time of day should be considered together. The operational and medical requirements apply to the operational decision. The learning goal is not self-diagnosis, but the recognition of a risk factor and a responsible handling of it. Address restrictions early, before time pressure becomes a barely correctable process.

Decision errors and CRM

Those who expect a plan often perceive suitable information more easily than contradictory ones. Time pressure and already invested effort can increase the adherence to an unfavorable project. Crew Resource Management helps to bring in information and doubt clearly. A factual query can make a false assumption visible early on. What is important is the confirmed distribution of tasks, a common situational picture and an understandable decision. An individual pilot can also use available resources, such as air traffic services and early prepared fallback planning.

Case in point: Planning continuation error

The target is only a few minutes away. Visibility and cloud position deteriorate, while someone is already waiting for arrival on the ground. This expectation does not change the minimum conditions or one’s own abilities. A pre-agreed decision point makes it easier to implement a secure alternative. Formulate the situation concretely: Which prerequisite is missing, which alternative remains and how long is it available? The proximity to the target is a psychological pressure factor, not proof of a safely feasible approach.

Learning Check and Next Step

Check your understanding. Is a convincing movement impression always right? No. Sensory impressions can deceive. Why do predefined decision points help? They facilitate timely decisions under pressure. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Is a convincing movement impression always right?

2. Why do predefined decision points help?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• FAA: Helicopter Flying Handbook – technical addition, no EU legal reference

Your learning goal

Welcome to the subject Meteorology of ATPL Helicopter Theory. You combine weather reports with clouds, wind, icing and the special risks of a helicopter flight. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Atmospheric pressure, temperature and humidity

Atmospheric pressure, temperature and humidity describe different properties of the atmosphere. If moist air is sufficiently cooled, saturation can be achieved and condensation can begin. A small distance between temperature and dew point is an indication of possible near-saturation, but not a complete cloud forecast. Increasing, mixing and moisture supply change the development. Therefore, combine ground observations with weather conditions and information along the route. Weather learning means understanding causes and spatial distribution, not memorizing individual abbreviations in isolation.

Wind and land

Wind arises from pressure differences and is influenced by further forces and friction. In the vicinity of the ground, the actual flow can be strongly influenced by terrain and obstacles. Behind an obstacle, turbulent areas can arise, on slopes also strong up and down winds. Therefore, a wind value of a distant airfield does not automatically describe a mountain landing site. Differentiate medium wind, gusts and local current. The performance of the helicopter shall be sufficient under the conditions actually expected.

Fronts, thunderstorms and ice

Fronts mark transitions between different air masses. Clouds, precipitation and wind changes depend on the specific location. Thunderstorms combine hazards such as strong vertical movement, turbulence, hail and electrical activity. Icing can affect rotor blades, inlets and instrumentation systems. A heating device on a single component does not imply general approval for icing conditions. Check the approval of the type and operational limits. In addition, a weather display in the cockpit only shows what the sensor, data source and transmission path actually capture.

METAR, TAF and other products

A METAR describes an aerodrome observation, a TAF a time-structured forecast for an aerodrome. Both do not replace a complete assessment of the weather along the route. Validity period, date of issue and expected changes must fit the scheduled flight time. For significant dangers, you use the appropriate other products. Even a correct message cannot guarantee a later or spatially distant state. Compare the expected situation on the road with the actual development and keep alternatives achievable.

Case study: aerodrome report and operating site

Good visibility shall be reported at the departure aerodrome. Your goal lies in a valley where humid air and shadowing favor a different development. The good start report does not provide a guaranteed view at the destination. Check out appropriate regional and up-to-date information, the course of the route and your alternatives. The crucial question is not whether any report shows good conditions. The decisive factor is whether the expected conditions at the required location and time match the planned flight.

Learning Check and Next Step

Check your understanding. Is a METAR a route forecast? No. It's an airfield observation. Does a single heater prove an icing permit? No. Approval and limits of the entire model are crucial. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Is a METAR a route forecast?

2. Does a single heater prove an icing permit?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• FAA: Aviation Weather Handbook – meteorological supplement

Your learning goal

Welcome to General Navigation of ATPL Helicopter Theory. You distinguish directional references, course, steering course and wind correction. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Position and map

A position on Earth can be described with geographical latitude and longitude. Maps represent the curved surface of the earth on a plane. Each projection has properties and distortions that are important for the respective usage. Before a calculation, you clarify the scale, coordinate system and required accuracy. Don’t just measure a distance in centimeters and treat the value as nautical miles. Use the appropriate scale and check if the map is suitable for the task and current.

Righteous, Missing and Compass

Direction indications can refer to geographically North, magnetically North or the compass actually read. Misrepresentation and deviation are different corrections. A secure invoice identifies each intermediate step with its reference. For example, don’t just write a number with degree signs, but complement the directional reference. Wind indications and map courses must also be brought together appropriately. Many errors are not caused by difficult mathematics, but by combining two correctly determined values with different references unchecked.

Track, Heading and Wind Triangle

The track describes the direction of movement over ground. The heading is the direction in which the longitudinal axis points. In crosswinds, both are usually different. The wind vector combines the velocity through the air with the velocity above ground. In order to maintain a desired track, a suitable wind correction is required. Headwind changes the flight time, crosswind can additionally demand a course correction. Use the speed reference provided for the wind triangle and the same north reference for all directions.

Check the coupling and position

Coupling means deriving a new position from a known position and the movement assumptions. Uncertainties in wind, time or speed grow with the distance. Therefore, the invoice needs regular checking by suitable position information. A striking terrain feature, radio navigation or satellite data can help if their limits are observed. A single clue should plausibly fit into the overall picture. An expected position must not tempt you to interpret an inappropriate terrain sign.

Calculating example: distance from time

In a simplified example, you fly ninety knots above the ground and look at twenty minutes. Twenty minutes is a third of an hour. Ninety nautical miles per hour times a third of an hour is thirty nautical miles. The units can be shortened in a comprehensible manner. If you use the true air speed instead, the result without looking at the wind is not necessarily the ground distance. Therefore, start with the units and the reference, only then with the multiplication.

Learning Check and Next Step

Check your understanding. Do the heading and track have to be identical? No. Crosswinds may require wind correction. Are rejection and deviation the same correction? No. They describe different directional deviations. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Do the heading and track have to be identical?

2. Are rejection and deviation the same correction?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• FAA: Instrument Flying Handbook – Technical Supplement

Your learning goal

Welcome to the subject of radio navigation of ATPL helicopter theory. You understand the basic principles of VOR, DME, ILS and satellite navigation and their limitations. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Spread and range

Radio navigation systems use different frequencies and measurement principles. In many systems in the higher frequency range, the usable connection is highly dependent on the line of sight. Terrain can shadow signals; reflections can cause additional errors. A large nominal range therefore does not guarantee reception in a valley. Check identification, operational status and intended terms of use. The display of a plausible value is not sufficient if a warning or the identifier speaks against use.

VOR and DME

A VOR radial describes a magnetic direction from the station to the outside. This is not automatically your heading to the station. The course display must be interpreted correctly with TO FROM Information and selected course. D M E measures the oblique distance, not directly the horizontal map distance. Particularly close above the station is the height proportion. Therefore, combine measurement principle and geometry. An advertisement can be technically correct and still be misunderstood.

ILS and ad logic

An instrument landing system shall provide lateral and vertical guidance information under intended conditions. Localizer and Glideslope are different signal components. A central display does not alone prove that every requirement for the approach is met. Identification, validity indication, published procedures and the correct position are included. Also note the different display logics of instruments and operating modes. This basic principle explains the system; the safe conduct of an instrument approach requires appropriate training, rating and a concrete procedure.

GNSS, RNAV and integrity

Satellite navigation determines a position from propagation time information of several signals and further data. For operation, not only an instantaneously accurate position indication is sufficient. Integrity concerns the ability to warn in good time about undue errors. Availability, continuity, approval and database status are other important aspects. RNAV and power-based navigation describe more than a single satellite device. Interference or deception can affect information. Compare anomalies with independent sources and use the procedures foreseen.

Computational example: DME above the station

In a simplified geometric example, you are directly above a D M E station. The height difference is about six thousand seventy-six feet, so a nautical mile. The horizontal distance is almost zero, the oblique distance displayed is approximately one nautical mile. That is not a contradiction. The greater the horizontal distance relative to the height difference, the smaller this relative difference is. For exact tasks, use the specified units and the appropriate rectangular geometry.

Learning Check and Next Step

Check your understanding. Is a VOR-Radial automatically the heading to the station? No. It is a direction from the station to the outside. Does DME measure horizontal card distance? No. It measures the oblique distance. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Is a VOR-Radial automatically the heading to the station?

2. Does DME measure horizontal card distance?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• FAA: Instrument Flying Handbook – Technical Supplement

Your learning goal

Welcome to the subject of operating procedures of ATPL helicopter theory. You combine briefing, standard procedures and risk assessment with the helicopter operation. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Standard procedures and briefing

Standard procedures create a common process. A briefing supplements them with the specific situation: weather, performance limits, obstacles, distribution of tasks and alternatives. It is not enough to read a long list quickly. The parties involved must have the same situational picture and clear thresholds for action. If an important condition changes, the plan is re-evaluated. During a helicopter operation, landing area, people and obstacles can change in the short term. The briefing must therefore remain connected with the actual situation.

Rotor area and ground operation

Ground operations contain special hazards due to rotating rotors, downwind, noise and limited communication. Persons may approach only in accordance with the applicable procedures and the intended briefing. A general rule from another pattern does not replace this instruction. Loose objects can be stirred up. Slopes and changing leaf freedom change the situation additionally. The safe organization of the area begins before starting. Check who takes control of people, materials and access to the helicopter.

Dust, Snow and Visual References

Rotor downwind can whirl dust or snow and abruptly deteriorate external references. A flat, bright surface can make orientation even more difficult. Performance alone makes a landing site then not suitable. Prior to approach, consideration shall be given to the environment, visibility and procedures foreseen. An improvised continuation of lost references can exacerbate the situation. This video explains the risk; the required operational techniques must be taught in the appropriate training and operational framework on the model.

Incidents and emergency procedures

In the event of a disruption, clear priorities and practiced procedures help. The immediate actions to be performed depend on the pattern and the actual disturbance. Do not invent memory actions from a general system explanation. After the immediate measures envisaged, further steps are checked on the appropriate checklist. Coordination of occupation reduces omitted or duplicate actions. In addition, a warning signal alone does not say that any emergency landing area is reachable or suitable. Location, flight performance and environment remain part of the decision.

Case in point: Landing site decision

A performance diagram shows mathematically sufficient reserves for a landing site. On site, however, there are unprotected persons and loose objects in the area of influence of the rotor downwind. Can the positive performance invoice determine the decision alone? No. The operation must also be feasible under the other safety and operational conditions. Clear the organization on the ground and a suitable alternative. The example shows: A technical proof is important, but does not automatically cover all risks of the specific use.

Learning Check and Next Step

Check your understanding. Does a general statement replace the model emergency procedure? No. Relevant are the valid procedures and checklists of the model. Is sufficient performance for a suitable landing site? No. Environment and other operational requirements must also fit. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Does a general statement replace the model emergency procedure?

2. Is sufficient performance for a suitable landing site?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• EASA: Air Operations
• FAA: Helicopter Flying Handbook – technical addition, no EU legal reference

Your learning goal

Welcome to the subject Aerodynamics of the helicopter ATPL Helicopter theory. You understand rotor forces, blade movement, forward flight and the basics of autorotation. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Rotor blade and angle of attack

rotor blade is a moving support profile. Its velocity and the inflowing air give the local direction of flow. The angle of adjustment describes a geometric position of the blade, and the angle of incidence describes the angle with respect to the local inflow. Both are therefore not identical. Along the sheet and over the circulation, conditions change. More adjustment angles do not mean any more usable lift under all circumstances. Flow separation and performance limits must be taken into account. You can understand the rotor thrust as a result of the distributed blade forces.

Torque and control

If the main rotor is driven, a corresponding reaction moment acts on the fuselage. In the usual configuration, the tail rotor compensates for this torque and enables yaw control. Other helicopter concepts solve this differently. If the required main rotor torque changes, the necessary counteraction also changes. At the same time, the lateral force of the tail rotor and the position of the rotor force may require further compensation reactions. Therefore, consider the forces and moments together. A single control movement rarely has only an isolated effect.

Forward flight and lift distribution

In forward flight, the local inflow velocity of a leading blade is different from that of a returning blade. Blade movement and cyclic control contribute to the distribution of forces. At high speeds, large angles of incidence and flow separation can become relevant on the returning side. On the leading side, high local speeds can cause other limits. These relationships explain why a helicopter does not reach an arbitrarily high forward speed. The valid speed limits are taken from the specific flight manual.

Vortex ring state and rotor energy

With certain combinations of low forward speed, descending movement and power, the rotor can come into an unfavorable state in its own track. Such a vortex ring state is not simply synonymous with every rapid sinking. Rotor loading and the available control effect are decisive. Low rotor speed is in turn a dangerous situation of its own: the stored rotational energy is limited. Generalized discharge recipes are unsuitable. Recognition, avoidance and reaction must be learned from the training and procedures of the respective pattern.

Understanding Autorotation

In the autorotation, the air flow through the rotor maintains its rotation. Different blade regions contribute to the torque in a driving or braking manner. The state is therefore not a consequence of an additional engine energy from the freewheel. Descent, forward movement and stored rotor energy form a limited energy balance. The necessary speeds, speeds and actions are pattern-specific. The theoretical understanding explains why rotor energy needs to be monitored; it does not replace practical autorotation training with a qualified flight instructor.

Learning Check and Next Step

Check your understanding. Are angles of incidence and angles of incidence identical? No. The angle of incidence relates to the local inflow. Where does the driving effect come from in autorotation? From the air flow through the rotor, within a limited energy balance. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Are angles of incidence and angles of incidence identical?

2. Where does the driving effect come from in autorotation?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• FAA: Helicopter Flying Handbook – technical addition, no EU legal reference

Your learning goal

Welcome to the subject Communication of ATPL Helicopter Theory. You practice clear messages, closed feedback and the correct classification of urgency. This video gives you a compact introduction and helps with repetition. The schematic representations and calculation values are learning examples. They do not replace the full curriculum of your training organization or an aeroplane manual. Stop briefly for a task and explain the connection with your own words.

Radio as a closed sequence

An effective radio link consists of more than sending a message. The right recipient must understand it and essential content must be confirmed. First, listen, organize your content and send in an understandable way. Call signs and standardized speech groups facilitate the assignment. Avoid unnecessary filler words, but do not omit crucial information. A message will remain incomplete if you do not notice that it has been misunderstood. Therefore, check the answer and correct any recognizable misunderstandings immediately.

Readback and Hearback

Reading back safety-relevant releases makes transmission and understanding errors recognizable. The receiving page must also check the read-back content. A quick Roger does not replace every prescribed repetition. Which contents are to be read back is determined by the applicable rules and procedures. If you have an unclear altitude or direction, ask. A plausible value is not a reliable basis if you have not clearly understood the actual statement.

Numbers, voice and frequency changes

Number rotators can change highs, rates or frequencies. Therefore, use the prescribed pronunciation and the appropriate standard phraseology. A frequency change involves the correct input and control of whether the new connection has come about. A radio can be set correctly, while audio source, volume or dial button are misconfigured. The entire communication chain must work. In special situations, plaintext helps in addition to standard phraseology if standardized speech groups do not sufficiently describe the facts.

Urgency and urgency

Emergency and emergency traffic differ in the nature and severity of the situation. An emergency concerns a serious and immediate danger and requires immediate assistance. An urgency notification concerns security without this emergency situation. The message is intended to convey the identity, nature of the problem, position and intention under the circumstances. However, radio organisation must not displace the necessary guidance of the helicopter. You learn the concrete handling with the applicable radio rules and realistic training exercises.

Case in point: Incorrectly read back height

In a training example, a height is released but read back with a different number. The conversation must not be considered as successfully concluded. The deviation must be corrected and the correct instruction clearly confirmed. In the cockpit, both crew members should also have relevant clearances in the common situational picture where possible. The learning goal is the closed communication loop. Sending, receiving correctly, reporting back and checking belong together. Speed in the radio is not a substitute for clearly understood content.

Learning Check and Next Step

Check your understanding. Does Roger replace every necessary read-back? No. Prescribed content must be read back appropriately. What must happen in the event of a detected readback deviation? The derogation must be explicitly clarified and corrected. The questions are self-created. Repeat unclear chapters and deepen the subject with the learning goals of your training organization. Sources, chapter marks and the full speaker text can be found under the video.

1. Does Roger replace every necessary read-back?

2. What must happen in the event of a detected readback deviation?

• EASA: European questionnaire and current curriculum basis
• EASA: Aircrew / Part-FCL and learning objectives
• EASA: Standardised European Rules of the Air (SERA)