ASX Glossary - S: Difference between revisions

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        <a href="https://wiki.alsresume.com/index.php?title=Area_51" target="_blank"
          style="color: #00ff01; font-weight: bold; text-decoration: none; cursor: pointer;"
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          R-4808 N/Area 51/Groom Lake
        </a>
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    <td class="description">
        <span style="color: #00ff01; font-weight: bold; text-decoration: none; cursor: pointer;"
              onmouseover="this.style.color='#ff4f01';"
              onmouseout="this.style.color='#00ff01';"
              onclick="window.open('https://www.google.com/maps/@37.2815,-115.805667,15z/data=!3m1!1e3', '_blank')">
              Area 51/Groom Lake
        </span> is a highly classified U.S. Air Force facility located in southern Nevada, officially known as Homey Airport or Groom Lake. Established in 1955 for testing the Lockheed U-2 aircraft, its operations remain secretive, fueling numerous UFO conspiracy theories. The CIA publicly acknowledged its existence in 2013. Situated 83 miles northwest of Las Vegas, the area attracts tourists, especially to the nearby town of Rachel on the "Extraterrestrial Highway."
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    <td class="image-column">
        <img src="https://www.alsresume.com/wp-content/uploads/2025/03/Area-51.jpg" alt="Area 51/Groom Lake/R-4808 N">
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    <td class="term">
        <a href="https://wiki.alsresume.com/index.php?title=Radar_altimeter" target="_blank"
          style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"
          onmouseover="this.style.color='#ff4f01';"
          onmouseout="this.style.color='#40E0D0';">Radar Altimeter</a>
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    <td class="description">A radar altimeter measures an aircraft's altitude above ground level using radio waves. It provides precise altitude readings during landing approaches and low-altitude operations. Essential for terrain awareness and automated landing systems, radar altimeters enhance safety by helping pilots maintain proper clearance from obstacles.</td>
    <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Radar-Altimeter.jpg" alt="Radar Altimeter"></td>
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     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Radar_Vectoring" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Safe_Life_(Aircraft_Design_Principle)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
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           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Radar Vectoring</a>
           onmouseout="this.style.color='#40E0D0';">Safe Life (Aircraft Design Principle)</a>
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     <td class="description">Radar vectoring is a navigation technique where air traffic controllers provide headings to pilots using radar. It is used for traffic sequencing, avoiding weather, or guiding aircraft during approaches. Pilots rely on radar vectoring to maintain situational awareness and ensure safe separation.</td>
     <td class="description">Safe life is an engineering principle ensuring that an aircraft component will function safely for a predetermined lifespan before requiring mandatory replacement. Components designed under this philosophy are monitored for fatigue and wear, preventing failures through strict maintenance schedules, particularly in critical structures like landing gear and wings.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Radar-Vector.jpg" alt="Radar Vectoring"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Safe-Life.jpg" alt="Safe Life"></td>
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         <a href="https://wiki.alsresume.com/index.php?title=Radio_beacon" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Satellite_navigation" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
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           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Radio Beacon</a>
           onmouseout="this.style.color='#40E0D0';">Satellite Navigation (SatNav)</a>
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     <td class="description">A radio beacon is a ground-based transmitter that emits signals to guide aircraft. Used in non-directional navigation systems, pilots locate and fly towards or away from beacons to maintain course. They are critical for navigation, especially in areas with limited GPS coverage.</td>
     <td class="description">Satellite navigation, or SatNav, is a global positioning system used in aviation for precise flight planning and real-time navigation. It improves situational awareness, enhances safety, and allows for accurate approaches, particularly in GPS-based landing systems, replacing traditional ground-based navigation aids in many modern aircraft.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Radio-Beacon.jpg" alt="Radio Beacon"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Satellite-NAv.jpg" alt="Satellite Navigation"></td>
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         <a href="https://wiki.alsresume.com/index.php?title=Radio_Communication_Failure" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Scalloping_(Aerodynamics)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Radio Communication Failure</a>
           onmouseout="this.style.color='#40E0D0';">Scalloping (Aerodynamics)</a>
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     <td class="description">A radio communication failure occurs when an aircraft loses the ability to transmit or receive messages. Pilots follow standard procedures, including squawking transponder code 7600, to alert air traffic control and follow pre-established routes to ensure safe operation.</td>
     <td class="description">Scalloping refers to the aerodynamic phenomenon where sections of an aircraft surface, such as propeller blades or wings, develop a wavy pattern due to pressure differentials. This can cause structural stress, reduce efficiency, and impact lift characteristics, necessitating precise engineering to mitigate its effects.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Radio-Communication-Failure.jpg" alt="Radio Communication Failure"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Scalloping.jpg
" alt="Scalloping"></td>
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         <a href="https://wiki.alsresume.com/index.php?title=Ramp_Check" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Scramjet" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Ramp Check</a>
           onmouseout="this.style.color='#40E0D0';">Scramjet (Supersonic Combustion Ramjet)</a>
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     <td class="description">A ramp check is an inspection conducted by aviation authorities to ensure compliance with regulations. It involves checking aircraft documents, equipment, and crew certifications. Pilots and operators must cooperate fully to avoid penalties or grounding of the aircraft.</td>
     <td class="description">A scramjet is an advanced propulsion system designed for hypersonic speeds above Mach 5. Unlike conventional jet engines, scramjets compress incoming air at supersonic speeds without using rotating compressor blades, making them ideal for high-speed military and space applications.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Ramp-Check.jpg" alt="Ramp Check"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Ramjet.jpg" alt="Scramjet"></td>
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     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Rate_of_climb" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Sea-Level_Standard_Atmosphere_(SLSA)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
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           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Rate of Climb</a>
           onmouseout="this.style.color='#40E0D0';">Sea-Level Standard Atmosphere (SLSA)</a>
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     <td class="description">The rate of climb measures how quickly an aircraft gains altitude, expressed in feet per minute (fpm). It is critical for ensuring obstacle clearance and optimizing climb performance during takeoff and flight. Aircraft specifications often list best rate-of-climb speeds for efficiency.</td>
     <td class="description">Sea-Level Standard Atmosphere (SLSA) is a reference model defining standard atmospheric conditions at sea level: 15°C temperature, 1013.25 hPa pressure, and 1.225 kg/m³ air density. It is used in aircraft performance calculations, engine power ratings, and aerodynamic assessments.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Rate-of-Climb.jpg" alt="Rate of Climb"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Sea-Level-Standard-Atmosphere-SLSA.jpg" alt="Sea-Level Standard Atmosphere"></td>
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         <a href="https://wiki.alsresume.com/index.php?title=Rated_Engine_Thrust" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Seaplane_Base" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Rated Engine Thrust</a>
           onmouseout="this.style.color='#40E0D0';">Seaplane Base</a>
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</td>
     <td class="description">Rated engine thrust is the maximum amount of thrust an engine can produce under standard operating conditions. It ensures the engine operates within safe limits, balancing performance and longevity. Exceeding rated thrust can cause overheating or structural damage.</td>
     <td class="description">A seaplane base is a dedicated airport or docking facility for seaplanes and amphibious aircraft. It includes water runways, docking areas, and maintenance facilities, allowing for operations in remote areas, coastal regions, or inland lakes where traditional runways are unavailable.</td>
    <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Rate-of-Thrust.jpg"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Philadelphia-Seaplane-Base.jpg" alt="Philadelphia Seaplane Base"></td>
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<tr>
    <td class="term">
        <a href="https://wiki.alsresume.com/index.php?title=Raven_Rock_Mountain_Complex" target="_blank"
          style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"
          onmouseover="this.style.color='#ff4f01';"
          onmouseout="this.style.color='#40E0D0';">Raven Rock</td>
    <td class="description">
        The Raven Rock Mountain Complex (RRMC), also known as “Site R (<span style="color: #00ff01; font-weight: bold; text-decoration: none; cursor: pointer;"
            onmouseover="this.style.color='#ff4f01';"
            onmouseout="this.style.color='#00ff01';"
            onclick="window.open('https://www.google.com/maps/@39.733119,-77.418647,15z/data=!3m1!1e3', '_blank')">N39°43'59.23" W77°25'07.13"</span>) is a secure underground U.S. military facility near the Pennsylvania–Maryland border. Built during the Cold War for continuity of government, it serves as a backup Pentagon and command center. Operated by the Department of Defense, it supports emergency communications, military coordination, and national security operations during crises or attacks.
    </td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Raven-Rock.jpg" alt="Raven Rock"></td>
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<tr>
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     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Reduced_Vertical_Separation_Minimum_(RVSM)" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Secondary_Flight_Controls" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Reduced Vertical Separation Minimum (RVSM)</a>
           onmouseout="this.style.color='#40E0D0';">Secondary Flight Controls</a>
</td>
    <td class="description">RVSM is a standard that reduces vertical separation between aircraft from 2,000 feet to 1,000 feet at altitudes between 29,000 and 41,000 feet. This increases airspace capacity and efficiency while maintaining strict altitude monitoring and certification requirements.</a>
</td>
</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Separation.jpg" alt="RVSM"></td>
    <td class="description">Secondary flight controls include flaps, slats, spoilers, and trim systems that enhance an aircraft’s performance beyond primary control surfaces. They optimize efficiency during takeoff, cruise, and landing, helping pilots manage aerodynamic forces more effectively.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Flaps-Tabs.jpg" alt="Secondary Flight Controls"></td>
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<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Aerial_refueling" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Sector_Entry_(Holding_Patterns)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Refueling Boom</a>
           onmouseout="this.style.color='#40E0D0';">Sector Entry (Holding Patterns)</a>
</td>
</td>
     <td class="description">A refueling boom is a rigid tube used in aerial refueling operations to transfer fuel between tanker and receiver aircraft. Commonly used by military aircraft, the boom allows efficient fuel transfer during flight without landing.</td>
     <td class="description">Sector entry refers to the predefined procedures pilots follow to enter a holding pattern at a navigation fix. It ensures orderly traffic management in congested airspace and allows for safe spacing before an approach or clearance to proceed.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Refueling-Boom.jpg" alt="Refueling Boom"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Holding.jpg" alt="Sector Entry"></td>
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     <td class="term">
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         <a href="https://wiki.alsresume.com/index.php?title=Afterburner" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Separation_Minimums_(Air_Traffic_Control)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Reheat (Afterburner)</a>
           onmouseout="this.style.color='#40E0D0';">Separation Minimums (Air Traffic Control)</a>
</td>
</td>
     <td class="description">Reheat, or afterburner, is a system in jet engines that injects additional fuel into the exhaust stream for increased thrust. Used in supersonic and military aircraft, it provides a significant boost in performance at the cost of high fuel consumption.</td>
     <td class="description">Separation minimums define the required distance between aircraft in controlled airspace to prevent collisions. These include vertical, horizontal, and time-based separation standards, ensuring safe navigation under both visual and instrument flight rules.</td>
     <td class="image-column"><img src=https://www.alsresume.com/wp-content/uploads/2025/03/Reheat.jpg" alt="Reheat"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Separations.jpg" alt="Separation Minimums"></td>
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     <td class="term">
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         <a href="https://wiki.alsresume.com/index.php?title=Relay_Station" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Ceiling_(aeronautics)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Relay Station</a>
           onmouseout="this.style.color='#40E0D0';">Service Ceiling</a>
</td>
</td>
     <td class="description">A relay station retransmits communication or navigation signals to extend their range. It is often used in remote or mountainous areas where direct line-of-sight transmission is unavailable, ensuring reliable communication for pilots and controllers.</td>
     <td class="description">The service ceiling is the maximum altitude at which an aircraft can maintain a specified rate of climb, usually 100 feet per minute. It is an important performance limitation for pilots when planning flights in high-altitude environments.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Relay-Station.jpg" alt="Relay Station"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Service-Ceiling.jpg" alt="Service Ceiling"></td>
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     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Bearing_(navigation)#Relative" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Shock_Stall_(Supersonic_Aerodynamics)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Relative Bearing</a>
           onmouseout="this.style.color='#40E0D0';">Shock Stall (Supersonic Aerodynamics)</a>
</td>
</td>
     <td class="description">Relative bearing is the angle between the aircraft's nose and the direction to a navigational aid or target, measured clockwise. Pilots use it for situational awareness and precise navigation, especially when relying on non-directional beacons.</td>
     <td class="description">A shock stall occurs when a high-speed aircraft encounters shock waves that disrupt airflow over the wings, leading to a sudden loss of lift. This is a critical factor in transonic and supersonic flight, requiring careful speed management and advanced wing design.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Relative-Position.jpg" alt="Relative Bearing"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Mach.jpg" alt="Shock Stall"></td>
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         <a href="https://wiki.alsresume.com/index.php?title=Rendezvous_Point" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=STOL" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Rendezvous Point</a>
           onmouseout="this.style.color='#40E0D0';">Short Takeoff and Landing (STOL)</a>
</td>
</td>
     <td class="description">A rendezvous point is a pre-determined location where aircraft meet for refueling, formation flying, or coordinated operations. It ensures efficiency and synchronization during military missions, aerial refueling, or search-and-rescue efforts.</td>
     <td class="description">STOL aircraft are designed to operate on short runways, using enhanced lift devices such as leading-edge slats, powerful engines, and optimized wing designs. They are used for remote area access, bush flying, and military operations where conventional runways are unavailable.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Rendezvous-Point.jpg" alt="Rendezvous Point"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/STOL.jpg" alt="Short Takeoff and Landing"></td>
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     <td class="term">
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         <a href="https://wiki.alsresume.com/index.php?title=Required_navigation_performance" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Side-stick" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Required Navigation Performance (RNP)</a>
           onmouseout="this.style.color='#40E0D0';">Side Stick Controller</a>
</td>
</td>
     <td class="description">RNP specifies the accuracy and performance capabilities required for aircraft to fly certain routes. It integrates navigation, monitoring, and alerting systems, allowing precise operations in congested or complex airspace.</td>
     <td class="description">A side stick is a joystick-style flight control system replacing traditional yokes in modern aircraft. Used in Airbus and fighter jets, it provides precise control inputs and reduces cockpit clutter, improving ergonomics and pilot workload management.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Required-Navigation.jpg" alt="RNP"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Side-Stick.jpg" alt="Side Stick Controller"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Restricted_airspace" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Situation_awareness" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Restricted Airspace</a>
           onmouseout="this.style.color='#40E0D0';">Situational Awareness (SA)</a>
</td>
</td>
     <td class="description">Restricted airspace is an area where flight is limited or prohibited for safety or security reasons. Pilots require special clearance to enter these zones, often used for military operations or sensitive installations.</td>
     <td class="description">Situational awareness refers to a pilot’s ability to accurately perceive flight conditions, including position, weather, traffic, and aircraft performance. It is crucial for decision-making, accident prevention, and safe flight operations, especially in high-pressure or emergency scenarios.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Restricted-Airspace.jpg" alt="Restricted Airspace"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Situational-Awareness.jpg" alt="Situational Awareness"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Return_to_Base_(RTB)" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Yaw_String_(Slip_String)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Return to Base (RTB)</a>
           onmouseout="this.style.color='#40E0D0';">Skid (Yaw Control)</a>
</td>
</td>
     <td class="description">RTB is a directive for an aircraft to return to its home base or origin point. It is issued during emergencies, mission completions, or adverse conditions, ensuring the aircraft’s safe recovery.</td>
     <td class="description">A skid occurs when an aircraft turns too sharply without sufficient rudder input, causing it to slide sideways. Skids can lead to dangerous loss of control, making coordinated rudder and aileron use essential for smooth, efficient turns.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Return-to-Base.jpg" alt="Return to Base"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Skid.jpg" alt="Skid (Yaw Control)"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Thrust_reversal" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Leading-edge_slat" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Reverse Thrust</a>
           onmouseout="this.style.color='#40E0D0';">Slat (Leading Edge Device)</a>
</td>
</td>
     <td class="description">Reverse thrust is a mechanism that redirects engine thrust forward to slow an aircraft during landing. Common in jet and turboprop aircraft, it reduces wear on brakes and shortens landing distances.</td>
     <td class="description">A slat is a moveable aerodynamic surface on the leading edge of a wing, extending at low speeds to increase lift. It improves stall resistance and enhances takeoff and landing performance by delaying airflow separation.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Reverse-Thrust.jpg" alt="Reverse Thrust"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/slats.jpg" alt="Slat (Leading Edge Device)"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Reynolds_Number" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Slipstream_Effect" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Reynolds Number</a>
           onmouseout="this.style.color='#40E0D0';">Slipstream Effect</a>
</td>
</td>
     <td class="description">The Reynolds number measures the ratio of inertial forces to viscous forces in fluid flow around an aircraft. It helps predict aerodynamic behavior and is crucial for wing design and performance analysis.</td>
     <td class="description">Slipstream refers to the high-velocity air pushed behind a propeller or jet engine. It affects aerodynamic performance and yaw tendencies, requiring pilots to counteract slipstream-induced rolling or yawing motions, particularly during takeoff and landing.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Reynolds-Number.jpg" alt="Reynolds Number"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Slipstream.jpg" alt="Slipstream Effect"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Right_of_Way_(Aviation_Rules)" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Leading-edge_slot" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Right of Way (Aviation Rules)</a>
           onmouseout="this.style.color='#40E0D0';">Slot (Aerodynamics)</a>
</td>
</td>
     <td class="description">Right of way rules dictate which aircraft has priority during potential conflicts. For instance, gliders have right of way over powered aircraft, and aircraft on final approach take precedence over others in the pattern.</td>
     <td class="description">A slot is a fixed or moveable opening on a wing’s leading edge that enhances airflow over the surface, preventing premature stalls. Used in high-lift wing designs, slots improve performance in slow-speed operations.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Right-of-Way.jpg" alt="Right of Way"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Slotted-Wing.jpg" alt="Slot (Aerodynamics)"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Aircraft_principal_axes" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Sluggish_Controls_(High-Altitude_Effects)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Roll Axis</a>
           onmouseout="this.style.color='#40E0D0';">Sluggish Controls (High-Altitude Effects)</a>
</td>
</td>
     <td class="description">The roll axis is the longitudinal axis of an aircraft, running nose-to-tail. Movement around this axis is controlled by ailerons, affecting the aircraft’s banking angle and lateral stability during turns.</td>
     <td class="description">At high altitudes, thinner air can make an aircraft’s control surfaces feel less responsive, a phenomenon known as sluggish controls. Pilots must anticipate this effect, using greater control deflections or hydraulic assistance to maintain precise handling.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Roll-Axis.jpg" alt="Roll Axis"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Sluggish-controls.jpg" alt="Sluggish Controls (High-Altitude Effects)"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Rotorcraft" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Spoiler_(aeronautics)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Rotary-Wing Aircraft</a>
           onmouseout="this.style.color='#40E0D0';">Speed Brakes (Spoilers)</a>
</td>
</td>
     <td class="description">Rotary-wing aircraft, such as helicopters, use spinning rotor blades to generate lift and thrust. They are capable of vertical takeoff, landing, and hovering, making them ideal for rescue, military, and urban transport missions.</td>
     <td class="description">Speed brakes are aerodynamic surfaces that deploy to increase drag and reduce speed. They are commonly used during descent, approach, and landing to manage airspeed without overloading the braking system.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Rotary-wing.jpg" alt="Rotary-Wing Aircraft"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Speedbreaks.jpg" alt="Speed Brakes"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Rotor_Wash" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Spin_(aerodynamics)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Rotor Wash</a>
           onmouseout="this.style.color='#40E0D0';">Spin Recovery</a>
</td>
</td>
     <td class="description">Rotor wash refers to the strong downward airflow generated by helicopter rotors. It can create turbulence and affect nearby objects or people, requiring caution during low-altitude operations.</td>
     <td class="description">Spin recovery is the procedure pilots use to regain control after an aircraft enters an aerodynamic spin. It involves reducing power, applying opposite rudder, and neutralizing the ailerons to break the spin cycle and restore controlled flight.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Rotor-Wash.jpg" alt="Rotor Wash"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Spin-Recovery.jpg" alt="Spin Recovery"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Vertical_stabilizer" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Spoileron" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Rudder</a>
           onmouseout="this.style.color='#40E0D0';">Spoileron (Roll Control Device)</a>
</td>
</td>
     <td class="description">The rudder is a control surface on the vertical stabilizer, controlling yaw motion. Pilots use the rudder for directional control, especially during crosswind landings or coordinated turns.</td>
     <td class="description">A spoileron is a combination of a spoiler and an aileron, used to enhance roll control while reducing lift. Found on advanced aircraft, spoilerons assist in smoother maneuvering and greater stability in high-speed flight.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Rudder.jpg" alt="Rudder"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Spoileron.jpg" alt="Spoileron (Roll Control Device)"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Runway_Centerline_Lights" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=List_of_transponder_codes" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Runway Centerline Lights</a>
           onmouseout="this.style.color='#40E0D0';">Squawk Code (Transponder Setting)</a>
</td>
</td>
     <td class="description">Runway centerline lights are in-ground lights marking the runway’s centerline, aiding pilots during low-visibility operations. They are white and turn alternating red and white near the runway end.</td>
     <td class="description">A squawk code is a four-digit number assigned by air traffic control for aircraft identification. It allows controllers to track and communicate with aircraft efficiently, including emergency codes like 7500 (hijacking), 7600 (radio failure), and 7700 (emergency).</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Runway-Centerline-Lights.jpg" alt="Runway Centerline Lights"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Skwalk.jpg" alt="Squawk Code (Transponder Setting)"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Runway_edge_lights" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Stall_Margin" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Runway Edge Lights</a>
           onmouseout="this.style.color='#40E0D0';">Stall Margin</a>
</td>
</td>
     <td class="description">Runway edge lights outline the edges of a runway, providing visual guidance for pilots during night or low-visibility conditions. They are typically white but turn yellow near the runway's far end.</td>
     <td class="description">Stall margin is the buffer between an aircraft’s current angle of attack and its critical stall angle. Maintaining a sufficient stall margin ensures safe operations, particularly during takeoff, landing, and maneuvering in turbulent air.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Runway-edge-lights.jpg" alt="Runway Edge Lights"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Stall-Margin.jpg" alt="Stall Margin"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Runway_excursion" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Static_Discharger_(Lightning_Protection)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Runway Excursion</a>
           onmouseout="this.style.color='#40E0D0';">Static Discharger (Lightning Protection)</a>
</td>
</td>
     <td class="description">A runway excursion occurs when an aircraft veers off or overruns the runway during landing or takeoff. It is caused by factors like poor braking, adverse weather, or pilot error.</td>
     <td class="description">A static discharger is a small rod or wick on an aircraft that dissipates built-up electrical charge, reducing the risk of lightning strikes and radio interference. These devices enhance the safety of communication and navigation systems.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Runway-Excursion.jpg" alt="Runway Excursion"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Static.jpg" alt="Static Discharger (Lightning Protection)"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Runway_incursion" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Pitot%E2%80%93static_system" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Runway Incursion</a>
           onmouseout="this.style.color='#40E0D0';">Static Port (Pitot-Static System Component)</a>
</td>
</td>
     <td class="description">A runway incursion is any unauthorized presence of an aircraft, vehicle, or person on an active runway. It poses significant safety risks, requiring immediate action by air traffic controllers and pilots.</td>
     <td class="description">A static port is an external opening on an aircraft that measures atmospheric pressure for the pitot-static system. It provides essential data for airspeed, altitude, and vertical speed indicators.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Runway-incursion.jpg" alt="Runway Incursion"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/02/Pitot-Tube.jpg" alt="Static Port (Pitot-Static System Component)"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Runway_Threshold" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Step_Climb_(Fuel_Efficiency_Technique)" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Runway Threshold</a>
           onmouseout="this.style.color='#40E0D0';">Step Climb (Fuel Efficiency Technique)</a>
</td>
</td>
     <td class="description">The runway threshold is the beginning portion of the runway usable for landing. Marked with white stripes, it ensures proper touchdown alignment and distance for safe operations.</td>
     <td class="description">A step climb is a gradual increase in cruising altitude during long-haul flights to optimize fuel efficiency. As an aircraft burns fuel and becomes lighter, it can ascend to higher, more efficient flight levels.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Runway-Threshold.jpg" alt="Runway Threshold"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Step-Climb.jpg" alt="Step Climb"></td>
</tr>
</tr>


<tr>
<tr>
     <td class="term">
     <td class="term">
         <a href="https://wiki.alsresume.com/index.php?title=Runway_visual_range" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Supersonic_transport" target="_blank"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           style="color: #40E0D0; font-weight: bold; text-decoration: none; cursor: pointer;"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseover="this.style.color='#ff4f01';"  
           onmouseout="this.style.color='#40E0D0';">Runway Visual Range (RVR)</a>
           onmouseout="this.style.color='#40E0D0';">Supersonic Transport (SST)</a>
</td>
</td>
     <td class="description">RVR measures the distance a pilot can see down the runway, indicating visibility conditions. It is critical for determining landing and takeoff minimums, especially in fog or heavy rain.</td>
     <td class="description">Supersonic transport refers to commercial aircraft capable of flying faster than Mach 1, such as the Concorde. SSTs significantly reduce travel time but require specialized aerodynamics and materials to withstand high-speed stresses.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Runway-Visual-Range.jpg" alt="Runway Visual Range"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/SST.jpg" alt="Supersonic Transport"></td>
</tr>
</tr>


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         <a href="https://wiki.alsresume.com/index.php?title=Runway-Taxiway_Intersection" target="_blank"  
         <a href="https://wiki.alsresume.com/index.php?title=Synthetic_vision_system" target="_blank"  
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           onmouseout="this.style.color='#40E0D0';">Runway-Taxiway Intersection</a>
           onmouseout="this.style.color='#40E0D0';">Synthetic Vision System (SVS)</a>
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     <td class="description">A runway-taxiway intersection is a point where a runway and taxiway cross, requiring clear communication between pilots and air traffic control to ensure safe ground operations.</td>
     <td class="description">SVS is an advanced avionics technology that displays a real-time, 3D-rendered view of terrain, runways, and obstacles on cockpit screens. It enhances pilot awareness in low-visibility conditions, improving safety and navigation accuracy.</td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/Runway-Taxiway.jpg" alt="Runway-Taxiway Intersection"></td>
     <td class="image-column"><img src="https://www.alsresume.com/wp-content/uploads/2025/03/SVS.jpg" alt="Synthetic Vision System (SVS)"></td>
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Latest revision as of 19:35, 23 April 2025


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Aviation Glossary - A

Safe Life (Aircraft Design Principle) Safe life is an engineering principle ensuring that an aircraft component will function safely for a predetermined lifespan before requiring mandatory replacement. Components designed under this philosophy are monitored for fatigue and wear, preventing failures through strict maintenance schedules, particularly in critical structures like landing gear and wings. Safe Life
Satellite Navigation (SatNav) Satellite navigation, or SatNav, is a global positioning system used in aviation for precise flight planning and real-time navigation. It improves situational awareness, enhances safety, and allows for accurate approaches, particularly in GPS-based landing systems, replacing traditional ground-based navigation aids in many modern aircraft. Satellite Navigation
Scalloping (Aerodynamics) Scalloping refers to the aerodynamic phenomenon where sections of an aircraft surface, such as propeller blades or wings, develop a wavy pattern due to pressure differentials. This can cause structural stress, reduce efficiency, and impact lift characteristics, necessitating precise engineering to mitigate its effects. Scalloping
Scramjet (Supersonic Combustion Ramjet) A scramjet is an advanced propulsion system designed for hypersonic speeds above Mach 5. Unlike conventional jet engines, scramjets compress incoming air at supersonic speeds without using rotating compressor blades, making them ideal for high-speed military and space applications. Scramjet
Sea-Level Standard Atmosphere (SLSA) Sea-Level Standard Atmosphere (SLSA) is a reference model defining standard atmospheric conditions at sea level: 15°C temperature, 1013.25 hPa pressure, and 1.225 kg/m³ air density. It is used in aircraft performance calculations, engine power ratings, and aerodynamic assessments. Sea-Level Standard Atmosphere
Seaplane Base A seaplane base is a dedicated airport or docking facility for seaplanes and amphibious aircraft. It includes water runways, docking areas, and maintenance facilities, allowing for operations in remote areas, coastal regions, or inland lakes where traditional runways are unavailable. Philadelphia Seaplane Base
Secondary Flight Controls Secondary flight controls include flaps, slats, spoilers, and trim systems that enhance an aircraft’s performance beyond primary control surfaces. They optimize efficiency during takeoff, cruise, and landing, helping pilots manage aerodynamic forces more effectively. Secondary Flight Controls
Sector Entry (Holding Patterns) Sector entry refers to the predefined procedures pilots follow to enter a holding pattern at a navigation fix. It ensures orderly traffic management in congested airspace and allows for safe spacing before an approach or clearance to proceed. Sector Entry
Separation Minimums (Air Traffic Control) Separation minimums define the required distance between aircraft in controlled airspace to prevent collisions. These include vertical, horizontal, and time-based separation standards, ensuring safe navigation under both visual and instrument flight rules. Separation Minimums
Service Ceiling The service ceiling is the maximum altitude at which an aircraft can maintain a specified rate of climb, usually 100 feet per minute. It is an important performance limitation for pilots when planning flights in high-altitude environments. Service Ceiling
Shock Stall (Supersonic Aerodynamics) A shock stall occurs when a high-speed aircraft encounters shock waves that disrupt airflow over the wings, leading to a sudden loss of lift. This is a critical factor in transonic and supersonic flight, requiring careful speed management and advanced wing design. Shock Stall
Short Takeoff and Landing (STOL) STOL aircraft are designed to operate on short runways, using enhanced lift devices such as leading-edge slats, powerful engines, and optimized wing designs. They are used for remote area access, bush flying, and military operations where conventional runways are unavailable. Short Takeoff and Landing
Side Stick Controller A side stick is a joystick-style flight control system replacing traditional yokes in modern aircraft. Used in Airbus and fighter jets, it provides precise control inputs and reduces cockpit clutter, improving ergonomics and pilot workload management. Side Stick Controller
Situational Awareness (SA) Situational awareness refers to a pilot’s ability to accurately perceive flight conditions, including position, weather, traffic, and aircraft performance. It is crucial for decision-making, accident prevention, and safe flight operations, especially in high-pressure or emergency scenarios. Situational Awareness
Skid (Yaw Control) A skid occurs when an aircraft turns too sharply without sufficient rudder input, causing it to slide sideways. Skids can lead to dangerous loss of control, making coordinated rudder and aileron use essential for smooth, efficient turns. Skid (Yaw Control)
Slat (Leading Edge Device) A slat is a moveable aerodynamic surface on the leading edge of a wing, extending at low speeds to increase lift. It improves stall resistance and enhances takeoff and landing performance by delaying airflow separation. Slat (Leading Edge Device)
Slipstream Effect Slipstream refers to the high-velocity air pushed behind a propeller or jet engine. It affects aerodynamic performance and yaw tendencies, requiring pilots to counteract slipstream-induced rolling or yawing motions, particularly during takeoff and landing. Slipstream Effect
Slot (Aerodynamics) A slot is a fixed or moveable opening on a wing’s leading edge that enhances airflow over the surface, preventing premature stalls. Used in high-lift wing designs, slots improve performance in slow-speed operations. Slot (Aerodynamics)
Sluggish Controls (High-Altitude Effects) At high altitudes, thinner air can make an aircraft’s control surfaces feel less responsive, a phenomenon known as sluggish controls. Pilots must anticipate this effect, using greater control deflections or hydraulic assistance to maintain precise handling. Sluggish Controls (High-Altitude Effects)
Speed Brakes (Spoilers) Speed brakes are aerodynamic surfaces that deploy to increase drag and reduce speed. They are commonly used during descent, approach, and landing to manage airspeed without overloading the braking system. Speed Brakes
Spin Recovery Spin recovery is the procedure pilots use to regain control after an aircraft enters an aerodynamic spin. It involves reducing power, applying opposite rudder, and neutralizing the ailerons to break the spin cycle and restore controlled flight. Spin Recovery
Spoileron (Roll Control Device) A spoileron is a combination of a spoiler and an aileron, used to enhance roll control while reducing lift. Found on advanced aircraft, spoilerons assist in smoother maneuvering and greater stability in high-speed flight. Spoileron (Roll Control Device)
Squawk Code (Transponder Setting) A squawk code is a four-digit number assigned by air traffic control for aircraft identification. It allows controllers to track and communicate with aircraft efficiently, including emergency codes like 7500 (hijacking), 7600 (radio failure), and 7700 (emergency). Squawk Code (Transponder Setting)
Stall Margin Stall margin is the buffer between an aircraft’s current angle of attack and its critical stall angle. Maintaining a sufficient stall margin ensures safe operations, particularly during takeoff, landing, and maneuvering in turbulent air. Stall Margin
Static Discharger (Lightning Protection) A static discharger is a small rod or wick on an aircraft that dissipates built-up electrical charge, reducing the risk of lightning strikes and radio interference. These devices enhance the safety of communication and navigation systems. Static Discharger (Lightning Protection)
Static Port (Pitot-Static System Component) A static port is an external opening on an aircraft that measures atmospheric pressure for the pitot-static system. It provides essential data for airspeed, altitude, and vertical speed indicators. Static Port (Pitot-Static System Component)
Step Climb (Fuel Efficiency Technique) A step climb is a gradual increase in cruising altitude during long-haul flights to optimize fuel efficiency. As an aircraft burns fuel and becomes lighter, it can ascend to higher, more efficient flight levels. Step Climb
Supersonic Transport (SST) Supersonic transport refers to commercial aircraft capable of flying faster than Mach 1, such as the Concorde. SSTs significantly reduce travel time but require specialized aerodynamics and materials to withstand high-speed stresses. Supersonic Transport
Synthetic Vision System (SVS) SVS is an advanced avionics technology that displays a real-time, 3D-rendered view of terrain, runways, and obstacles on cockpit screens. It enhances pilot awareness in low-visibility conditions, improving safety and navigation accuracy. Synthetic Vision System (SVS)