Approach Slope
A comprehensive glossary entry on the aviation concept of approach slope, including definitions, associated concepts (glide slope/path, pitch angle, angle of at...
Descent in aviation is the controlled downward flight phase crucial for landing, approach, and safety. Explore key terms, procedures, and practical examples.
Descent in aviation describes the deliberate, controlled downward movement of an aircraft from a higher to a lower altitude. This maneuver is vital in every flight—executed for approach, landing, obstacle avoidance, airspace transitions, and to comply with air traffic control (ATC) instructions. Effective descent management ensures safety, operational efficiency, passenger comfort, and regulatory compliance. This glossary provides comprehensive definitions, explanations, and practical examples of key terms and procedures related to descent in aviation. It is a valuable technical reference for pilots, flight students, and aviation professionals.
Definition:
The approach is the flight phase where an aircraft transitions from en route or initial descent to runway alignment, following a pre-determined descent path. It is divided into segments: initial, intermediate, final, and missed approach. Each segment serves a purpose based on procedure type (visual, instrument, precision, or non-precision).
Operational Usage:
Pilots manage descent angle, airspeed, and configuration (flaps, landing gear, spoilers) and maintain awareness of terrain, obstacles, and traffic. Instrument approaches use navigational aids like ILS, VOR, or GPS to define descent paths. Stabilized approach is critical for safety and timely go-arounds.
Example:
A Boeing 737 intercepts the ILS glideslope at 2,500 feet AGL, selects flaps 15, extends landing gear, and reduces speed to 145 knots, maintaining a 3° descent angle.
Definition:
Attitude is the aircraft’s orientation relative to the horizon—pitch (nose up/down), roll (bank left/right), and yaw (nose left/right). The attitude indicator (artificial horizon) displays this in the cockpit.
Use in Descent:
In powered descents, pitch attitude controls descent rate, while power controls airspeed. In glides, pitch controls airspeed and glide angle. Correct attitude prevents stalls or unsafe descent rates.
Example:
A Cessna 172 lowers the nose for descent, adjusting pitch and power to maintain stable airspeed.
Definition:
Best glide speed (Vg) is the speed for maximum distance per unit altitude lost in a power-off glide, based on the aircraft’s design and weight. It’s critical for forced landings and emergencies.
Use:
Pilots set Vg promptly during engine failure to maximize survivability.
Example:
A Piper Archer (PA-28-181) experiences engine failure at 4,000 feet AGL. The pilot pitches for 76 knots (Vg) toward the nearest airport.
Definition:
Carburetor heat is a system to prevent ice formation in carburetors, common during low-power descents in cool, humid conditions.
Use in Descent:
Pilots apply carburetor heat before reducing power for descent, especially in high humidity and temperatures between -7°C and 21°C.
Example:
Descending through clouds at 15°C, a Cessna 152 pilot applies full carburetor heat before throttling back.
Definition:
Climb is controlled upward movement; descent is controlled downward movement. Both require coordinated power, pitch, and configuration changes.
Example:
After cruise, a pilot is cleared to descend to 4,000 feet, reduces power, pitches down, and configures for descent.
Definition:
A cruise descent is a steady, moderate descent during the en route phase, maintaining higher airspeeds and fuel efficiency compared to approach descent.
Use:
Used to transition from cruise to a lower altitude with minimal configuration changes.
Example:
At top of descent, a pilot reduces thrust and descends at 1,500 fpm at Mach 0.78 from 36,000 feet in cruise configuration.
Definition:
Descent is the controlled reduction in altitude, managed through pitch, power, and configuration. Descents vary by intent (en route, approach, emergency), power setting, and rate.
Example:
An Airbus A320 reduces thrust, pitches nose down, and monitors descent rate after ATC clearance.
Definition:
Descent angle is the angle between the aircraft’s flight path and the horizontal during descent. Typical precision approaches use a 3° angle.
Example:
On a standard ILS, the aircraft follows a 3° glideslope, descending at 700 fpm at 140 knots groundspeed.
Definition:
Descent approach is the segment transitioning from en route descent to final approach, involving speed reduction, flap extension, gear down, and checklist completion.
Example:
At 3,000 feet AGL, 15 miles out, a pilot slows the aircraft, extends flaps, and prepares for final approach.
Definition:
Descent landing is the final segment, including the flare, where descent rate is arrested prior to touchdown.
Example:
On glideslope, the pilot flares at 20 feet AGL, reducing descent rate for a smooth touchdown.
Definition:
Descent planning calculates when and how to descend from cruise, considering groundspeed, wind, required descent rate, and crossing restrictions.
Example:
A pilot at 30,000 feet planning to cross 3,000 feet at 10 miles uses the “3:1 rule” to start descent 81 miles out.
Definition:
The descent profile is the planned altitude, distance, speed, and configuration changes during descent, often displayed on flight management systems.
Example:
A STAR may require 10,000 feet at 250 knots at a waypoint, with further step-downs to the final approach fix.
Definition:
Descent speed is the airspeed maintained in descent, set by aircraft type, configuration, and operational constraints.
Example:
A Boeing 777 descends at 280 knots above 10,000 feet, then at 240 knots below.
Definition:
A descending turn combines a heading change with altitude loss, requiring coordinated aileron, rudder, and elevator input.
Example:
Descending from 2,000 to 1,500 feet, a pilot executes a 30° bank turn onto base leg.
Definition:
Drag opposes aircraft motion. During descent, increased drag (using flaps, gear, speedbrakes) helps control airspeed and descent angle.
Example:
On approach, a pilot extends gear and flaps to steepen descent and reduce speed.
Definition:
An en route descent is a planned descent from cruise, often at higher speeds and minimal configuration changes, initiated by ATC.
Example:
ATC instructs descent from FL350 to FL210; the crew reduces thrust, pitches down, and descends at Mach .78.
Definition:
In descent, equilibrium is achieved when lift, weight, thrust, and drag are balanced, resulting in steady, controlled descent.
Example:
In a steady glide, gravity pulls the aircraft forward, drag opposes motion, and lift supports part of the weight.
Definition:
Final approach is the last approach segment, with the aircraft aligned with the runway and on a constant descent path.
Example:
A CRJ200 intercepts the localizer and glideslope at 1,800 feet AGL and descends on a 3° path to touchdown.
Definition:
Flaps are movable surfaces on the wing’s trailing edge, increasing lift and drag to allow lower approach speeds and steeper descent angles.
Example:
A Cessna 182 extends flaps to 20° for a safe, controlled descent to landing.
Definition:
The flight path is the aircraft’s trajectory through the air, managed to ensure safe descent and alignment with the runway.
Example:
On precision approach, the aircraft remains within one dot of the glideslope and localizer.
Definition:
Flap settings are the selected degrees of flap extension, affecting lift, drag, and stall speed for each descent phase.
Example:
A Boeing 737 uses Flaps 5 for initial approach, Flaps 15 on final, and Flaps 30 for landing.
Definition:
A glide is a power-off descent, relying on gravity and aerodynamics. Glide angle and range depend on aircraft L/D ratio and airspeed.
Example:
A DA40 glides at 68 knots from 3,500 feet AGL, giving 5.5 nm of range.
Definition:
The glideslope is the vertical guidance component of ILS, usually set at 3°, leading to the runway touchdown zone.
Example:
An E190 follows the ILS glideslope on final, maintaining a constant descent to decision altitude.
Descent is a critical phase of flight, demanding skillful management of aircraft performance, configuration, and situational awareness. Mastering descent enhances safety, efficiency, and comfort for every flight. The terms and concepts above serve as the foundation for understanding, teaching, and executing controlled descents in aviation.
For more in-depth learning, consult your aircraft’s Pilot Operating Handbook (POH), participate in recurrent training, and practice descent procedures in a certified flight simulator or with a qualified instructor.
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Descent is the controlled reduction of an aircraft’s altitude, managed through pitch, power, and configuration adjustments. It is essential for approach, landing, and operational flexibility. Descents must be carefully planned and executed to ensure safety, regulatory compliance, and passenger comfort.
Pilots use descent planning formulas, flight management systems, or electronic flight bags to calculate the top of descent. They consider factors such as altitude to lose, groundspeed, wind, and required descent rates to ensure timely arrival at target altitudes while complying with ATC and terrain requirements.
A stabilized approach means the aircraft is on the correct path, at the appropriate speed, descent rate, and configuration for landing by a defined point (typically 1,000 feet AGL for instrument approaches). This reduces the risk of go-arounds and enhances safety.
Best glide speed (Vg) gives the maximum distance per unit altitude lost in a power-off situation. Maintaining this speed during engine failure maximizes the range to reach a safe landing site.
Drag slows the aircraft and can be increased deliberately using flaps, landing gear, or speedbrakes to steepen descent or reduce speed. Managing drag is crucial for maintaining safe speeds and descent angles, especially on approach.
Mastering descent techniques improves safety, fuel efficiency, and passenger comfort. Explore our advanced training, resources, and expert guidance to optimize every phase of flight.
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