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Aircraft approach category
Grouping used for air traffic control
Grouping used for air traffic control
An aircraft approach category is a grouping which differentiates aircraft based on the speed at which the aircraft approaches a runway for landing.
They are used to determine airspace, obstacle clearance and visibility requirements for instrument approaches.
Definition
The International Civil Aviation Organization (ICAO) classifies aircraft by their indicated airspeed at runway threshold (Vat, also known as approach speed or VREF).
The categories are as follows:
- Category A: less than 169 km/h indicated airspeed (IAS)
- Category B: 169 km/h or more but less than 224 km/h IAS
- Category C: 224 km/h or more but less than 261 km/h IAS
- Category D: 261 km/h or more but less than 307 km/h IAS
- Category E: 307 km/h or more but less than 391 km/h IAS
- Category H: Helicopters
Helicopters may use Category A minima on instrument procedures designed for aeroplanes, or may use specific procedures designed for helicopters.
Threshold speed is calculated as 1.3 times stall speed Vs0 or 1.23 times stall speed Vs1g in the landing configuration at maximum certificated landing mass. Aircraft approach categories do not change during day-to-day operation. To change an aircraft's category, an aircraft must be re-certified with a different maximum landing mass. Pilots may not use a lower category than the one certified, but may choose to use a higher category for higher speed approaches.
The maximum permitted speed for visual manoeuvring is significantly higher than the threshold speed. Additional speed ranges are specified for other segments of the approach.
Approach plates generally include visibility requirements up to category D. While ICAO specify a top speed of 391 km/h for Category E, there exist no aircraft with an approach speed above this.
United States of America
Approach category definitions in the United States of America are similar to those defined by ICAO. They are defined in terms of VREF of a given aircraft, or if VREF is not specified, 1.3 Vs0 at the maximum certificated landing weight. The values of VREF, VS0, and the maximum certificated landing weight are established for the aircraft by the certification authority of the country of registry. The United States does not give a top speed for Category E.
Examples
Selected examples from FAA Circular 150/5300-13A - Airport Design:
| Aircraft | Code | Approach Speed |
|---|---|---|
| Piper PA-28R Cherokee Arrow | A | 70 kn |
| Douglas DC-3 | A | 74 kn |
| Cessna 210 Centurion | A | 75 kn |
| Douglas DC-4 | B | 94 kn |
| Douglas DC-6 | B | 108 kn |
| Fokker F27 Friendship | B | 120 kn |
| Boeing 707-320B | C | 128 kn |
| McDonnell Douglas DC-9-15 | C | 132 kn |
| Boeing 737-700 | C | 130 kn |
| Boeing 737-800 | D | 142 kn |
| Airbus A350-900 | D | 145 kn |
| Boeing 747-400 | D | 157 kn |
The Northrop T-38 Talon is an example of an Approach Category E aircraft.
The Space Shuttle had a landing speed of about 346 km/h.
References
References
- "ICAO Doc 8168: Procedures for Air Navigation Services: Aircraft Operations: Volume I − Flight Procedures. Sixth edition, 2018.". ICAO.
- "AIM Revision Clarifies 'Approach Category' and Related Procedures".
- "14 CFR § 97.3 - Symbols and terms used in procedures.".
- "AC 150/5300-13B - Airport Design - Change 1".
- "The Space Shuttle and Its Operations".
This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page.
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