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- Published: 30 Oct 2008
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- Author: machinima
A Flight Level (FL) is a standard nominal altitude of an aircraft, in hundreds of feet. This altitude is calculated from the International standard pressure datum of 1013.25 hPa (29.92 inHg), the average sea-level pressure, and therefore is not necessarily the same as the aircraft's true altitude either above mean sea level or above ground level.
To display altitude above sea level, a pilot must recalibrate the altimeter according to the local air pressure at sea level, to take into account natural variation of pressure over time and in different regions. If this is not done, two aircraft could be flying at the same altitude even though their altimeters appear to show that they are at considerably different altitudes. This is a critical safety issue.
Flight levels solve this problem - of aircraft flying at the same altitude, though their altimeters indicate different barometric heights - by defining altitudes based on a standardised air pressure at sea-level. All aircraft operating on flight levels calibrate to this setting regardless of the actual sea level pressure.
Flight levels are usually designated in writing as FLxxx, where xxx is a one- to three-digit number indicating the pressure altitude in units of 100 feet. In radio communications, FL290 would be pronounced as "flight level two niner zero", in most jurisdictions. The phrase "flight level" makes it clear that this refers to the standardized pressure altitude.
The transition altitude (TA) is the altitude above sea level at which aircraft change from the use of altitude to the use of flight levels. When operating at or below the TA, aircraft altimeters are usually set to show the altitude above sea level. Above the TA, the aircraft altimeter pressure setting is normally adjusted to the standard pressure setting of 1013 hectopascals (millibars) or 29.92 inches of mercury and aircraft altitude will be expressed as a flight level.
{| class="wikitable" align="right"
|+ Table for determining transition level
|-
!rowspan=2| QNH
(in millibars) !! colspan=5 | Transition altitude (in feet)
|-
! 3,000 !! 4,000 !! 5,000 !! 6,000 !! 18,000
|-
| align="center" | 1032–1050 || FL25 || FL35 || FL45 || FL55 || FL175
|-
| align="center" | 1014–1032 || FL30 || FL40 || FL50 || FL60 || FL180
|-
| align="center" | 996-1013 || FL35 || FL45 || FL55 || FL65 || FL185
|-
| align="center" | 978-995 || FL40 || FL50 || FL60 || FL70 || FL190
|-
| align="center" | 960-977 || FL45 || FL55 || FL65 || FL75 || FL195
|-
| align="center" | 943-959 || FL50 || FL60 || FL70 || FL80 || FL200
|-
|}
In the United States and Canada, the transition altitude is 18,000 ft. In Europe, the transition altitude varies and can be as low as 3,000 ft. There are discussions to standardise the transition altitude within the Eurocontrol area.
On November 25, 2004 the Civil Aviation Authority of New Zealand raised New Zealand's transition altitude from 11,000 feet to 13,000 feet and changing the transition level from FL130 to FL150.
The transition level is the lowest flight level above the transition altitude. The table on the right shows the transition level according to transition altitude and QNH. When descending below the transition level, the pilot starts to refer to altitude of the aircraft by setting the altimeter to the QNH for the region or airfield. Note that the transition level is, by definition, less than 500 ft above the transition altitude. Aircraft are not normally assigned to fly at the transition level as this does not guarantee separation from other traffic flying (on QNH) at the transition altitude; the lowest usable flight level is the transition level plus 500 ft.
The transition layer is the airspace between the transition altitude and the transition level.
In some countries, e.g., Norway, the transition level is determined including a buffer of minimum 1000 ft (depending on QNH) to the transition altitude. Therefore aircraft may be flying at both transition level and transition altitude, and still be vertically separated by at least 1000 ft. In those areas the transition layer will be a given vertical distance between 1000 ft and 1500 ft, depending on QNH.
The rule is non-binding upon flights operating under VFR.
Minimum vertical separation between two flights abiding by the UK Quadrantal Rule is 500 ft (note these are in geopotential foot units). The level to be flown is determined by the magnetic track of the aircraft, as follows:
* Magnetic Track 000 to, and including, 089° - odd thousands of feet (FL70, 90, 110 etc)
The semicircular rule (also known as the hemispheric rule) applies, in slightly different version, in all of the world, including in the UK inside controlled airspace.
The standard rule defines an East/West track split:
* Eastbound - Magnetic Track 000 to 179° - odd thousands (FL 250, 270, etc.)
Countries where the major airways are oriented north/south (e.g. New Zealand; Italy; Portugal) have semicircular rules that define a North/South rather than an East/West track split. In Italy, for example, southbound traffic uses odd flight levels.
Reduced Vertical Separation Minima or RVSM reduces the vertical separation above FL 290 from 2,000 ft to 1,000 ft. This allows aircraft to safely fly more optimum routes, gain fuel savings and increase airspace capacity by adding six new flight levels. Only aircraft that have been certified to meet RVSM standards, with several exclusions, are allowed to fly in RVSM airspace. It was introduced into the UK in March 2001. On January 20, 2002, it entered European airspace. The United States, Canada and Mexico transitioned to RVSM between FL 290 and FL 410 on January 20, 2005, and Africa on September 25, 2008.
* Track 000 to 179° - odd thousands (FL 290, 310, 330, etc.)
The flight levels below apply to Russia, Mongolia, North Korea, Kyrgyzstan, Kazakhstan, Tajikistan and Uzbekistan and 6,000 m or below in Turkmenistan (where feet is used for FL210 and above). Flight levels are read as e.g. "flight level 7,500 metres": ;Track 000 to 179°
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