Learning. Goals. of pressure. aircraft. Altimeter knob. Page 1 of 8. Document : V1.1

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LEVELS AND ALTITUDES Learning Goals LEVELS AND ALTITUDES In aviation it is of the utmost importance that a pilot knows his height above ground level for safe landing and obstacle avoidance. For air traffic controllers its for obvious reasons absolutely necessary to know at which altitudes aircrafts are flying. For this reason, every aircraft is equipped with some sort of pressure altimeter. A pressure altimeter (also called barometric altimeter) is the altimeter found in most aircrafts. In it, an aneroid baromete r measures the atmospheric pressure from a static port outside the aircraft. Air pressure decreases with an increase of altitude approximately: 1Hpa ( 1mbar) for every 27ft (below FL180) 1Hpa ( 1mbar) for every 48ft (above FL180) The altimeter is calibrated to show the pressure directly as an altitude above MSL (Mean Sea Level), in accordance with a mathematical model defined by the ISA (International Standard Atmosphere). Older aircraft used a simple ameroid barometer where the needle made less than one revolution around the face from zero to full scale. Modern aircraft use a "sensitive altimeter" which has a primary needle that makes multiple revolutions, and one or more secondary needles that show the number of revolutions, similar to a clock face. In other words, each needle points to a different digit of the current altitude Altimeter measurement. On a sensitive altimeter, the sea level reference pressure can be adjusted by a setting knob. The reference pressure, in inches of mercury in Canada amd the US and hectopascals (previously millibar) elsewhere, is displayed in the Kollsman window. This is necessary, since sea level reference atmospheric pressure varies with temperature and the movement of pressure systems in the atmosphere. Altimeter knob Kollsman window Page 1 of 8

Reference pressure levels QNE Transtion level Transition Layer Transtion Altitude QFE Sea level QNH Terrain level Q-codes The Q code is a standardized collection of three-letter message encodings, all starting with the letter "Q", initially developedd for commercial radiotelegrapgh communication, and later adopted by other radio services, especially amateur radio. Although Q codes were created when radio used Mores code exclusively, they continued to be employed after the introduction of voice transmissions. Although the majority of the Q codes have slipped out of common use, several remain part of the standard ICAO radiotelephony phraseology in aviation. Page 2 of 8

QNH: QNE: QFE: QFF: Atmospheric pressure at mean sea level (may be either a local, measured pressure or a regional forecast pressure) Pressuree altitude in the International Standard Atmosphere (1013.25 mbar at sea level) Atmospehric pressure at airfield elevation Baromettric pressure at a place, reduced to MSL (Mean Sea Level) using the actual temperature at the time of obeservation as the mean temperature QNH As reference pressure level the actual pressure at terrain level is reduced to sea level pressure (MSL) via the standard elapsed rate. The pressure altitude is referred to as altitude in feet. At low levels the QNH-setting is used to assure obstacle clearancee based on MSL. Since the elapsed rate almost never equals the standardd elapsed rate the terrain height will not be in accordance with the altitude reading based on the QNH. QNE E Standard Altimeter Setting (SAS = 1013,2 Hpa) As reference pressure level the Standard Altimeter Setting (1013,2 Hpa) is used. This setting is one of the most used pressure settings. All air traffic flying above the transition altitude is required to use the SAS. In this manner it is possible to create safe altitude separation for all air traffic in controlled airspace. The Altitude based on the SAS is expressed in Flight levels (FL) in hundreds of feet. Thus 10000ft = FL100. Note that Flight level is not a true altitude but a relative altitude. QFE As reference pressure level the actual pressure at terrain level is used. The height readout from your barometric pressure altimeter will be the airport height above the earth surface. When entering the runway your barometric pressure altimeter should indicate 0 foot. The readout from you barometric altimeter set to QFE is expressed in heights in feet. A country that frequently uses the QFE is the United Kingdom and Russia Page 3 of 8

What is Transition Altitude?: Transition altitude is the maximum altitude where to fly under the local barometric pressure (QNH), use your altimeter. an aircraft is permitted this is where you would You should receive this barometric pressure in the relevant ATIS when you are parked at a gate, or the Departure or Tower controller may also inform you of this. This type of pressure is what's known as QNH. Above the Transition Altitude (QFE) a pilot would need to change his altimeter to the standard barometric pressure of 1013,25 (1013 for short ) Hpa or 29,92 inches of Mercury ( Which equals the barometric pressure at sea level). What is Transition Level?: This is the minimum altitude at which you are permitted to fly under the standard barometric pressure of 1013,25 Hpa. To this point the altitude at which you are flying willl be referred to as FL Flight Level. In the diagram below we can clearly see the red line denoting the TRL Transition Level and below that we see the TA Transition Altitude. What is Transition layer?: For safe transition from QNH-setting to QNE setting or vice versa a separation layer is needed. The This layer between the Transition altitude and Transition level is called the Transition Layer. width of this layer is determined by ATC The reason for applying this separation layer is due to the fact that Pressure Altitude Variation (PAV) will occur. Hence: a:) The pressure at sea level usually deviates from 1013,2 Hpa b:) The actual elapsed rate usually deviates from the standard elapsed rate. Page 4 of 8

As we can see there is a gap between the TRL and the TA. This gap is created by means of the current local QNH. For example let's imagine the local QNH at Schiphol Amsterdamm EHAM was 1015Hpa. The Transition altitude is fixed at 3000ft, then the TL would be at FL040. The following table should clarify this in more detail. QNH (hpa) 942-9599 960-9777 978-995 996-1013 1014-10311 1032-10500 1051-3000ft FL 060 FL 055 FL 050 FL 045 FL 040 FL 035 FL 030 4000ft FL 070 FL 065 FL 060 FL 055 FL 050 FL 045 FL 040 5000ft FL 080 FL 075 FL 070 FL 065 FL 060 FL 055 FL 050 6000ft 7000ft FL 0900 FL 100 FL 085 FL 095 FL 0800 FL 090 FL 075 FL 085 FL 0700 FL 080 FL 065 FL 075 Inch. of Merc *) 27.82-28.33 28.34-28.86 28.87-29.39 29.40-29.92 29.93-30.46 30.47-31.03 FL 0600 FL 070 31..04 - Page 5 of 8

It is therefore very important for a pilot to insert the correct barometric pressure in his altimeter. This could mean the difference between life and death. Now Let's Recap: When you are on the ground wanting to depart, you would work with Transition Altitude. Until climbing passed the TA you would use the local QNH setting. If you are descending from the cruise you would work with Transition Level. Until you reach the TL you would have your altimeter set to 1013,25Hpa or 29,92 Inches of Mercury. When you descendd throughh the TL you would change your altimeter to the local barometric setting ( QNH) of the airport. For every 27 feet you climb the barometric pressure changes by 1 Hpa. Imagine you are at 600 feet with a barometric pressure of 1013,0 Hpa the calculation would be as follows: 600 27 = 22,2 Hpa 1013,00 22,2 = 990.8 Hpa Read this document carefully should you require it. Make sure you know when to use Flight levels or Altitude in Feet. QNH QFE : Query Nautical Height (Regional Pressure Setting) : Query Field Elevation Page 6 of 8

Semi Circular Rules To improve separation during cruising flight, pilots have to select a Level (Level means an Altitude or a Flight Level) according the direction of their flight. This is called the semi-circular cruising level system.. Pilots who fly more or less in the same direction select the same levels so aircraft from the opposite direction are passed above or below. This way, the risk of head-on collisions is reduced because there is slightly more time to see opposite traffic. East-West configuration: East West : heading 00 00-179 degrees : heading 180-359 degrees Choose ODD flightlevel Choose EVEN flightlevel North-South configuration: North South : heading 270-089 degrees : heading 090-269 degrees Choose ODD flightlevel Choose EVEN flightlevel Countries like: France, Portugal, Spain, Italy, Egypt etc. use the North-South configuration. From Levels 3000ft and below, IFR and VFR is allowed to use any level VFR altitudes are limited to FL200 and fly 500ft above the odd and even flightlevels RVSM airspace: (reduced vertical separation minimum) The airspace between Flight level 290 and 410 are with 2000ft. normally separated fl 290 fl 310-330 - 370-350 - 390 The airspace was limited to 6 levels only for safety reasons. As instrument accuracy improved and more commercial airlines started using thesee economical flight levels, aircrafts which comply to MNPS ( minimumm navigational performance specifications) are allowed to fly levels that are separated by 1000ft, thus doubling the capacity fl 290 fl 300-310 - 330-350 - 320-340 - 360-370 - 390-380 - 400 For detailed information...check : http:// /academy. ivao.aero/ /node/340 Page 7 of 8

APENDIX A : Pressure conversion Altimeter setting: Non- US: QNH ( Q code Nautical height) in HectoPascal (hpa) / Millibar (mbar) US: Altimeter in inches of mercury (inchhg) (kwikdruk) QNH / ALTIMETER 950 951 28.05 28.08 960 961 28.35 28.38 970 971 28.64 28.67 980 981 28.94 28.97 990 991 29.23 29.26 1000 1001 29.53 29.56 1010 1011 29.83 29.85 1020 1021 30.12 30.15 1030 1031 30.42 30.45 1040 1041 30.71 30.74 952 28.11 962 28.41 972 28.7 982 29 992 29.29 1002 29.59 1012 29.88 1022 30.18 1032 30.47 1042 30.77 953 28.14 963 28.44 973 28.73 983 29.03 993 29.32 1003 29.62 1013 29.91 1023 30.21 1033 30.5 1043 30.8 954 28.17 955 28.2 956 28.23 957 28..26 958 28.29 959 28.322 964 28.47 965 28.5 966 28.53 967 28..56 968 28.59 969 28.61 974 28.76 975 28.79 976 28.82 977 28..85 978 28.88 979 28.91 984 29.06 985 29.09 986 29.12 987 29..15 9888 29.18 989 29.21 994 29.35 995 29.38 996 29.41 997 29..44 998 29.47 999 29.5 1004 1005 1006 1007 1008 1009 29.65 29.68 29.71 29..74 29.77 29.8 1014 1015 1016 1017 1018 1019 29.94 29.97 30 30..03 30.06 30.09 1024 1025 1026 1027 1028 1029 30.24 30.27 30.3 30..33 30.36 30.39 1034 1035 1036 1037 1038 1039 30.53 30.56 30.59 30..62 30.65 30.68 1044 1045 1046 1047 1048 1049 30.83 30.86 30.89 30..92 30.95 30.98 Page 8 of 8