density altitude and True altitude
Hi there,
Could someone help me solve this question/calculation? I am not sure I am doing it right, most probably I am not :) QNH 981 station at MSL temperature = minus 14 ISA, what is your true altitude at FL090? standard pressure = 1013 1013 - 981 = 32 32 times 30(some use 27) = 960 Pressure is lower so ground is closer. FL090 = 90.000 ft 90.000 ft - 960 ft = 89.040 ft So pressure altitude is 89.040 ft, correct?? Then for true altitude we have minus 14 ISA, so: 120ft x -14 = -1.680 ft 89.040 ft - 1.680 ft = 87.360 ft |
FL 090 IS 9000FT,NOT 90000.
9000-960=8040 TEC=4ft/1000/8C- 4X8X14 =448. 8040-448= 7592 FT..... |
Hello Fly.b737
FL090 = 9000ft indicated, with 1013.25hpa in your altimeter window. Now remember the rule "from high to low(pressure) and from warm to cold(temperature) => look below" So your pressure corrections & your temperature corrections have to be subtracted from 9000ft with a QNH 981 and an ISA -14°C atmosphere giving 9000ft - 960ft - 448ft = 7592ft true altitude Density altitude(used for performance calculations, wings & engines only "know" density altitudes) = pressure alt, corrected for non standard temperatures Density alt. = press.alt 9000ft +120(delta ISA) = 9000 + 120(-14) = 9000 - 1680 = 7320ft BM |
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