TOD calculation 3° slope |
Calculation of the descent rate 3° / 5% slope | Calculator | ||||||||
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OR OR From the indicated speed (IAS) | |||||||||
IAS = Indicared AirSpeed >> speed directly indicated by the instruments, it comes directly from the external probes (Pitot), it is thus impacted by the density of the air mass. |
TAS = True Air Speed >> speed of an aircraft in relation to the air mass in which it is located, independently of its density. |
GS = Ground Speed >> speed relative to the ground. |
MACH = is the ratio of the speed of the aircraft in the air mass to the speed of sound in the same air mass. |
Ratio between the speeds: |
TAS=IAS+(FL/2) |
GS=TAS+-Wind component |
MACH=TAS/600 | Formulas used : | TOD distance = ( Cruise altitude (ft) - Target altitude(ft) / 𝟏𝟎𝟎 ) / 3° | TOD distance = ( FL cruise -FL target) / 3° | VS (ft/min) = GS x 5 |
VS (ft/min) = MACH x 3 x 3000 |
The calculation of the SV from the MACH and IAS speeds takes into account the wind component The calculation of the VS from the IAS speed uses the formula TAS=IAS+(FL/2). The FL used is the intermediate FL between the cruise FL and the target FL. | Source : https://mediawiki.ivao.aero/index.php?title=Top_of_descent_calculation |
Descent speed (source Eurocontrol) | ||
Aircraft code ICAO | Cruise >> FL 260 | FL260 >> FL100 |
A319/A19N//A320/A32N//A321/A21N | .78 | 290 |
A332 | .80 | |
A333/A338/A339 | .81 | |
A342/A343/A345/A346 | .81 | |
A388 | .83 | 300 |
B722 | .72 | 280 |
B731 | .68 | 270 |
B732/B733 | .70 | 280 |
B734/B735 | .74 | 280 |
B736/B738 | .78 | 280 |
B737 | .76 | 280 |
B742 | .84 | 290 |
B748 | .85 | 250 |
MD11 | .83 | 300 |
DH8D | - | 270 |
CL60 | .75 | 250 |
T154 | .72 | 290 |
AN24 | - | 240 |