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Flugzeugklasse S 3.1a - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 93,0 | 1,2 |
| 2 | 94,0 | 1,2 |
| 3 | 94,0 | 1,2 |
| 4 | 92,0 | 1,2 |
| 5 | 92,0 | 1,1 |
| 6 | 91,0 | 1,0 |
| 7 | 86,0 | 1,0 |
| 8 | 73,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 1800 | 0 | 80 | 0 |
| 4300 | 0 | 80 | - |
| 4800 | - | 80 | 460 |
| 5300 | -3 | 80 | - |
| 9000 | -3 | 80 | 920 |
| 20000 | -3 | 135 | 1470 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 20000 | 0 | 0 | 0,05 |
Flugzeugklasse S 3.1b - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 93,0 | 1,2 |
| 2 | 94,0 | 1,2 |
| 3 | 94,0 | 1,2 |
| 4 | 92,0 | 1,2 |
| 5 | 92,0 | 1,1 |
| 6 | 91,0 | 1,0 |
| 7 | 86,0 | 1,0 |
| 8 | 73,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 45 | 0 |
| 3200 | 0 | 90 | 0 |
| 7300 | 0 | 90 | - |
| 7800 | - | 90 | 460 |
| 8300 | -3 | 90 | - |
| 15600 | -3 | 90 | 920 |
| 24600 | -3 | 135 | 1190 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 24600 | 0 | 0 | 0,03 |
Flugzeugklasse S 3.1a/b - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 83,0 | 1,2 |
| 2 | 85,0 | 1,2 |
| 3 | 82,0 | 1,2 |
| 4 | 82,5 | 1,2 |
| 5 | 83,0 | 1,1 |
| 6 | 78,5 | 1,0 |
| 7 | 80,5 | 1,0 |
| 8 | 68,5 | 1,0 |
(3) PF: Landeschwelle
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| -300 | 0 | 67 | 0 |
| 7400 | 0 | 67 | - |
| 8400 | -2,5 | 82 | - |
| X | -2,5 | 98 | h0 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > X | 0 | 0 | 0 |
X = h0 ⋅ cot w - 300
h0 Flughöhe nach Nr. 2.2.2.6 bzw. Nr. 2.2.3.5 VBUF-DES
w Gleitwinkel nach Nr. 2.2.2.3 bzw. Nr. 2.2.3.6 VBUF-DES
Flugzeugklasse S 3.2a - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 96,0 | 1,2 |
| 2 | 97,0 | 1,2 |
| 3 | 97,0 | 1,2 |
| 4 | 95,0 | 1,2 |
| 5 | 95,0 | 1,1 |
| 6 | 94,0 | 1,0 |
| 7 | 89,0 | 1,0 |
| 8 | 76,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 3200 | 0 | 90 | 0 |
| 7300 | 0 | 90 | - |
| 7800 | - | 90 | 460 |
| 8300 | -3 | 90 | - |
| 15600 | -3 | 90 | 920 |
| 24600 | -3 | 135 | 1525 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 21100 | 0 | 0 | 0,055 |
Flugzeugklasse S 3.2b - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 96,0 | 1,2 |
| 2 | 97,0 | 1,2 |
| 3 | 97,0 | 1,2 |
| 4 | 95,0 | 1,2 |
| 5 | 95,0 | 1,1 |
| 6 | 94,0 | 1,0 |
| 7 | 89,0 | 1,0 |
| 8 | 76,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 45 | 0 |
| 3300 | 0 | 90 | 0 |
| 7700 | 0 | 90 | - |
| 8200 | - | 90 | 460 |
| 8700 | -3 | 90 | - |
| 17100 |
(Stand: 20.01.2025)
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