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Flugzeugklasse S 6.1 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 87,5 | 1,0 |
| 2 | 91,0 | 1,0 |
| 3 | 89,0 | 1,0 |
| 4 | 87,5 | 1,0 |
| 5 | 84,5 | 1,0 |
| 6 | 81,5 | 1,0 |
| 7 | 78,5 | 1,0 |
| 8 | 69,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 1900 | 0 | 90 | 0 |
| 4100 | 0 | 90 | - |
| 4600 | - | 90 | 460 |
| 5100 | -2,5 | - | - |
| 8300 | -2,5 | 120 | 670 |
| 12000 | -2,5 | 135 | 1030 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 12000 | 0 | 0 | 0,135 |
Flugzeugklasse S 6.1 - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 70,5 | 1,0 |
| 2 | 78,5 | 1,0 |
| 3 | 76,0 | 1,0 |
| 4 | 77,5 | 1,0 |
| 5 | 75,0 | 1,0 |
| 6 | 72,0 | 1,0 |
| 7 | 72,5 | 1,0 |
| 8 | 59,0 | 1,0 |
(3) PF: Landeschwelle
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| -300 | 0 | 70 | 0 |
| 7400 | 0 | 75 | - |
| X | -1 | 108 | 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 6.2a - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 92,0 | 1,0 |
| 2 | 95,5 | 1,0 |
| 3 | 93,5 | 1,0 |
| 4 | 92,0 | 1,0 |
| 5 | 89,0 | 1,0 |
| 6 | 86,0 | 1,0 |
| 7 | 83,0 | 1,0 |
| 8 | 73,5 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 1500 | 0 | 85 | 0 |
| 3400 | 0 | 85 | - |
| 3900 | - | 85 | 460 |
| 4400 | -3 | - | - |
| 6500 | -3 | 110 | 650 |
| 11000 | -3 | 135 | 1050 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 11000 | 0 | 0 | 0,145 |
Flugzeugklasse S 6.2b - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 92,0 | 1,0 |
| 2 | 95,5 | 1,0 |
| 3 | 93,5 | 1,0 |
| 4 | 92,0 | 1,0 |
| 5 | 89,0 | 1,0 |
| 6 | 86,0 | 1,0 |
| 7 | 83,0 | 1,0 |
| 8 | 73,5 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 2100 | 0 | 90 | 0 |
| 5000 | 0 | 90 | - |
| 5500 | - | 90 | 460 |
| 6500 | -3 | - | - |
| 9600 | -3 | 120 | 720 |
| 15900 | -3 | 140 | 1200 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 15900 | 0 | 0 | 0,107 |
Flugzeugklasse S 6.2a/b - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 73,0 | 1,0 |
| 2 | 81,0 | 1,0 |
| 3 | 79,0 | 1,0 |
| 4 | 80,0 | 1,0 |
| 5 | 77,5 | 1,0 |
| 6 | 74,5 | 1,0 |
| 7 | 75,0 | 1,0 |
| 8 | 61,5 | 1,0 |
(3) PF: Landeschwelle
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| -300 | 0 | 73 | 0 |
| 7400 | 0 | 77 | - |
| X | -1 | 108 | h0 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > X | 0 | 0 | 0 |
(Stand: 20.01.2025)
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