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Flugzeugklasse P 2.1 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 87,0 | 1,0 |
| 2 | 85,5 | 1,0 |
| 3 | 81,5 | 1,0 |
| 4 | 77,0 | 1,0 |
| 5 | 73,5 | 1,0 |
| 6 | 69,5 | 1,0 |
| 7 | 69,5 | 1,0 |
| 8 | 64,5 | 1,0 |
(3) PF: Startpunkt
| σ"[m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 35 | 0 |
| 900 | 0 | 70 | 0 |
| 3800 | 0 | 70 | - |
| 4300 | - | 70 | 310 |
| 4800 | -2 | 70 | 340 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 4800 | 0 | 0 | 0,06 |
Flugzeugklasse P 2.1 - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 77,5 | 1,0 |
| 2 | 72,0 | 1,0 |
| 3 | 73,5 | 1,0 |
| 4 | 74,5 | 1,0 |
| 5 | 71,0 | 1,0 |
| 6 | 69,5 | 1,0 |
| 7 | 71,5 | 1,0 |
| 8 | 60,5 | 1,0 |
(3) PF: Landeschwelle
| σ"[m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| -300 | 0 | 60 | 0 |
| X - 1000 | 0 | 60 | - |
| X | 5 | 70 | 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 P 2.2 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 94,5 | 1,0 |
| 2 | 93,0 | 1,0 |
| 3 | 89,0 | 1,0 |
| 4 | 84,5 | 1,0 |
| 5 | 81,0 | 1,0 |
| 6 | 77,0 | 1,0 |
| 7 | 77,0 | 1,0 |
| 8 | 72,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 35 | 0 |
| 900 | 0 | 70 | 0 |
| 3800 | 0 | 70 | - |
| 4300 | - | 70 | 310 |
| 4800 | -2 | 70 | 340 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 4800 | 0 | 0 | 0,06 |
Flugzeugklasse P 2.2 - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 77,5 | 1,0 |
| 2 | 72,0 | 1,0 |
| 3 | 73,5 | 1,0 |
| 4 | 74,5 | 1,0 |
| 5 | 71,0 | 1,0 |
| 6 | 69,5 | 1,0 |
| 7 | 71,5 | 1,0 |
| 8 | 60,5 | 1,0 |
(3) PF: Landeschwelle
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| -300 | 0 | 60 | 0 |
| X - 1000 | 0 | 60 | - |
| X | 5 | 70 | 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 1.0 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 82,0 | 1,0 |
| 2 | 85,5 | 1,0 |
| 3 | 83,5 | 1,0 |
| 4 | 82,0 | 1,0 |
| 5 | 79,0 | 1,0 |
| 6 | 76,0 | 1,0 |
| 7 | 73,0 | 1,0 |
| 8 | 63,5 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 1100 | 0 | 75 | 0 |
| 5100 | 0 | 75 | - |
| 5600 | - | 75 | 460 |
| 6100 | -1 | - | - |
| 10400 | -1 | 110 | 650 |
| 15000 | -1 | 135 | 1000 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 15000 | 0 | 0 | 0,126 |
Flugzeugklasse S 1.0 - An
(Stand: 20.01.2025)
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