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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
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 1.1 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 94,0 | 1,2 |
| 2 | 100,5 | 1,2 |
| 3 | 100,5 | 1,2 |
| 4 | 98,5 | 1,2 |
| 5 | 95,5 | 1,1 |
| 6 | 91,5 | 1,0 |
| 7 | 87,5 | 1,0 |
| 8 | 72,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 3 | 40 | 0 |
| 1300 | 0 | 80 | 0 |
| 3600 | 0 | 80 | - |
| 4100 | - | 80 | 460 |
| 4600 | -3 | 80 | - |
| 7800 | -3 | 80 | 920 |
| 18800 | -3 | 135 | 1283 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 18800 | 0 | 0 | 0,033 |
Flugzeugklasse S 1.1 - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 76,0 | 1,2 |
| 2 | 78,5 | 1,2 |
| 3 | 80,0 | 1,2 |
| 4 | 78,0 | 1,2 |
| 5 | 75,5 | 1,1 |
| 6 | 77,0 | 1,0 |
| 7 | 77,5 | 1,0 |
| 8 | 65,0 | 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 | 82 | - |
| X | -2 | 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 1.2 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 94,0 | 1,2 |
| 2 | 100,5 | 1,2 |
| 3 | 100,5 | 1,2 |
| 4 | 98,5 | 1,2 |
| 5 | 95,5 | 1,1 |
| 6 | 91,5 | 1,0 |
| 7 | 87,5 | 1,0 |
| 8 | 72,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 3 | 40 | 0 |
| 1400 | 0 | 80 | 0 |
| 3100 | 0 | 80 | - |
| 3600 | - | 80 | 460 |
| 4100 | -3 | 80 | - |
| 6700 | -3 | 80 | 920 |
| 12300 | -3 | 135 | 1120 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 12300 | 0 | 0 | 0,13 |
Flugzeugklasse S 1.2 - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 75,5 | 1,2 |
| 2 | 78,0 | 1,2 |
| 3 | 79,5 | 1,2 |
| 4 | 77,5 | 1,2 |
| 5 | 75,0 | 1,1 |
| 6 | 76,5 | 1,0 |
| 7 | 77,0 | 1,0 |
| 8 | 64,5 | 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 | 67 | - |
| 9300 | -2 | 67 | - |
| X | -2 | 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 1.3 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 96,0 | 1,2 |
| 2 | 102,5 | 1,2 |
| 3 | 102,5 | 1,2 |
| 4 | 100,5 | 1,2 |
| 5 | 97,5 | 1,1 |
| 6 | 93,5 | 1,0 |
| 7 | 89,5 | 1,0 |
| 8 | 74,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 3 | 40 | 0 |
| 1900 | 0 | 80 | 0 |
| 4400 | 0 | 80 | - |
| 4900 | - | 80 | 460 |
| 5400 | -3 | 80 | - |
| 9600 | -3 | 80 | 920 |
| 13000 | -3 | 110 | 960 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 13000 | 0 | 0 | 0,12 |
Flugzeugklasse S 1.3 - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 77,0 | 1,2 |
| 2 | 79,5 | 1,2 |
| 3 | 81,0 | 1,2 |
| 4 | 79,0 | 1,2 |
| 5 | 76,5 | 1,1 |
| 6 | 78,0 | 1,0 |
| 7 | 78,5 | 1,0 |
| 8 | 66,0 | 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 | 67 | - |
| 9300 | -2 | 67 | - |
| X | -2 | 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 2 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 95,5 | 1,2 |
| 2 | 102,0 | 1,2 |
| 3 | 102,0 | 1,2 |
| 4 | 100,0 | 1,2 |
| 5 | 97,0 | 1,1 |
| 6 | 93,0 | 1,0 |
| 7 | 89,0 | 1,0 |
| 8 | 73,5 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 3 | 40 | 0 |
| 1300 | 0 | 80 | 0 |
| 3600 | 0 | 80 | - |
| 4100 | - | 80 | 460 |
| 4600 | -3 | 80 | - |
| 7800 | -3 | 80 | 920 |
| 18800 | -3 | 135 | 1283 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 18800 | 0 | 0 | 0,033 |
Flugzeugklasse S 2 - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 81,0 | 1,2 |
| 2 | 83,5 | 1,2 |
| 3 | 85,0 | 1,2 |
| 4 | 83,0 | 1,2 |
| 5 | 80,5 | 1,1 |
| 6 | 82,0 | 1,0 |
| 7 | 82,5 | 1,0 |
| 8 | 70,0 | 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 | 82 | - |
| X | -2 | 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
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