| | |
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 |
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 6.3 - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 88,0 | 1,0 |
| 2 | 91,5 | 1,0 |
| 3 | 89,5 | 1,0 |
| 4 | 88,0 | 1,0 |
| 5 | 85,0 | 1,0 |
| 6 | 82,0 | 1,0 |
| 7 | 79,0 | 1,0 |
| 8 | 69,5 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 2800 | 0 | 90 | 0 |
| 7200 | 0 | 90 | - |
| 7700 | - | 90 | 460 |
| 8200 | -2 | - | - |
| 18700 | -2 | 140 | 700 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 18700 | 0 | 0 | 0,075 |
Flugzeugklasse S 6.3 - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 69,0 | 1,0 |
| 2 | 77,0 | 1,0 |
| 3 | 75,0 | 1,0 |
| 4 | 76,0 | 1,0 |
| 5 | 73,5 | 1,0 |
| 6 | 70,5 | 1,0 |
| 7 | 71,0 | 1,0 |
| 8 | 57,5 | 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 |
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 7a - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 95,5 | 1,0 |
| 2 | 99,0 | 1,0 |
| 3 | 97,0 | 1,0 |
| 4 | 95,5 | 1,0 |
| 5 | 92,5 | 1,0 |
| 6 | 89,5 | 1,0 |
| 7 | 86,5 | 1,0 |
| 8 | 77,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 1800 | 0 | 90 | 0 |
| 4700 | 0 | 90 | - |
| 5200 | - | 90 | 460 |
| 5700 | -4,5 | - | - |
| 15300 | -4,5 | 140 | 1080 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 15300 | 0 | 0 | 0,102 |
Flugzeugklasse S 7b - Ab
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 95,5 | 1,0 |
| 2 | 99,0 | 1,0 |
| 3 | 97,0 | 1,0 |
| 4 | 95,5 | 1,0 |
| 5 | 92,5 | 1,0 |
| 6 | 89,5 | 1,0 |
| 7 | 86,5 | 1,0 |
| 8 | 77,0 | 1,0 |
(3) PF: Startpunkt
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 40 | 0 |
| 2600 | 0 | 100 | 0 |
| 6600 | 0 | 100 | - |
| 7100 | - | 100 | 460 |
| 7600 | -4,5 | - | - |
| 21300 | -4,5 | 150 | 1140 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > 21300 | 0 | 0 | 0,084 |
Flugzeugklasse S 7a/b - An
Datenblatt s0 = 300 m
| n | (1) On [dB] | (2) Rn |
| 1 | 73,5 | 1,0 |
| 2 | 81,5 | 1,0 |
| 3 | 79,5 | 1,0 |
| 4 | 80,5 | 1,0 |
| 5 | 78,0 | 1,0 |
| 6 | 75,0 | 1,0 |
| 7 | 75,5 | 1,0 |
| 8 | 62,0 | 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 |
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 H 1 - Ab/An
Datenblatt s0 = 150 m
| n | (1) On [dB] | (2) Rn |
| 1 | 77,0 | 1,4 |
| 2 | 73,0 | 1,4 |
| 3 | 76,0 | 1,4 |
| 4 | 76,0 | 1,4 |
| 5 | 71,0 | 1,4 |
| 6 | 65,0 | 1,4 |
| 7 | 57,0 | 1,4 |
| 8 | 55,0 | 1,4 |
(3) PF: Hubschrauberstart- und -landestelle
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 30 | 0 |
| X | 0 | 30 | h0 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > X | 0 | 0 | 0 |
X = h0/0,2
h0 Flughöhe nach Nr. 2.2.7.5, Nr. 2.2.8.5 bzw. Nr. 2.2.9.5 VBUF-DES
Flugzeugklasse H 2 - Ab/An
Datenblatt s0 = 150 m
| n | (1) On [dB] | (2) Rn |
| 1 | 87,0 | 1,4 |
| 2 | 83,0 | 1,4 |
| 3 | 86,0 | 1,4 |
| 4 | 86,0 | 1,4 |
| 5 | 81,0 | 1,4 |
| 6 | 75,0 | 1,4 |
| 7 | 67,0 | 1,4 |
| 8 | 65,0 | 1,4 |
(3) PF: Hubschrauberstart- und -landestelle
| σ" [m] | (4) Z [dB] | (5) V [m/s] | (6) H [m] |
| 0 | 0 | 30 | 0 |
| X | 0 | 30 | h0 |
| σ" [m] | dZ/dσ" [dB/m | dV/dσ" [s-1] | dM/dσ" |
| > X | 0 | 0 | 0 |
X = h0/0,2
h0 Flughöhe nach Nr. 2.2.7.5, Nr. 2.2.8.5 bzw. Nr. 2.2.9.5 VBUF-DES
| | |