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Flugzeugklasse S 5.3 - Ab

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 89,0 1,0
2 93,0 1,0
3 93,5 1,0
4 92,0 1,0
5 89,0 1,0
6 85,5 1,0
7 78,5 1,0
8 70,0 1,0

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
2.000 0 85 0
4.400 0 85 -
4.900 - 85 460
5.400 -2 - -
8.100 -2 115 610
11.600 -2 135 830
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 11.600 0 0 0,117

Flugzeugklasse S 5.3 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 72,5 1,0
2 76,5 1,0
3 77,0 1,0
4 75,5 1,0
5 72,5 1,0
6 69,0 1,0
7 62,0 1,0
8 53,5 1,0

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
-300 0 68 0
7.400 0 72 -
X -1 108 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> x 0 0 0

X = ho · cot w - 300

ho 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 6.1 - Ab

Datenblatt

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

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
1.900 0 90 0
4.100 0 90 -
4.600 - 90 460
5.100 -2,5 - -
8.300 -2,5 120 670
12.000 -2,5 135 1 030
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 12.000 0 0 0,135

Flugzeugklasse S 6.1 - An

Datenblatt

n (1)
On
[dB]		 (2)
Rn
1 70,5 1,0
2 78,5 1,0
3 76,5 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

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 70 0
7.400 0 75 -
X -1 108 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> x 0 0 0

X = ho · cot w - 300

ho 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 6.2 a) - Ab

Datenblatt

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

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
1.500 0 85 0
3.400 0 85 -
3.900 - 85 460
4.400 -3 - -
6.500 -3 110 650
11.000 -3 135 1.050
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 11.000 0 0 0,145

Flugzeugklasse S 6.2 b) - Ab

Datenblatt

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

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
2.100 0 90 0
5.000 0 90 -
5.500 - 90 460
6.500 -3 - -
9.600 -3 120 720
15.900 -3 140 1.200
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 15.900 0 0 0,107

Flugzeugklasse S 6.2 a/b) - An

Datenblatt

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

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
-300 0 73 0
7 400 0 77 -
X -1 108 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho · cot w - 300

ho 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

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

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
2.800 0 90 0
7.200 0 90 -
7.700 - 90 460
8.200 -2 - -
18.700 -2 140 700
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 18.700 0 0 0,075

Flugzeugklasse S 6.3 - An

Datenblatt

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

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 73 0
7.400 0 77 -
X -1 108 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> x 0 0 0

X = ho · cot w - 300

ho 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 7 a) - Ab

Datenblatt

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

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
1.800 0 90 0
4.700 0 90 -
5.200 - 90 460
5.700 -4,5 - -
15.300 -4,5 140 1.080
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 15.300 0 0 0,102

Flugzeugklasse S 7 b) - Ab

Datenblatt

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

so = 300 m

(3) PF: Startpunkt

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 40 0
2.600 0 100 0
6.600 0 100 -
7.100 - 100 460
7.600 -4,5 - -
21.300 -4,5 150 1.140
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> 21.300 0 0 0,084

Flugzeugklasse S 7 a/b) - An

Datenblatt

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

so = 300 m

(3) PF: Landeschwelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
- 300 0 73 0
7.400 0 77 -
X -1 108 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho cotw-300

ho 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

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

so = 150 m

(3) PF: Hubschrauberstart- und -landestelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 30 0
X 0 30 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho / 0,2

ho Höhenangabe 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

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

so=150m

(3) PF: Hubschrauberstart- und -landestelle

σ"
[m]		 (4)
Z
[dB]		 (5)
V
[m/s]		 (6)
H
[m]
0 0 30 0
X 0 30 ho
σ"
[m]		 dZ/dσ"
[dB/m]		 dV/dσ"
[s-1]		 dH/dσ"
> X 0 0 0

X = ho / 0,2

ho Höhenangabe nach Nr. 2.2.7.5, Nr. 2.2.8.5 bzw. Nr. 2.2.9.5 VBUF-DES

UWS Umweltmanagement GmbH . Frame öffnen