Propellerflugzeuge, Motorsegler und Tragschrauber bis 8'618kg MTOM
Annex II
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Luftfahrtentwicklung
17.03.2020 Seite 1 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
567
1.882300
76.0Continental A-65-8 Sensenich
74CK-0-74Univair J-3 Exhaust System
Aeronca Aircraft Corporation
11AC
// D
2300 /
/ 63.8
300
1.412045
65.0Alisport Srl. A302efi Alisport Srl.
MonoplanaOriginal
Alisport Srl.
Silent II
// D
2045 /
/ 59.9
313.5
1
22.0
4500
65.0LZ Design D.O.O. EFI LZ Design D.O.O.
EFI-SIL-P15-100
Alisport Srl.
Silent II electro
// D22.0
4500 /
/
noise level set to limit
65.0
554
1.88
66.8
2475
76.0Continental C-90-8F Sensenich
M76AK-2-46
American Champion Aircraft Corp
7AC
68.0 /61.9 / D
/
/
748
1.75
74.9
2650
79.1Continental O-200-A McCauley
1A100/ACM6948Andere
American Champion Aircraft Corp
7ECA
70.0 /66.0 / C
/
/
750
1.88
111.4
2700
79.1Lycoming O-320-A2B McCauley
1A170/7448Frankfurter
American Champion Aircraft Corp
7GCB
70.0 /68.0 / C
/
/
612
1.782490
76.3Rolls-Royce O-200-A MT-Propeller
MT 178R 110-2C
American Champion Aircraft Corp
7AC CONV
68.2 /66.5 / B
/
/
840
1.88
100.3
2500
80.8Lycoming O-290-D2 McCauley
1A170/GM7450
Auster
V
71.2 /71.6 / A
/
/
840
1.88
100.3
2500
Lycoming O-290-D2 McCauley
1A170/GM7448
Auster
V
71.2 /71.6 / A
/
/
840100.3
2500
Lycoming O-290-3 Hordern Richmond Aircra
HRA 53G
Auster
V
// -
/
/
LK A
450
1.745800
65.0Rotax 912 ULS AutoGyro
HTC 3B R (15°)ROTAX
AutoGyro
MTOsport
// D
5800 /
/ 64.9
1090
2.01
102.3
2300
84.5Gipsy 10-1-1 Fairey
A 66696
Beagle
A61 SRS.2
74.5 /65.5 / D
/
/
975
1.88
111.4
2600
82.9Franklin 6A4-150-B3 McCauley
1A170/DM7456
Binder
14-13-3
73.0 /71.6 / B
/
/
680
1.79
66.8
2475
77.8Continental C-90-12F McCauley
1B90/CM7150
Binder
CP301S
69.1 /64.3 / C
/
/
680
1.78
67.0
2475
77.8Continental C-90-12F Hoffmann
HO 14 HM-A 178 120Liese D76
Binder
CP301S "SMARAGD
// D67.0
2475 /
/ 66.4
680
1.7
74.9
2680
77.8Continental O-200-A McCauley
1A100/MCM6758
Binder
CP301S "SMARAGD"
69.1 /67.3 / B
/
/
680
1.83
66.8
2475
77.8Continental C-90-12F Hoffmann
F-H2LC1418311
Binder
CP301S "SMARAGD"
69.1 /70.3 / A
/
/
17.03.2020 Seite 2 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
1452
2.432050
88.0Pratt & Whitney R-985-AN-14B Hartzell
HC-B3R30-4
Boeing
E75
79.4 /73.0 / D
/
/
670
2
106.3
2350
77.5Hirth HM 504 A2 Hoffmann
HO-01-188 112Frankfurter FTF60
Bücker
131
68.9 /65.6 / C
/
/
670
1.88
111.4
2600
77.5Lycoming IO-320-E2A Hoffmann
HO-23-188 125MécanAir
Bücker
131
68.9 /67.7 / B
/
/
670
1.88
111.8
2700
77.5Lycoming IO-320-E2A Hoffmann
HO-23A-188125MécanAir
Bücker
131
// C111.8
2700 /
/ 70.8
670
1.88
111.8
2700
77.5Lycoming IO-320-E2A Hoffmann
HO-23A-188125
Bücker
131
// -111.8
2700 /
/
Considered to comply with requirements by virtue of early TC date without the need to determine ist noise level.Lärmklasse A
670
1.88
106.3
2350
77.5Hirth HM 504 A2 Hoffmann
HO-01-188 112Original
Bücker
131
68.9 /65.6 / C
/
/
670
1.89
111.8
2700
77.5Lycoming IO-320-E2A Hoffmann
HO 23-188 125MécanAir
Bücker
131
// C111.8
2700 /
/ 70.8
670
2
106.3
2350
77.5Hirth HM 504 A2 K+W Thun
D200/S111Frankfurter FTF60
Bücker
131
68.9 /65.6 / C
/
/
670
1.88
111.8
2700
77.5Lycoming IO-320-E2A MT-Propeller
MT 188R125-3EMécanAir
Bücker
131
// C111.8
2700 /
/ 70.8
670
1.89
119.3
2700
77.5Lycoming IO-320-E2A Hoffmann
HO-23A-188125Frankfurter
Bücker
131
// C119.3
2700 /
/ 69.7
670
1.88
119.3
2700
77.5Lycoming AEIO-320-E2A MT-Propeller
MT 188R125-3EFrankfurter
Bücker
131
// C119.3
2700 /
/ 69.7
670
2
106.3
2350
77.5Hirth HM 504 A2 K+W
D200/2111Original
Bücker
131
68.9 /65.6 / C
/
/
675
2.05
111.8
2700
77.7Lycoming O-320-A2B Hoffmann
F-H2/LC23-205 125 7,5RFrankfurter FTT60
Bücker
131
// D111.8
2700 /
/ 66.5
680
1.92
59.7
2300
77.8Letecke Zadody NP Walter Minor 4-III Zbinden
V-406ZFrankfurter
Bücker
131
69.1 /59.1 / D
/
/
680
1.92
59.7
2300
77.8Letecke Zadody NP Walter Minor 4-III Zbinden/Schneider
ZS 02-23Frankfurter
Bücker
131
69.1 /59.1 / D
/
/
670
1.882600
77.5Lycoming AIO-320-C1B Hoffmann
HO-23-188 125Schels
Bücker
131 APM
68.9 /64.5 / C
2600 /
/
640
2.15
95.2
2050
76.9Bramo SH-14A4 Hoffmann
HO-52-215-148
Bücker
133
68.5 /63.0 / D95.2
2050 /
/ 68.0
17.03.2020 Seite 3 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
640
2.2
95.2
2050
76.9Bramo SH-14A4 K+W
D220/S148
Bücker
133
68.5 /63.0 / D
/
/
640
2.2
148.9
2420
76.9Lycoming AIO-360-B1B Hoffmann
HO27HM200160
Bücker
133 BM
68.5 /71.0 / A
/
/
640
2
148.9
2420
76.9Lycoming AIO-360-B1B MT-Propeller
MT 188R150 4GFrankfurter
Bücker
133 BM
// D148.9
2420 /
/ 68.2
640
1.882300
76.9Lycoming AEIO-360-B2F MT-Propeller
188R150-4GBitz Augsburg + Liese Dämpfer
Bücker
133 C
// D
2300 /
/ 66.8
850
1.88
62.0
2300
80.9Hirth HM 500 A-1 Hoffmann
HOCO-F-H2-1881127 HO 1 RZOriginal
Bücker
181 B1
71.3 /63.8 / D62.0
2300 /
/
850
1.88
62.0
2300
80.9Hirth HM 504 A-2 Hoffmann
HO 01-188 112Original
Bücker
181 B1
71.3 /63.8 / D62.0
2300 /
/
720
2.11
92.1
1850
78.6Tigre G-IV-A()() Empresa
HC 212.111
C.A.S.A.
1.131-E S.2000
69.6 /69.4 / B92.4
1850 /
/
720
2.11
111.8
2300
78.6Tigre G-IV-BE MT-Propeller
MT 211 R 132-6V
C.A.S.A.
1.131-E S.2000
// C111.8
2300 /
/ 70.7
720
1.8
134.2
2500
78.6Lycoming AEIO-360-B2F Hoffmann
HO-27HM-180160Griener
C.A.S.A.
1.131-E S.2000
// D134.2
2500 /
/ 68.2
720
2.11
92.1
1850
78.6Tigre G-IV-A()() MT-Propeller
MT 211 R 162-6V
C.A.S.A.
1.131-E S.2000
69.6 /69.4 / B92.4
1850 /
/
720
1.88
127.5
2500
78.6Lycoming IO-360-B2F MT-Propeller
MT 188R130-4GGriener
C.A.S.A.
1.131-E S.2000
// D134.2
2700 /
/ 66.4
720
2.11
111.8
2300
78.6Tigre G-IV-B MT-Propeller
MT 211 R 132-6VOriginal
C.A.S.A.
1.131-E S.2000
69.6 /67.8 / B111.8
2300 /
/
720
1.8
132.0
2500
78.6Lycoming AEIO-360-B2F Hoffmann
HO-27HM-180160Bitz mit Dämmelement Liese R74
C.A.S.A.
1.131-E S.2000
// D132.0
2500 /
/ 65.1
720
2.11
93.2
1850
78.6Tigre G-IV-A()() Empresa
HC 212.111Bitz BI-L-CA-125/150
C.A.S.A.
1.131-E S.2000
// D93.2
1850 /
/ 69.7
720
2.11
111.8
2300
78.6Tigre G-IV-BE Empresa
HC 212.111Bitz BI-L-CA-125/150
C.A.S.A.
1.131-E S.2000
// D111.8
2300 /
/ 67.5
720
1.93
134.2
2700
78.6Lycoming IO-360-B1E Sensenich
W76MZ/60Gomolzig
C.A.S.A.
1.131-E S.2000
// A134.2
2700 /
/
Krybus-Modification. Christen Rückenflug-Ölsystem.
74.1
660
1.8
80.0
2600
77.3Lycoming O-235-K2A Hoffmann
HO-14-178-115
Cessna Aircraft Company
140
68.8 /70.4 / A
/
/
660
1.8
63.8
2500
Continental C-85-12F McCauley
1B90/CF7148
Cessna Aircraft Company
140
68.8 /70.4 / A
/
/
17.03.2020 Seite 4 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
660
1.879
67.0
2350
77.3Continental C-90-12F Sensenich
M76-AK
Cessna Aircraft Company
140
68.8 /65.3 / C
/
/
660
1.8
63.8
2500
77.3Continental C-85-12F McCauley
1A90/CF7150
Cessna Aircraft Company
140
68.8 /70.4 / A
/
/
660
1.75
74.9
2750
77.3Cont./Rolls-Royce O-200-A Sensenich
M69CK52
Cessna Aircraft Company
140
68.8 /69.0 / A
/
/
660
1.8
80.0
2600
77.3Lycoming O-235-K2A Sensenich
72CK-0-56
Cessna Aircraft Company
140
68.8 /70.4 / A
/
/
680
1.8
66.8
2475
77.8Continental C-90-12F McCauley
1B90/CM7146
Cessna Aircraft Company
140 A
69.1 /66.5 / C
/
/
998
1.952450
83.2Lycoming O-360-A4M Sensenich
76EM8S5-0-60
Cessna Aircraft Company
170 A
73.3 /66.1 / D
2450 /
/
998
1.82
126.6
2700
83.2Lycoming O-340-A1A Hartzell
HC-A2XL-1
Cessna Aircraft Company
170 A
73.3 /71.6 / B
/
/
998
1.952450
83.2Lycoming O-360-A3A Sensenich
76EM8S5-0-60
Cessna Aircraft Company
170 B
73.3 /66.1 / D
2450 /
/
998
1.88
133.7
2700
83.2Lycoming O-360-A1A Hartzell
HC-C2YK-1
Cessna Aircraft Company
170 B
73.3 /71.9 / B
/
/
998
1.93
109.6
2700
83.2Continental O-300-A McCauley
1A170/DM7653Liese 2 x D76
Cessna Aircraft Company
170,-A,-B
// D109.6
2700 /
/ 73.2
998
1.93
109.6
2700
83.2Continental C-145-2 McCauley
1A170/DM7653Liese 2 x D76
Cessna Aircraft Company
170,-A,-B
// D109.6
2700 /
/ 73.2
1000
1.93
108.4
2580
83.2Continental C-145-2 McCauley
1A170/DM7653
Cessna Aircraft Company
170,-A,-B
73.3 /72.2 / B
/
/
472.5
1.72140
65.0Rotax 912 Kievprop
BB 263/1700Heggemann
Comco
Ikarus C 42 B
// D
2140 /
/
Prop.: 22° bei 400mm ab Nabe
58.8
472.5
1.85800
65.0Rotax 912 S Neuform
CR3-V-80-R2HHeggemann
Comco
Ikarus C 42 B
// D
5800 /
/ 62.1
472.5
1.7475800
65.0Rotax 912 S Neuform
CR3-75Heggemann
Comco
Ikarus C 42 B
// D
5800 /
/
Prop.: 27° bei 365 mm ab Propmitte
57.5
900
2.13
104.3
2050
81.7Armstrong GENET MAJOR Hoffmann
HO53-213B126
Comte
AC-4
72.0 /69.5 / C
/
/
952
1.98
108.1
2400
82.5Gipsy MAJOR 10MK2 Hoffmann
HO-21-198B-140L
De Havilland
DHC 1MK 20 "Chipmunk"
// D108.1
2400 /
/ 68.1
17.03.2020 Seite 5 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
952
2.04
104.3
2400
82.5Gipsy MAJOR 10MK2 Fairey
FR-A-66 753
De Havilland
DHC 1MK 22
72.7 /70.0 / C
/
/
1000
2.06
104.3
2400
83.2Gipsy MAJOR 10M 2 Fairey
A66753Andere
De Havilland
DHC 1MK 22
73.3 /71.9 / B
/
/
1000
2.04
104.3
2400
83.2Gipsy MAJOR 10MK2 Fairey
A66753
De Havilland
DHC 1MK 22
73.3 /72.9 / B
/
/
3629
2.62200
88.0Pratt & Whitney PT6A-34 Hartzell
B3TN-3DY/T10282
De Havilland
DHC-3
80.0 /84.0 / A
2200 /
/
795
2.08
82.0
2000
80.0Gipsy MAJOR I De Havilland
5234/HX8
De Havilland
DH 60 C
70.6 /64.0 / D
/
/
828
1.98
108.4
2060
80.6Gipsy MAJOR 10MK2 Hoffmann
HO21-198B140
De Havilland
DH 82 A
71.0 /63.5 / D
/
/
828
1.93
82.0
2100
80.6Gipsy MAJOR 1C De Havilland
DH5220/H
De Havilland
DH 82 A
71.0 /64.1 / D
/
/
828
1.98
82.0
2100
80.6Gipsy MAJOR 1H Hoffmann
HO 21-HM194B 140LK
De Havilland
DH 82 A
71.0 /60.0 / D
/
/
828
1.98
104.4
2100
80.6Gipsy MAJOR 1 Hoffmann
HO21-198B140L
De Havilland
DH 82 A
// D104.4
2100 /
/ 68.4
828
1.98
82.0
2100
80.6Gipsy MAJOR 1C Hoffmann
HO 21-HM194B 142LK
De Havilland
DH 82 A (N.Z.)
71.0 /60.0 / D
/
/
828
1.98
82.0
2100
80.6Gipsy MAJOR 1C Hoffmann
HO 21-HM198B 140L
De Havilland
DH 82 A (N.Z.)
71.0 /60.0 / D
/
/
839
2.1
82.0
2100
80.7Gipsy MAJOR I DRG Propellers
67104
De Havilland
DH-82A
71.2 /69.0 / C
/
/
1850
2.36
253.2
2181
88.0Lycoming GSO-48OB1B6 Hartzell
HC-93Z20-2CLFrankfurter
Dornier
DO-27-H2
80.0 /75.4 / C
/
/
1850
2.36
238.0
2053
88.0Lycoming GSO-480B1B6 Hartzell
HC-93Z20-2C1Frankfurter FFT 60
Dornier
DO-27-H2
80.0 /72.3 / D
/
/
1850
2.49
194.0
3000
88.0Lycoming GO-480-B1A6 Hartzell
HC-A2MV20-1A/V10133()-3Liese 2x76x300-L
Dornier
DO-27-Q5
// D194.0
3000 /
/ 81.0
1850
2.49
194.0
3000
88.0Lycoming GO-480-B Hartzell
HC-82x20-1BLiese 2x76x300-L
Dornier
DO-27-Q5
// D
3000 /
/ 81.4
450
1.725800
65.0Rotax 914 UL2 DUC
Flash 2Florian Raboud J-RO AlpineGyro
DTA sas
J-RO AlpineGyro
// D
5800 /
/
Prop.pitch: 24.5°
62.4
17.03.2020 Seite 6 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
520
1.725800
65.0Rotax 914 UL2 DUC
Flash 2Florian Raboud J-RO AlpineGyro
DTA sas
J-RO AlpineGyro
// D
5800 /
/
Prop.pitch: 24.5°
64.7
472.5
1.64
84.0
5700
65.0Rotax 914 UL2 MT-Propeller
MTV-34-1-A/164-200ROTAX P/N 979406
Dyn-Aero
MCR-ULC
// D84.0
5700 /
/ 64.2
472.5
1.56
84.0
2366
65.0Rotax 914 UL2 Dyn'Aero
MKIHE 1000Original
Dyn-Aero
MCR-ULC
// D84.0
2366 /
/ 61.4
472.5
1.64
84.0
5700
65.0Rotax 914 UL3 MT-Propeller
MTV-34-1-A/164-200ROTAX P/N 979406
Dyn-Aero
MCR-ULC
// D84.0
5700 /
/ 64.2
472.5
1.56
84.0
2366
65.0Rotax 914 UL2 Neuform
DR3-56-47-101.6Original
Dyn-Aero
MCR-ULC
// D84.0
2366 /
/ 61.4
3100 88.0Hispano-Suiza HS 12Y51 Escher-Wyss
E-W V7
Eidg. Flugzeugwerk
C-3603
// -
/
/
Considered to comply with requirements by virtue of early TC date without the need to determine ist noise level.
3700
3.05
819.8
1693
88.0Lycoming T53L7A Hamilton
53C51-23
Eidg. Flugzeugwerk
C-3605
// D819.8
1693 /
/ 74.5
450
1.725800
65.0Rotax 914 UL2 DUC
Flash 2Florian Raboud J-RO AlpineGyro
ELA Aviacion S.L
ELA 10 Eclipse
// D
5800 /
/
Prop.pitch: 22.5°
62.3
572
1.8
66.8
2475
76.0Continental C-90-12F McCauley
1A90/CF7144
Ercoupe
415 C
68.0 /68.7 / A
/
/
635
1.8
66.8
2450
76.8Continental C-90-12F McCauley
1A90/CF7144MSW
Ercoupe
415 D
68.5 /59.6 / D
/
/
472.5
1.735800
65.0Rotax 912 S DUC
Swirl 174Evektor E604-1001
Evektor
EV 97 Modell 2000 R
// D
5800 /
/
Prop.: 24° bei 20cm von Blattspitze
57.9
472.5
1.725800
65.0Rotax 912 S Woodcomp
Classic 170/3/REvektor E604-1001
Evektor
EV 97 Modell 2000 R
// D
5800 /
/
Prop.: 22° bei r=51cm ab Blattwurzel
58.2
575
1.78
53.0
2300
76.0Continental C-90-8F Warp
Warp Drive
Experimental
PELICAN CLUB GS
// C53.0
2300 /
/
Propellereinstellung 8°
68.5
544117.6
2500
76.0Lycoming O-320-D1A MT-Propeller
MTV-18-C/175-36Communication Tech. CT-DF 02.020-60/Er
Experimental
Van's RV-3A
// C117.6
2500 /
/ 67.7
366
1.56
44.8
2750
76.0Hapi 212 (VW 1835) Arplast
4TGE/2Eigenbau
Experimental
Sonerai I
// A44.8
2750 /
/ 69.0
328
1.35
48.0
5600
76.0Hirth F23A Nater
VKN-V 130 LD
Experimental
Marco J5
// D48.0
5600 /
/ 63.7
17.03.2020 Seite 7 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
499
1.3713200
70.0Jabiru 3300 Sensenich
W54SK-64GJabiru
Experimental
Sonex Waiex
// A
3200 /
/
VEL Art. 2 (Kunstflug)
71.8
580
1.78
66.8
2280
76.0Continental C-90-8F Hoffmann
HO-14-178-120
Experimental
AERO 101
68.0 /70.4 / A
/
/
580
1.93
66.8
2280
76.0Continental C-90-8F Sensenich
W76CK42
Experimental
AERO 101
68.0 /70.4 / A
/
/
560
1.815800
70.0Rotax 914 UL FD-Composites
FDP-01Florian Raboud J-RO AlpineGyro
Experimental
FD-Composite AC10
// C
5800 /
/
Prop.pitch: 15.3°
68.0
580
1.744
73.5
5000
70.3Rotax 912 ULS Warp
Warp Drive 68"Heggemann Breezer
Experimental
Aerostyle Breezer
// D73.5
5000 /
/ 60.0
580
1.7
72.0
2200
76.0BMW R 1100 S Woodcomp
SR2000Aerostyle
Experimental
Aerostyle Breezer
// C72.0
2200 /
/ 67.4
580
1.68
73.5
5100
70.3Rotax 912 ULS Woodcomp
SR200
Experimental
Aerostyle Breezer
// D73.5
5100 /
/ 64.0
640
1.75700
71.8Rotax 912 ULS Neuform
CR3-V70-R2HCKT Titan/Breezer
Experimental
Aerostyle Breezer 600
// D
5700 /
/ 68.0
640
1.75500
71.8Rotax 912 ULS Neuform
CR3-V70-R2HCKT Titan/Breezer
Experimental
Aerostyle Breezer 600
// D
5650 /
/
Maximum take-off power limited to 5560 RPM
65.3
400
1.62
38.5
2326
76.0Rotax 462 Arplast
162 DAM F4ROTAX BRD
Experimental
AFM-01
// D38.5
2326 /
/ 63.4
540
1.625500
70.0Rotax 912 UL2 Arplast
PV50Millioud Olivier 4 en 1
Experimental
Andromède
// A
5500 /
/ 69.0
413
1.8
48.6
2325
76.0Rotax 532LC Perry
71-37
Experimental
AVID FLYER
68.0 /55.9 / D48.6
2325 /
/
492
1.53
61.8
2900
76.0Mosler 82-X Arplast
153Eigenbau
Experimental
AVID FLYER MK IV
// D61.8
2900 /
/ 65.2
521
1.737500
76.0Mid-West Aero Eng. AE100R DUC
Swirl 174Chabbord Mid West Engine
Experimental
AVID FLYER MK IV
// A
7500 /
/
Propeller pitch: 26°
72.4
521
1.75800
70.0Rotax 912 ULS Arplast
Ecoprop 4T DE 3Original
Experimental
AVID FLYER MK IV
// D
5800 /
/ 63.7
521
1.7
73.0
5400
76.0Mid-West Aero Eng. AE100R Arplast
PV50-3
Experimental
AVID FLYER MK IV
// C73.0
5400 /
/ 66.8
17.03.2020 Seite 8 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
522
1.8
55.1
2333
76.0Rotax 618 IVO
adjustable
Experimental
AVID FLYER MK IV STOL
// D55.1
2333 /
/ 65.4
476
1.66
57.5
2332
76.0Rotax 912 UL Arplast
175 DWAP
Experimental
Avid Mk IV Speedwing
// D59.6
2420 /
/ 63.9
492
1.74
59.7
2220
76.0Rotax 912 Arplast
175 DWAM
Experimental
AVID HAULER
// D59.7
2220 /
/ 61.6
492
1.765000
70.0Göbler-Hirth F30A IVOPROP
L372 HP
Experimental
AVID HAULER
// A
5000 /
/ 69.0
492
1.76
48.6
2000
76.0Rotax 582LC Warp
Warp Drive
Experimental
AVID HAULER
// C48.6
2000 /
/ 66.1
492
1.562750
70.0Jabiru 2200 Woodcomp
SR 35J
Experimental
AVID HAULER
// D
2750 /
/ 65.1
492
1.81
47.6
2450
76.0Rotax 532LC Perry
71-37
Experimental
AVID HAULER
// D47.6
2450 /
/ 64.9
492
1.72
55.2
2200
76.0Rotax 618 DUC
PA 100G33B 20-12-99
Experimental
AVID HAULER 1e
// A55.2
2200 /
/
Blattspitzen gebogen
70.9
750
1.93
134.2
2550
79.1Lycoming O-360-A3A Sensenich
76EM8S5-0-60Liese
Experimental
AVID Magnum
// C134.2
2550 /
/ 71.6
544
1.79
66.8
2475
76.0Continental C-90-8F Flottorp
72A48
Experimental
BREEZY RLU-1
68.0 /67.1 / B
/
/
793
1.76
132.0
2077
75.1Mazda Wankel Rotary 13B IVOPROP
MagnumMotiv Air STDMTV / ML372PQ26T
Experimental
BREEZY RLU-1
// D132.0
2077 /
/ 71.0
545
1.453000
76.0Limbach L 2000 EB1.B Hoffmann
HO-V62R-L-150AAndere
Experimental
BX-2
68.0 /69.8 / A59.6
3400 /
/
550
1.6
60.4
2553
76.0Rotax 912 UL MT-Propeller
MTV-1-AR-160-03Beninger/D'Epagnier
Experimental
BX-2
// A60.4
2553 /
/ 70.6
550
1.6
73.0
5225
70.0Rotax 912 ULS2 Woodcomp
SR2000/3Rotax/Aerotec
Experimental
BX-2
// D73.0
5225 /
/ 64.0
550
1.68
58.8
2332
76.0Rotax 912 Arplast
ARPLAST Ecoprop
Experimental
BX-2
// D60.4
2551 /
/ 64.4
550
1.75500
70.0Rotax 912 ULS Neuform
CR3-V-70R2Rotax Nirosta
Experimental
BX-2
// D
5500 /
/ 63.0
550
1.6
62.5
2700
70.0Sauer S2200UL Wolf Aviation
VP 2BL-160Sauer S2200UL
Experimental
BX-2
// D62.5
2700 /
/ 66.4
550
1.6
73.0
5225
70.0Rotax 912 ULS2 Woodcomp
SR3000/3Rotax/Aerotec
Experimental
BX-2
// D73.0
5225 /
/ 64.0
17.03.2020 Seite 9 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
550
1.6
66.8
2400
76.0Rolls-Royce C-90-8F Borgeaud/Pache
BX-2Andere
Experimental
BX-2
68.0 /64.9 / C66.8
2400 /
/
550
1.6
47.8
2300
76.0Continental A-65-8 Brändli
EVP1Crossover D121
Experimental
BX-2
// D47.8
2300 /
/ 63.6
550
1.6
48.6
2300
76.0Continental A-65 Brändli
160/150
Experimental
BX-2
68.0 /62.3 / D
/
/
550
1.6
67.1
2475
76.0Continental C-90-8F Brändli
160/150Eigenbau
Experimental
BX-2
68.0 /60.6 / D67.1
2475 /
/
600
1.6
73.0
5225
70.8Rotax 912 ULS2 Woodcomp
SR3000/3Rotax
Experimental
BX-2
// D73.0
5225 /
/ 63.8
375
1.3
35.7
3200
76.0VW 1600 Brändli
Experimental
BX-3 "Swing"
// D37.2
3500 /
/ 63.4
530
1.8
97.2
2600
76.0Rolls-Royce O-200-A Legere
2102
Experimental
BOUVREUIL P50
68.0 /66.8 / B
/
/
360
1.36
37.4
3350
76.0Societe JPX JPX 4T50 AE Brügger
136x75
Experimental
COLIBRI "D"
68.0 /64.5 / C37.4
3350 /
/
350
1.95
17.2
1300
76.0Koenig SC430 Ruppert
COFP
Experimental
COLIBRI SL 1
68.0 /54.6 / D
/
/
280
1.18
14.9
2640
76.0Solo 2350B Technoflug
KS-118-3-SBucher
Experimental
Canard SC
// D17.2
3000 /
/ 62.4
725
2.052450
73.7Rotec R3600 MT-Propeller
MT 205 R120-6COriginal
Experimental
Hatz CB-1
// A
2450 /
/ 73.7
170
0.695
23.3
5500
76.0JPX PUL 212 Eigenbau
MC/AS 695-200-103Eigenbau JPX
Experimental
CRI-CRI MC 15
// C23.3
5500 /
/ 66.5
600
1.745800
70.8Rotax 912 ULS Woodcomp
SR 3000/2WCZAW
Experimental
Sportcruiser
// D
5800 /
/ 65.5
630
1.785800
71.5Rotax 912 ULS Sensenich
2A0R5R70ENCZAW SportCruiser
Experimental
Sportcruiser
// D
5800 /
/ 63.5
300
1.616500
70.0Göbler-Hirth 3503 Kievprop
243Rotor Tec
Experimental
Gyrotec DF02
// D
6500 /
/ 65.6
375
1.33
28.3
3200
76.0Auto 1500 Hoffmann
F-H2/S11-133
Experimental
ERLA 5
68.0 /68.8 / A
/
/
410
1.45
28.3
3200
Great Plains Aviation Supply 1600cc Long Hoffmann
HO 11(A)HM-145 B 75
Experimental
ERLA 5
68.0 /68.8 / A
/
/
By virtue of the date of type certification this aircraft type is in accordance with SR 748.215.3 without the need to comply with the Standards of ICAO Annex 16, Volume I.
17.03.2020 Seite 10 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
590
1.6
73.5
5500
76.0Rotax 912 ULS Woodcomp
SR2000XA
Experimental
Europa
// D73.5
5500 /
/ 62.1
590
1.585800
70.5Rotax 912 ULS Warp Drive
62"ROTAX Europa XS
Experimental
Europa
// D
5800 /
/
Prop: 17.5°
64.8
621
1.65800
71.3Rotax 914 UL2 Woodcomp
SR3000/3
Experimental
Europa XS
// D
5800 /
/ 67.6
527
1.75
140.0
2500
76.0LOM M-332 AK MT-Propeller
MTV-7-C/C175-112Fry Aircraft Design
Experimental
Esprit VFII "SC"
// D140.0
2500 /
/ 65.4
1700
1.98
231.6
2500
85.0Continental IO-580-B1A MT-Propeller
MTV-9D/198-52MSW MSW/Express
Experimental
Express 2000 ER
// D231.6
2500 /
/ 80.0
1497
1.98
228.0
2500
85.0Continental IO-550-N MT-Propeller
MTV-9D/198-52MSW
Experimental
Express S-90
// D228.0
2500 /
/ 79.0
1454
1.82600
84.5Lycoming Lyc IO-360-ES (1) B MT-Propeller
MTV-12-D//180-17Eigenbau Walser/Rieben
Experimental
Wheeler Express CT
// D
2600 /
/ 76.7
952
1.88
129.7
2500
82.5Lycoming IO-360-B1E Hartzell
HC-C2YK-1MécanAir
Experimental
GLASAIR II FT
72.7 /65.7 / D134.2
2700 /
/
999
1.73
180.0
2565
83.2Lycoming IO-360-B1E Hartzell
HC-F2YR-1BF/F7068-2Bullet 416
Experimental
GLASAIR II RG
// C180.0
2565 /
/ 75.7
1088
2.032
304.2
2500
84.4Lycoming IO-540-K1H5 Hartzell
HC-C2YK-1BF/F8475J-4Eigenbau
Experimental
GLASAIR III RG
// C304.2
2500 /
/ 76.7
1134
2.08
213.2
2500
85.0Lycoming IO-540-EXP McCauley
B2D37C229/90RHCModel Theo Abt
Experimental
GLASAIR III RG
// C213.2
2500 /
/ 78.4
862
1.93
134.2
2700
81.1Lycoming IO-360-B1E Hartzell
HC-C2YK-1
Experimental
GLASAIR RG
71.5 /70.5 / B134.2
2700 /
/
862
1.88
133.7
2700
81.1Lycoming IO-360-B1E Hartzell
HC-C2YK-1MécanAir
Experimental
GLASAIR RG
71.5 /69.8 / B133.7
2700 /
/
862
1.88
128.2
2500
81.1Lycoming IO-360-B1E Hartzell
HC-C2YK-1MécanAir
Experimental
GLASAIR RG
71.5 /65.9 / D134.2
2700 /
/
951
1.75
119.3
2700
82.5Lycoming O-320-D1A MT-Propeller
MTV-12-CMécanAir
Experimental
GLASAIR II RG
// C119.3
2700 /
/ 75.0
889
1.78
110.0
2150
81.6Lycoming O-320 Felix Propeller Inc.
A70 61 BC9
Experimental
Glastar GS1
// D110.0
2150 /
/ 68.0
889
1.722150
81.6Lycoming O-320 Prince
CF P-TIP 68/64 PK Glastar 1
Experimental
Glastar GS-1
// D
2150 /
/ 72.6
889
1.832500
76.9Teledyne Mattituck O-360 MT-Propeller
MTV-15-B/183-402Glasair Aviation Lyc 360 (P/N 504-03000-0
Experimental
Glastar GS-1
// D
2500 /
/ 71.1
17.03.2020 Seite 11 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
889
1.854
114.0
2500
81.6Lycoming O-320-D1F Hartzell
HC-F2YL-1FNGS/Stoddard Hamilton 504-0200-01
Experimental
Stoddard Hamilton / Glastar GS
// D114.0
2500 /
/
Startdrehzahl reduziert auf 2500 1/min
70.9
889
1.854
114.0
2650
81.6Lycoming O-320-D1F Hartzell
HC-F2YL-1FNGS/Stoddard Hamilton 504-0200-01
Experimental
Stoddard Hamilton / Glastar GS
// C114.0
2650 /
/ 74.1
700
1.86
72.0
4000
78.2Porsche Austria VW-HB-2400 G/2 HB-Flugtechnik
HB-VP-3G 186 160 RZ
Experimental
HB-207 ALFA
// D72.0
4000 /
/ 69.3
700
1.72
60.3
1682
78.2Porsche Austria VW-HB-2400 G/2 HB-Flugtechnik
HB-VP 5G-170 160 RZBrditschka
Experimental
HB-207 ALFA
// D60.3
1682 /
/ 60.2
320
1.3
33.4
3200
76.0VW AUTO 1500 Schächtelin
SC-EvraAndere
Experimental
JODEL D-9
68.0 /54.6 / D
/
/
320
1.36
33.4
3200
76.0VW AUTO 1500 Evra
N 19ST
Experimental
JODEL D-9
68.0 /61.6 / D
/
/
320
1.37
32.4
3100
76.0VW 1600 Hoffmann
HO-11-137B85LAndere
Experimental
JODEL D-9
68.0 /56.2 / D
/
/
700
1.532800
73.2Jabiru 3300cc Airmaster
AP332Jabiru 4A293A0D1
Experimental
Jabiru J250
// A
2800 /
/ 72.0
476
1.78
58.9
2235
76.0Rotax 912 UL Warp
3black
Experimental
KITFOX 3
// D58.9
2235 /
/ 64.4
476
1.5242700
70.0Jabiru 2200A Jabiru
C000242 D 60 PO 42Original
Experimental
KITFOX 3
// C
2700 /
/ 67.4
476
1.676
48.4
2000
76.0Rotax 582LC GSC
Tech III, HolzROTAX
Experimental
KITFOX 3; -4
// D48.4
2000 /
/ 63.1
544
1.83
60.7
2420
76.0Rotax 912 UL IVO
IVO-PropellerAndere Skystar
Experimental
KITFOX 4
// D60.7
2420 /
/ 63.1
544
1.73
35.7
2066
76.0Rotax 582LC Warp
Warp Drive 68"
Experimental
KITFOX 4
// D35.7
2066 /
/ 63.5
500
1.78
47.8
2273
76.0Subaru EA-81 1800 Warp
Warp Drive 70"Stratus Inc
Experimental
KiTFOX IV-1100
// D47.8
2273 /
/ 59.0
544
1.7342420
76.0Rotax 912 ULS IVO
IVO-Propeller
Experimental
KiTFOX IV-1200
// D
2420 /
/ 63.3
544
1.935700
70.0Rotax 912 ULS Airmaster
AP430
Experimental
KiTFOX IV-1200
// A
5700 /
/ 69.9
544
1.785000
70.0HKS 700T Warp Drive
T6139
Experimental
KiTFOX IV-1200
// D
5000 /
/ 64.8
17.03.2020 Seite 12 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
544
1.78
56.0
2288
76.0Rotax 912 UL IVO
IVO-PropellerSkystar
Experimental
KiTFOX IV-1200 Speedster
// D56.0
2288 /
/
Prop. Einstellung auf 9°
65.9
544
1.734
58.8
2420
76.0Rotax 912 UL IVO
IVO-Propeller
Experimental
KiTFOX IV-1200 Speedster
// D58.9
2420 /
/ 64.8
500
1.752420
70.0Rotax 912 UL Arplast
175DWAP 62/3
Experimental
KITFOX S4
// D
2420 /
/ 65.0
634
1.7
73.5
2455
76.8Subaru EA-81 Woodcomp
SR2000XAStratus Inc
Experimental
KiTFOX V
// C73.5
2455 /
/ 69.4
547
1.75
59.6
2420
76.0Rotax 912 Arplast
175DWAMSkystar
Experimental
KITFOX 5
// D59.6
2420 /
/ 66.2
703
1.75600
73.2Rotax 912 ULS Woodcomp
SR2000Skystar
Experimental
KiTFOX VI
// D
5600 /
/ 66.6
703
1.745800
73.2Rotax 912ULS Sensenich
3BOR5R68CKitfox Aircraft
Experimental
KITFOX S7
// D
5800 /
/
Pitch Setting Gage Nr. 2
68.4
703
1.775500
73.2Rotax 912ULS IVOPROP
Medium 70Kitfox LLC
Experimental
KITFOX S7
// D
5500 /
/
max RPM: 55001/min
69.3
635
1.75
58.9
2423
76.8Rotax 912 UL Arplast
175 DWAP
Experimental
KITFOX Vixen 1400
// D58.9
2423 /
/ 66.0
300
1.37
32.4
3100
76.0VW 1600 Brügger
BRUEGGER
Experimental
KOLIBRI
68.0 /54.5 / D
/
/
340
1.38
32.4
3200
76.0VW 1600 Hoffmann
HO-02-136B75
Experimental
KOLIBRI 2
68.0 /62.1 / D
/
/
340
1.33
32.0
3200
76.0VW 1600 MT-Propeller
MT 133L75-L B
Experimental
KOLIBRI MB2
68.0 /61.5 / D32.0
3200 /
/
340
1.43
32.4
3200
76.0VW 1600 Eigenbau
D143/P78
Experimental
KOLIBRI MB2
68.0 /58.5 / D
/
/
340
1.33
32.4
3200
76.0VW 1600 Hoffmann
HO-11*133S70
Experimental
KOLIBRI MB2
68.0 /61.5 / D
/
/
340
1.28
44.5
3500
76.0VW 1800 Eigenbau
108/3BHT
Experimental
KOLIBRI MB2
68.0 /65.6 / C
/
/
340
1.372950
70.0VW 1600 GT Prop.
GT-2/137/NT-FW101SLTCEigenbau
Experimental
KOLIBRI MB2
// A
2950 /
/ 68.7
355
1.36
32.4
3100
76.0VW 1600 Hoffmann
HO-02-136B75
Experimental
KOLIBRI MB2
68.0 /62.1 / D
/
/
17.03.2020 Seite 13 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
370
1.45
46.6
3200
76.0Societe JPX JPX 4T60/B MT-Propeller
MT 145 L80-1
Experimental
KOLIBRI MB2
68.0 /65.5 / C
/
/
380
1.463400
70.0HAPI (VW) 75 DMH E-Props
Belisandre
Experimental
KOLIBRI MB2
// A
3400 /
/ 69.9
390
1.36
32.4
3200
76.0VW 2180 CC Brügger
100x136
Experimental
KOLIBRI MB2
68.0 /58.5 / D
/
/
710
1.6
86.9
2700
78.4Lycoming O-235-L2A MT-Propeller
MTV-1-FLancair/Liese
Experimental
LANCAIR 235
// A86.9
2700 /
/ 74.2
710
1.572500
78.4Lycoming O-235-P2A MT-Propeller
MTV-1-F/157-07Dobis
Experimental
LANCAIR 235
69.5 /60.8 / D
2500 /
/
710
1.62500
78.4Lycoming O-235-P2A MT-Propeller
MTV-1-F/160-07Liese
Experimental
LANCAIR 235
69.5 /62.0 / D
2500 /
/
765
1.92
117.6
2500
74.6Lycoming IO-320-B1A MT-Propeller
MTV-12-B/175-17Liese
Experimental
LANCAIR 320
// C117.6
2500 /
/ 72.0
765
1.75
111.8
2700
79.4Lycoming O-320-E2A; -E2D MT-Propeller
MTV-17-C/175-17Erni 01
Experimental
LANCAIR 320
// A111.8
2700 /
/ 76.4
794
1.7
111.8
2700
75.1Lycoming O-320-D1F MT-Propeller
MTV-12-C/170-36Liese
Experimental
LANCAIR 320
// C111.8
2700 /
/ 72.8
765
1.778
132.0
2500
74.6Lycoming IO-360-A1A Aero Composites
ACI 2000MécanAir
Experimental
LANCAIR 360
// C132.0
2500 /
/ 72.0
765
1.752550
74.6Lycoming O-360-A1A MT-Propeller
MTV-12-B/175-59d Muffler Tube
Experimental
LANCAIR 360
// A
2550 /
/ 74.2
765
1.75
134.0
2522
79.4Lycoming O-360-A1A MT-Propeller
MTV-12-B/175-17dLiese
Experimental
LANCAIR 360 MKII
// D134.0
2522 /
/ 70.0
520
1.58
58.0
2305
76.0Rotax 912 UL Sport Prop
Varia 16-2 R
Experimental
Lambada UFM 13/520
// D58.0
2305 /
/
Prop.: Einstellwinkel 16°
62.5
998
1.83
230.0
2450
78.7Continental IO-550-N13 MT-Propeller
MTV 9-D/183-50aTuboly T1
Experimental
LANCAIR Legacy 2000
// D230.0
2450 /
/ 74.0
646
1.6
88.1
2650
77.0Lycoming O-235-L2A Great American
62X60MEIGA/Wülsag
Experimental
LONG EZE
68.6 /68.9 / A
/
/
646
1.48
88.1
2700
77.0Lycoming O-235-L2A Hoffmann
HO-14BHM148BMEIGA/Wülsag
Experimental
LONG EZE
68.6 /71.4 / A
/
/
660
1.59
80.0
2600
77.3Lycoming O-235-C2A Hendrickson
H62XL66
Experimental
LONG EZE
68.8 /66.7 / C
/
/
660
1.65
82.0
2700
77.3Lycoming O-235-P1 Hoffmann
HO-V72G/170U
Experimental
LONG EZE
68.8 /66.9 / C89.4
2800 /
/
17.03.2020 Seite 14 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
660
1.5
80.0
2500
77.3Lycoming O-235-P2A Hoffmann
HO-V113B-L
Experimental
LONG EZE
68.8 /66.3 / C89.4
2800 /
/
660
1.6
86.1
2700
77.3Lycoming O-235-L2C Eigenbau
B+T 62X66
Experimental
LONG EZE
68.8 /68.7 / B
/
/
660
1.5
80.0
2500
77.3Lycoming O-235-P2A Hoffmann
HO-V113B-L
Experimental
LONG EZE
68.8 /64.4 / C89.4
2800 /
/
660
1.46
86.1
2680
77.3Lycoming O-235-L2A Hendrickson
H58G74MEIGA/Wülsag
Experimental
LONG EZE
68.8 /68.5 / B
/
/
660
1.66
88.1
2600
77.3Lycoming O-235-P1 Hoffmann
HO-V72G/170U
Experimental
LONG EZE
68.8 /67.9 / B89.4
2800 /
/
660
1.55
86.1
2700
77.3Lycoming O-235-L2C MT-Propeller
MTV-1-F
Experimental
LONG EZE
68.8 /66.0 / C89.4
2800 /
/
660
1.59
121.5
2700
77.3Lycoming O-320-D3G Eigenbau
B+T Prop.62X75
Experimental
LONG EZE
68.8 /67.6 / B121.5
2700 /
/
660
1.46
86.1
2700
77.3Lycoming O-235-L2A Hendrickson
H58G74MEIGA/Wülsag
Experimental
LONG EZE
68.8 /64.8 / C
/
/
690
1.5752700
73.0Lycoming O-320-D2A Great American
62X72
Experimental
LONG EZE
// A
2700 /
/ 72.8
635
1.82
66.8
2400
76.8Rolls-Royce C90-14F Hoffmann
HO-14-183100
Experimental
LUTON MAJOR LA5
68.5 /64.5 / C
/
/
490
1.78
48.6
2300
76.0Continental A-65-8 Hoffmann
HO-14-178-100
Experimental
MIGNET HM19C
68.0 /63.0 / D
/
/
530
1.78
66.8
2475
76.0Continental C-90-12 Hoffmann
HO-14-178-100
Experimental
MIGNET HM19C
68.0 /63.7 / C
/
/
590
1.78
66.8
2475
76.0Continental C-90-14F Hoffmann
HO-14-178-115
Experimental
MIGNET HM380
68.0 /63.4 / C
/
/
544
1.715800
70.0Rotax 914 F3 MT-Propeller
MTV-6-A/170-125Rotax/ASPES MK II
Experimental
Dyn-Aero MCR M
// D
5800 /
/ 59.4
544
1.75800
70.0Rotax 914 F2 MT-Propeller
MTV-6-A/170-125Rotax/ASPES
Experimental
Dyn-Aero MCR M
// D
5800 /
/ 60.7
450
1.52
58.0
2420
76.0Rotax 912 UL MT-Propeller
MTV 7-A/152-106Dyn-Aero MMOMOE 101
Experimental
Dyn-Aero MCR-01
// C58.0
2420 /
/ 66.9
490
1.52
60.5
5800
70.0Rotax 912 UL MT-Propeller
MTV 6-A/152-106Chabord EV1
Experimental
Dyn-Aero MCR-01
// C60.5
5800 /
/ 67.0
490
1.52
60.5
5800
70.0Rotax 912 UL MT-Propeller
MTV 7-A/152-106Chabord EV1
Experimental
Dyn-Aero MCR-01
// C60.5
5800 /
/ 67.0
17.03.2020 Seite 15 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
490
1.56
73.5
2160
76.0Rotax 912 ULS MT-Propeller
MTV 7-A/156-122Chabord
Experimental
Dyn-Aero MCR-01
// D73.5
2160 /
/ 63.0
544
1.75800
70.0Rotax 914 F MT-Propeller
MTV-6-A/170-125
Experimental
Dyn-Aero MCR-01
// D
5800 /
/ 65.0
490
1.52
59.6
5300
70.0Rotax 912 UL MT-Propeller
MTV 7-A/152-106Chabord EV1
Experimental
Dyn-Aero MCR-01 Club
// D59.6
5300 /
/ 65.0
490
1.56
74.5
5500
70.0Rotax 912 S MT-Propeller
MTV 7-A/156-122Chabord MCR-01
Experimental
Dyn-Aero MCR-01 Club
// C74.5
5500 /
/ 67.0
490
1.56
84.0
2390
76.0Rotax 914 UL MT-Propeller
MTV 7-A/152-106
Experimental
Dyn-Aero MCR-01 VLA 914
// C84.0
2390 /
/ 67.7
750
1.57
73.5
5500
74.2Rotax 912 ULS MT-Propeller
MTV 6-A/156-122Chabord
Experimental
Dyn-Aero MCR-4S
// C73.5
5500 /
/ 72.0
1150
2.4
208.0
4200
80.9Chevrolet SB V8 400C MT-Propeller
MTV-9-E-C/CL240-27XEigenbau
Experimental
MJ-10 Haug Spitfire
// D208.0
4200 /
/ 73.9
260
1.605
30.3
2325
76.0Rotax 447E FA GT Prop.
160x90
Experimental
MINI MAX
// C30.3
2325 /
/ 67.3
295
1.605
29.5
6200
76.0Rotax 447 UL SCDI GT Prop.
GT-2/160/NO-FW75SLTC
Experimental
MINI MAX
// D29.5
6200 /
/ 63.1
680
1.68
111.4
2700
77.8Lycoming O-320-E3H Sensenich
74DM6-8-70
Experimental
MUSTANG II
69.1 /67.2 / B
/
/
31026.3
2370
76.0Hirth 2702R03E Diverse
FALTPROPELLER
Experimental
NEUKOM AN 20B
68.0 /60.7 / D
/
/
260
1.33
11.1
2375
76.0Koenig SC430 Neukom
Diverse
Experimental
NEUKOM AN-20B
68.0 /56.4 / D
/
/
260
1.183900
76.0Koenig SD570 Borowski
KS-118-3
Experimental
NEUKOM AN-20B
68.0 /62.1 / D
/
/
250
1.05
11.1
3300
76.0Koenig SC430 Neukom
Diverse
Experimental
NEUKOM AN-20C
68.0 /60.0 / D
/
/
567
1.72
134.2
2700
76.0Lycoming IO-360-X Performance Propellers
OA 3 bladeLPE Corp. Custom made
Experimental
One Design
// A134.2
2700 /
/ 76.4
610
1.83
134.2
2600
76.2Lycoming IO-360-C1B MT-Propeller
MTV-12-B-C/C183-17eMSW
Experimental
One Design
// C134.2
2600 /
/ 69.1
846
2.032
132.4
2700
76.1Cub Crafters Inc. CC340 Catto Prop
80" 50Eigenbau
Experimental
CCK-1865 (Carbon Cub)
// D132.4
2700 /
/ 71.7
560
1.76
73.5
5700
70.0Rotax 912 ULS2 Alisport Srl.
IdrovarioROTAX
Experimental
Pioneer 300
// C73.5
5700 /
/ 67.6
17.03.2020 Seite 16 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
612
1.43
55.7
3500
76.3Revmaster 2100-D Maloof
2C 3.9
Experimental
POLLIWAGEN
68.2 /68.1 / B
/
/
550
1.505
60.7
3400
76.0Limbach L 2000 EB1 Hoffmann
HO-V62R
Experimental
POTTIER P-180
68.0 /75.3 / A60.7
3400 /
/
550
1.505
54.7
3000
76.0Limbach L 2000 EB1 Hoffmann
HO-V62R
Experimental
POTTIER P-180
68.0 /66.4 / B
/
/
550
1.52700
70.0Sauer SD 2500 H1S Arplast
Ecoprop 4TG/3
Experimental
POTTIER P-180S
// D
2700 /
/ 66.0
360
1.323300
70.0VW Typ 1 (1835) Hoffmann
HO-17A-132B-97LEigenbau
Experimental
POTTIER P-80S
// D
3300 /
/ 65.7
453
1.43
48.6
2630
76.0Rotax 582 GSC
GSC Prop. 56x38
Experimental
PULSAR
// A48.4
2630 /
/ 74.7
480
1.41
48.6
2703
76.0Rotax 582 GSC
GSC Prop. 56x38
Experimental
PULSAR
// A48.6
2703 /
/ 71.8
480
1.422700
70.0Jabiru 2200 Prince
P-Tip P56AT52LKOriginal
Experimental
PULSAR
// D
2700 /
/ 60.5
477
1.53
57.7
2290
76.0Rotax 912 GSC Canada
GSCROTAX
Experimental
PULSAR XP
// C60.4
2551 /
/ 67.7
480
1.475250
76.0Rotax 912 ULS FR Woodcomp
SR3000/3
Experimental
PULSAR XP
// D60.4
5250 /
/ 61.5
480
1.47
60.4
5800
76.0Rotax 912 UL Woodcomp
SR2000XA
Experimental
PULSAR XP
// A60.4
5800 /
/ 72.4
480
1.63
56.8
2107
76.0Rotax 912 UL GSC
Wooden bladesROTAX Aero Design
Experimental
PULSAR XP
// C56.8
2107 /
/ 67.9
480
1.542
59.6
2420
70.0Rotax 912 UL2 GSC Canada
2-Bl. 60"Heggemann 4/4 Standard
Experimental
PULSAR XP
// D59.6
2420 /
/
Prop. Einstellwinkel: 21°
64.2
480
1.47
60.4
5250
76.0Rotax 912 ULSFR Woodcomp
SR2000XA
Experimental
PULSAR XP
// D60.4
5250 /
/ 62.1
480
1.475250
76.0Rotax 912 ULS FR Woodcomp
SR2000
Experimental
PULSAR XP
// D60.4
5250 /
/ 61.5
480
1.52
59.6
2420
76.0Rotax 912 UL MT-Propeller
MTV 7-A/152-106Eigenbau
Experimental
PULSAR XP
// D59.6
2420 /
/ 61.9
505
1.75500
70.0Rotax 912 UL Woodcomp
VAR2Aerodesigns Pulsar XP
Experimental
PULSAR XP
// D
5500 /
/ 64.6
505
1.52
59.6
2420
76.0Rotax 912 UL MT-Propeller
MTV 7-A/152-106Eigenbau
Experimental
PULSAR XP
// D59.6
2420 /
/ 62.6
17.03.2020 Seite 17 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
505
1.542
59.6
2420
76.0Rotax 912 UL2 GSC Canada
2-Bl. 60"Heggemann 4/4 Standard
Experimental
PULSAR XP
// D59.6
2420 /
/
Prop. Einstellwinkel: 21°
62.5
225
1.06
16.2
3600
76.0Onan 22 HP Cowley
P30 D42
Experimental
QUICKIE
68.0 /57.7 / D
/
/
225
1.06
13.1
3600
76.0Onan 18 HP Cowley
P30 D42
Experimental
QUICKIE
68.0 /56.8 / D
/
/
255
1.15
26.0
3250
76.0Mosler MMCB Brügger
115x80Eigenbau
Experimental
QUICKIE Q2
68.0 /61.2 / D26.0
3250 /
/
410
1.43
33.4
3450
76.0VW VW 1600 Bezzola
2R-143
Experimental
RETRO
68.0 /71.6 / A
/
/
680
1.75
117.6
2700
72.7Lycoming IO-320-A2C MT-Propeller
MTV-18-C/175-36aDanielsson RV-4
Experimental
Van's RV-4
// A117.6
2700 /
/ 72.5
680
1.832500
72.7Lycoming O-360-A1A MT-Propeller
MTV-12-BExperimental
Experimental
Van's RV-4
// A
2500 /
/ 72.2
680
1.73
117.6
2200
77.8Lycoming O-320-D1A Prince
68/74PK Q-TipSuppertrapp 422-25000
Experimental
Van's RV-4
// C117.6
2200 /
/ 70.4
680
1.73
117.6
2700
77.8Lycoming O-320-D1A Prince
68/76 LK P-TipEigenbau
Experimental
Van's RV-4
// D117.6
2700 /
/ 67.7
726
1.78
114.0
2200
78.7Lycoming O-320-D1A Sensenich
70CM7S9-0-79Gomolzig Typ 3
Experimental
Van's RV-6
// D114.0
2200 /
/ 65.9
726
1.832600
73.7Lycoming O-360-A3A MT-Propeller
MTV-12-B/183-59Gomolzig RV6-NSD-3-606500
Experimental
Van's RV-6
// C
2600 /
/ 71.8
749
1.812350
74.2Lycoming IO-360-EXP-ZAE Whirlwind
GA200L-816Liese RV-6A - 2x76/150
Experimental
Van's RV-6A
// D
2350 /
/ 67.0
815
1.782240
75.5Lycoming O-320-D1A Sensenich
70CM7S9-0-80Liese 60x150 L
Experimental
Van's RV-7
// D
2240 /
/ 70.3
816
1.832500
75.6Lycoming IO-360-M1B MT-Propeller
MTV-12-B/183-59BLiese 2x76x150-L
Experimental
Van's RV-7
// A
2500 /
/ 73.4
817
1.832500
75.6Lycoming IO-360-M1B MT-Propeller
MTV-12-B/183-59BLiese RV-7
Experimental
Van's RV-7
// C
2500 /
/ 72.3
816
1.732500
75.6Aro Sport Power IO-320-D1A Sensenich
70CM7S9-0-79Vettermann 4-2
Experimental
Van's RV-7A
// D
2500 /
/ 69.0
816.5
1.8282500
75.6Mattituck TMX IO-360 Hartzell
C2YR-1BFP/F7497-2Vettermann/Liese RV-7
Experimental
Van's RV-7A
// D
2500 /
/ 70.9
817
1.832700
75.6Mattituck TMX IO-360 Catto Prop
72x74Liese RV-7
Experimental
Van's RV-7A
// D
2700 /
/ 70.9
17.03.2020 Seite 18 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
817
1.762600
75.6Mattituck TMX IO-320 Sensenich
70CM7S9-0-79Liese RV-7A
Experimental
Van's RV-7A
// D
2600 /
/ 69.5
817
1.882500
75.6Lycoming YIO-360-M1B Hartzell
HC-C2YR-1BFP/F7497Vettermann Trombone 2 in 2
Experimental
Van's RV-7A
// C
2500 /
/
Maximum take-off engine rotational speed limited to 2500 RPM
71.4
817
1.82350
75.6Mattituck TMX IO-360 Sensenich
72FM8S9-1-85Liese RV-7A
Experimental
Van's RV-7A
// D
2350 /
/ 71.2
1225
1.932500
81.9Mattituck TMX IO-540-X MT-Propeller
MTV-12-B/193-53Vettermann 6-2
Experimental
Van's RV-10
// D
2500 /
/ 77.5
1225
2.032500
81.9Lycoming IO-540-X Hartzell
C2YR-1BFP/F8068DLiese 2xRV-10
Experimental
Van's RV-10
// C
2500 /
/ 79.2
1225
2.0252500
81.9Lycoming IO-540-D4A5 Hartzell
C2YR-1BFP/F8068DVettermann RV-10
Experimental
Van's RV-10
// D
2500 /
/ 77.7
599
1.7785800
70.8Rotax 912 ULS Sensenich
2A0R5R70E-V-0Original
Experimental
Van's RV-12
// D
5800 /
/ 65.1
816
1.832500
75.6Lycoming IO-360-M1B MT-Propeller
MTV-12-B-C/C183-59bLiese 76-300-L
Experimental
Van's RV-8
// D
2500 /
/ 69.5
816
1.832500
75.6Lycoming YIO-360-M1B Hartzell
HC-C2YR-1BFP/F7497-2Vettermann EA EXH8 IO360M1B
Experimental
Van's RV-8
// A
2500 /
/
Propeller is limited to a maximum of 2500 RPM by the governor.
75.2
817
1.832500
75.6Lycoming Mattitick TMX-IO-360 Prince
68/83PKLiese 2x76x150L
Experimental
Van's RV-8
// D
2500 /
/ 71.2
475
1.725500
70.0Rotax 912 UL2 Woodcomp
SR 3000/2WRans Inc.
Experimental
Rans S-10
// C
5800 /
/
AFM Section 4.4: Takeoff: 50ft AGL - MAX CONT PWR (5500RPM)
67.4
499
1.573300
70.0Jabiru 2200 GT Prop.
GT-2/157/NO-FW101SRTCJabiru 2200
Experimental
Rans S-6S
// C
3300 /
/ 67.3
600
1.88
73.5 70.8Rotax 912 ULS MT-Propeller
MT 188R108-1ASlepcev/Rotax EO-1513
Experimental
Slepcev Storch Mk. IV
// C73.5
/
/ 69.6
366
1.562550
76.0VW 1835 Arplast
ECO-4 TGE-2Eigenbau
Experimental
Sonerai I
68.0 /61.1 / D44.8
2550 /
/
320
1.37
33.4
3100
76.0VW 1500 Hoffmann
HO-FH2/S1113
Experimental
STARK TURBULENT
68.0 /59.6 / D
/
/
270
1.33
22.2
3200
76.0VW 1200 Rousseau
Rousseau
Experimental
STARK T. D31
68.0 /65.0 / C
/
/
17.03.2020 Seite 19 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
460
1.55
74.9
2730
76.0Rolls-Royce O-200-A Hegi
60X60
Experimental
TAYLOR TITCH
68.0 /63.7 / C
/
/
648
1.732700
72.0Lycoming O-320-E3H Felix Propeller Inc.
68x74"Liese 2x60x150L
Experimental
Tailwind W10
// C
2700 /
/ 70.1
280
1.28
32.4
3000
76.0VW VW 1600 Hegi
50X40Andere
Experimental
TEENIC'S
68.0 /63.0 / D
/
/
300
1.37
33.4
3060
76.0VW 1500 Hoffmann
HO-11-137B85
Experimental
TIPSY N. MK II
68.0 /62.0 / D
/
/
300
1.37
32.4
2900
76.0VW 1600 Hoffmann
HO-11-137B85
Experimental
TIPSY N. MK II
68.0 /57.8 / D
/
/
330
1.45
29.3
2950
76.0ARDEM 4C02 DRG Propellers
Z3405
Experimental
TIPSY N. MK3
68.0 /65.7 / C
/
/
33029.3
2950
76.0ARDEM 4C02 Evra
HR 1201
Experimental
TIPSY N. MK3
68.0 /65.7 / C
/
/
175
1.12
16.2
3700
76.0Koenig SC430 Ernst Ruppert
01/02
Experimental
TWIN BABY
68.0 /62.2 / D
/
/
480
1.48
88.1
2600
76.0Lycoming O-235-C2C Great American
58X68MEIGA/Wülsag
Experimental
VARI EZE
68.0 /65.8 / C
/
/
480
1.49
88.1
2700
76.0Lycoming O-235-C2C Hendrickson
H58G74MEIGA/Wülsag
Experimental
VARI EZE
68.0 /65.1 / C
/
/
480
1.58
82.0
2600
76.0Lycoming O-235-C2C MT-Propeller
MT 157LD160-2
Experimental
VARI EZE
68.0 /64.5 / C
/
/
480
1.49
74.9
2750
76.0Rolls-Royce O-200-A Beaufils
Beaufils ET-122
Experimental
VARI EZE
68.0 /67.0 / B
/
/
480
1.48
66.8
2475
76.0Rolls-Royce C90-8F Brügger
BRUEGGER
Experimental
VARI EZE
68.0 /65.6 / C
/
/
480
1.56
82.0
2600
76.0Lycoming O-235-C2C MT-Propeller
MTV-1-AFLD1560MEIGA/Wülsag
Experimental
VARI EZE
68.0 /64.4 / C
/
/
480
1.47
66.8
2475
76.0Rolls-Royce C90-8F GAP
56CX70P
Experimental
VARI EZE
68.0 /63.8 / C
/
/
480
1.473
82.0
2500
76.0Lycoming O-235-L2C Bruce Tifft (Holz)
58X72Andere
Experimental
VARI EZE
68.0 /63.0 / D
/
/
520
1.53
75.9
2750
76.0Rolls-Royce O-200-A MT-Propeller
MTV-1-F
Experimental
VARI EZE
68.0 /63.3 / C75.9
2750 /
/
550
1.53
75.9
2750
76.0Rolls-Royce O-200-A MT-Propeller
MTV-1-F
Experimental
VARI EZE
68.0 /64.1 / C75.9
2750 /
/
17.03.2020 Seite 20 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
1089
1.73
200.0
2500
80.0Lycoming IO-360-C1E6 MT-Propeller
MTV-12-B-230/LD 168-24CAT-Breer
Experimental
Velocity
// C200.0
2500 /
/ 76.5
750
1.932500
74.2Lycoming AEIO-390-X MT-Propeller
MTV-9-B-C/C193-18bMSW
Experimental
Votec 221
// C
2500 /
/ 70.6
950
1.95
230.0
2500
77.9Lycoming O-540-J3A5 MT-Propeller
MTV-14-B-C/C195-30dMSW
Experimental
Votec 252 T
// D230.0
2500 /
/ 72.8
950
2.032500
77.9Lycoming YAEIO-580-EXP MT-Propeller
MTV-9-B-C/C203-20dMSW-Aviation 1
Experimental
Votec 322
// C
2500 /
/ 73.8
950
1.95
231.0
2500
82.5Lycoming AEIO-540-C1B MT-Propeller
MTV-14-B-C/C195-30dMSW
Experimental
Votec 322
// D231.0
2500 /
/ 68.7
950
1.952500
82.5Lycoming YAEIO-580-EXP MT-Propeller
MTV-14-B-C/C195-30dMSW
Experimental
Votec 322
// D
2500 /
/ 68.7
950
2.032500
77.9Lycoming AEIO-540-X MT-Propeller
MTV-9-B-C/C203-20dMSW
Experimental
Votec 322
// D
2500 /
/ 72.8
950
1.95
240.0
2650
82.5Lycoming AEIO-540-C1B MT-Propeller
MTV-14-B-C/C195-30dMSW
Experimental
Votec 322
// A240.0
2650 /
/ 81.0
870
2.032500
76.6Lycoming AEIO-580 MT-Propeller
MTV-9-B-C/C203-20dMSW-Aviation 1
Experimental
Votec 351
// D
2500 /
/ 70.9
440
1.52850
70.0VW 1800 CC Woodcomp
SR 29 T-VW 1800
Experimental
Volksplane VP-1
// C
2850 /
/ 67.0
380
1.37
33.4
3300
76.0VW 1500H Hegi
8-74
Experimental
Volksplane VP-1
68.0 /65.7 / C
/
/
440
1.45
47.8
6200
70.0Rotax 582 Woodcomp
SR200Original
Experimental
Volksplane VP-1
// A47.8
6200 /
/ 69.8
440
1.6
47.8
6400
70.0Rotax 582 Woodcomp
SR200Original
Experimental
Volksplane VP-1
// D47.8
6400 /
/
Einstellwinkel: 12.5°
62.2
520
1.52
74.9
2750
76.0Rolls-Royce O-200-A Eigenbau
PONCELET 59 X 62Eigenbau
Experimental
W.A.R. FW 190 1/2
// D74.9
2750 /
/ 65.2
450
1.86300
70.0Rotax 582 Schmidtler
4-BlattOriginal
Experimental
Enduro
// A
6300 /
/ 68.9
545
1.75250
70.0Rotax 912 ULS2 Woodcomp
SR2000XAROTAX Nirosta
Experimental
Zenair CH-701
// D
5250 /
/ 65.0
545
1.72725400
70.0Rotax 912 UL Warp Drive
CF68RZenair Rotax
Experimental
Zenair CH-701 STOL
// C
5400 /
/ 67.5
545
1.785400
70.0Rotax 912 UL Warp Drive
CF70RZenair Rotax
Experimental
Zenair CH-701 STOL
// A
5400 /
/ 69.8
17.03.2020 Seite 21 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
1050
1.78
132.0
2500
79.5Lycoming IO-360-B1B Prince
P-Tip Comp 6423 P70AT 66LKHeggemann Archer II
Experimental
Zenith CH-300 TRI-Z (Mk II)
// C132.0
2500 /
/ 76.0
840
1.8
111.8
2700
80.8Lycoming O-320-A2B MT-Propeller
MT 180R145-3D
Experimental
Zenair TRI-Z
71.2 /66.9 / C111.8
2700 /
/
545
1.73
59.0
2288
70.0Rotax 912 UL Warp
Warp Drive 68"
Experimental
Zenair Zodiac 601 HDS
// D59.0
2288 /
/
Prop.: am Boden einstellbar (19°)
65.1
545
1.73
59.0
5200
76.0Rotax 912 UL Woodcomp
SR2000XA
Experimental
Zenair Zodiac 601 HDS
// D59.0
5500 /
/
MCP ab 500ft/GND
64.9
1162
2.14
122.5
2300
85.4Ranger 6-440-C5 Hoffmann
HO-33-214-12
Fairchild
24R46A
75.5 /72.9 / C
/
/
1162
2.18
122.5
2100
85.4Warner R-500-7 Hoffmann
HO-33-218-132
Fairchild
24-W-41-A
75.5 /73.0 / C
/
/
1162
2.2
122.5
2350
85.4Ranger 6-440-C5 Sensenich
86AB-54
Fairchild
F24R46A
75.5 /75.3 / B
/
/
750
1.82
122.5
2700
79.1Lycoming O-320-A2B Hartzell
HC-A2XL-1Andere
Falco
F8L
70.0 /70.6 / A
/
/
820
1.82
111.4
2700
80.4Lycoming O-320-A2A Hartzell
HC-C2YL-1BRobin (modifiziert)
Falco
F8L
70.9 /70.2 / B
/
/
820
1.82
111.4
2700
80.4Lycoming O-320-A2B Hartzell
HC-C2YL-1BAndere
Falco
F8L
70.9 /71.6 / A
/
/
820
1.83
110.0
2700
80.4Lycoming O-320-E1C Hartzell
HC-C2YL-1BF/F7663A-4Meeder Zeichn. Nr. 599-02.02.92
Falco
F8L
// C110.0
2700 /
/
STC SA 0452
73.1
820
1.85
117.6
2500
80.4Lycoming O-320-B3B Hartzell
HC-C2YL-1/7663A-4
Falco
F8-L 4
70.9 /71.4 / A117.6
2500 /
/
1485
2.56
88.0Argus Motorenwerke AS 10E MT-Propeller
MT 256 R 140-6ABOriginal
Fieseler
FI 156 C-3
// D176.5
2000 /
/ 76.9
472.5
1.7
64.5
4800
70.0Rotax 912 ULS Neuform
СR3-65-47-101.6"Original
Flight Design
CT SW
// D64.5
4800 /
/ 57.3
1080
2.08
275.1
2030
84.3Allison DDA 250-B17C Hartzell
HC-BTF-7A/10173N-19R
Flugzeugwerke Altenrhein AG (FF
AS 202/32TP
// D275.1
2030 /
/ 68.9
1080
2.1
275.1
2030
84.3Allison DDA 250-B17C MT-Propeller
MTV-5-1-D-C-F-R(A)/CFR210-56
Flugzeugwerke Altenrhein AG (FF
AS 202/32TP
// D275.1
2030 /
/ 66.6
3561
2.51
297.8
2200
88.0Pratt & Whitney R985 AN1 Hamilton
2D30-237
Hawker Beechcraft Corporation
C18S
80.0 /86.0 / A
/
/
17.03.2020 Seite 22 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
1200
2.13
122.5
2050
85.8Continental E-185-8 Hartzell
HC-A2X20-4A1
Hawker Beechcraft Corporation
A35
76.0 /67.5 / D
/
/
1225
2.23
137.7
2300
86.1Continental E-185-11 Beech
215-109
Hawker Beechcraft Corporation
C35
76.3 /72.0 / C
/
/
1236
2.23
137.7
2300
86.2Continental E-185-11 Beech
215-107
Hawker Beechcraft Corporation
D35
76.5 /72.6 / C152.8
2600 /
/
1327
2.134
137.9
2300
87.2Continental E-185-11 Hartzell
A2V20-4MEIGA/Wülsag
Hawker Beechcraft Corporation
D35
// A152.8
2600 /
/ 86.3
1250
2.13
137.7
2300
86.4Continental E-225-8 Hartzell
HC-A2X20-4A1
Hawker Beechcraft Corporation
F35
76.7 /69.8 / D
/
/
1350
2.13
137.7
2300
87.5Continental E-225-8 Beech
215-107
Hawker Beechcraft Corporation
G35
78.0 /68.8 / D
/
/
965
1.93
134.2
2700
82.7Lycoming O-360-A3A Sensenich
76EM8S5-0-56Gomolzig JOB15-606500
Job
15-180/2
// D134.2
2700 /
/ 68.9
965
1.93
134.2
2700
82.7Lycoming O-360-A3A Sensenich
76EM8S5-0-56
Job
15-180/2
72.9 /68.9 / D134.2
2700 /
/ 73.2
620
1.775
66.8
2475
76.4Continental C-90-14F Evra
D11-28-1BLiese Jodel D11
Jodel
D11-2
68.3 /62.2 / D
/
/
320
1.37
31.4
3100
76.0Stamo MS 1500/2 Hoffmann
HO-11-137B 85L
Jodel
D9
68.0 /57.6 / D
/
/
320
1.37
31.4
3100
76.0Stamo 1400 Hoffmann
F-H2/S11-137
Jodel
D9
68.0 /57.6 / D
/
/
620
1.8
66.8
2500
76.4Continental C-90-14F Evra
D 11 28 1B
Jodel
D11
68.3 /64.2 / C
/
/
620
1.75
74.5
2650
76.4Rolls-Royce O-200-A Sensenich
69CK-0-52Liese Jodel D11
Jodel
D11
// D74.5
2650 /
/ 67.2
620
1.8
63.8
2575
76.4Continental C-85-12F McCauley
1B90/CM/7152
Jodel
D11
68.3 /61.2 / D
/
/
620
1.77
63.8
2575
Continental C-85-8F Evra
D11-28-1B
Jodel
D11
68.3 /61.2 / D
/
/
620
1.8
66.8
2500
76.4Continental C-90-8F,12F,14F Versch. Festprop.Jodel
D11
68.3 /64.2 / C
/
/
620
1.78
66.8
2500
76.4Continental C-90-14F McCauley
1B90/CM 7152Liese Jodel D11
Jodel
D11-2
// D66.8
2500 /
/ 67.0
620
1.8
66.8
2500
76.4Continental C-90-14F Evra
D 11 28 1BLiese Jodel D11
Jodel
D11-2
// D66.8
2500 /
/ 67.0
17.03.2020 Seite 23 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
550
0
48.6
2300
76.0Continental A-65 Diverse
Festprop.
Jodel
D112
68.0 /61.4 / D
/
/
620
1.88
66.8
2400
76.4Continental C-90-8F Sensenich
74FK49
Jodel
D112
68.3 /60.2 / D
/
/
620
1.8
63.8
2400
76.4Continental C-85-8F McCauley
1B90/CM7148
Jodel
D112
68.3 /59.7 / D
/
/
620
1.67
74.9
2680
76.4Continental O-200-A Ratier
110600
Jodel
D112
68.3 /60.2 / D
/
/
620
1.775
66.8
2475
76.4Continental C-90-14F Evra
D11-28-1B
Jodel
D117
68.3 /62.2 / D
/
/
650
1.82
66.8
2475
77.1Continental C-90-12F Diverse
Festprop.
Jodel
D120
68.7 /62.2 / D
/
/
1200
1.93
133.7
2700
85.8Lycoming O-360-A1A Sensenich
M76EM8-0-62
Jodel
D140
76.0 /75.7 / B
/
/
1200
1.93
133.7
2700
85.8Lycoming IO-360B2F61 Sensenich
76EM8-0-62
Jodel
D140C
76.0 /75.6 / B
/
/
1200
1.93
133.7
2700
85.8Lycoming O-360-A3A Sensenich
76EM8-0-58Gomolzig
Jodel
D140C
76.0 /72.3 / C
/
/
1200
1.85
139.8
2500
85.8Lycoming IO-360-A1B6 MT-Propeller
MTV-18-B/185-17Gomolzig 74-0301
Jodel
D140C
// D139.8
2500 /
/ 72.7
1200
1.93
133.7
2700
85.8Lycoming IO-360-B2F6 Sensenich
76EM8-0-58Gomolzig
Jodel
D140C
76.0 /72.3 / C
/
/
1200
1.93
133.7
2600
85.8Lycoming IO-360-B2F6 Sensenich
76EM8-0-62Gomolzig
Jodel
D140C
76.0 /70.2 / D133.7
2700 /
/ 74.1
1200
1.93
133.7
2600
85.8Lycoming O-360-A3A Sensenich
76EM8-0-62Gomolzig
Jodel
D140C
76.0 /70.2 / D133.7
2600 /
/ 74.1
1200
1.88
180.0
2600
85.8Lycoming O-360-A1P MT-Propeller
MTV-12-B/188-53
Jodel
D140C
// D180.0
2600 /
/
mit Ski
76.8
1200
1.88
136.4
2500
85.8Lycoming IO-360-C1F Hartzell
HC-C2YK-1BF
Jodel
D140E
// A148.9
2700 /
/ 82.6
1200
1.93
134.2
2700
85.8Lycoming O-360-A3A Sensenich
76EM8-0-58Gomolzig 74-0301
Jodel
D140R
// D134.2
2700 /
/ 73.4
1200
1.932500
85.8Lycoming IO-360-A1D6 McCauley
B2D34C213/90DHA-16MécanAir 60-140-1000-60
Jodel
D140R
76.0 /68.7 / D
2500 /
/
960
1.815
133.7
2500
82.7Lycoming IO-360-B1B MT-Propeller
MTV-20-B/180220Gomolzig
Jodel
DR 250-160
72.8 /66.3 / D133.7
2500 /
/
17.03.2020 Seite 24 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
750
1.85
74.9
2750
79.1Continental O-200-A Diverse
Holzprop.
Jodel
DR 1050
70.0 /67.7 / C
/
/
750
1.76
74.6
2750
79.1Rolls-Royce O-200-A Evra
D 11-28-4CGomolzig DR 1050-606500
Jodel
DR 1050
// D74.6
2750 /
/ 68.6
750
1.85
74.9
2750
79.1Continental O-200-A Diverse
Metallprop.
Jodel
DR 1050
70.0 /66.8 / C
/
/
750
1.85
74.9
2750
79.1Continental O-200-A Ratier
FH 110-500R
Jodel
DR 1050
70.0 /67.7 / C
/
/
780
1.76
74.6
2750
79.7Rolls-Royce O-200-A Evra
D 11-28-4CGomolzig DR 1050-606500
Jodel
DR 1050 M1
// D74.6
2750 /
/ 68.6
780
1.85
74.9
2750
79.7Continental O-200-A Hoffmann
HO-14-170S-123
Jodel
DR 1050 M1
70.4 /66.8 / C
/
/
750
1.7
74.5
2500
79.1Potez 4-E-20 MT-Propeller
MTV-7F-170/09
Jodel
DR 1051
// D74.5
2500 /
/ 68.3
750
1.76
78.0
2670
79.1Potez 4-E-20 Diverse
Metallprop.
Jodel
DR 1051
70.0 /66.7 / C
/
/
750
1.76
78.0
2670
79.1Potez 4-E-20 Diverse
Holzprop.
Jodel
DR 1051
70.0 /66.7 / C
/
/
780
1.74
78.0
2650
79.7Potez 4-E-20 Diverse
Festprop.
Jodel
DR 1051 M
70.4 /68.6 / B
/
/
700
1.76
73.5
2600
78.2Rolls-Royce O-200-A Evra
D11-28-4CRobin 2160
Jodel
U2V
// A73.5
2600 /
/ 72.4
700
1.74
75.0
2431
78.2Cont./Rolls-Royce O-200-A Sensenich
69CK-0-52
Jodel
U2V
69.3 /57.6 / D75.0
2431 /
/
700
1.83
75.3
2750
78.2Continental O-200-A Hoffmann
HO-14-183-11
Jodel
U2V
69.3 /69.9 / A75.3
2750 /
/
700
1.73
75.3
2750
78.2Continental O-200-A Schneider
Schneider
Jodel
U2V
69.3 /66.2 / C75.3
2750 /
/
700
1.76
75.3
2750
78.2Continental O-200-A Evra
D11-28-4C
Jodel
U2V
69.3 /69.9 / A75.3
2750 /
/
1400
2.5
186.4
1900
88.0Wright-Hispano W.-HISPANO 9Q K+W
D250/S170
K+W Thun
DEWOITINE D 26
78.7 /68.8 / D
/
/
1400
2.5
186.4
1900
88.0Wright-Hispano W.-HISPANO 9QA K+W
D250/S180
K+W Thun
DEWOITINE D 26
78.7 /68.8 / D
/
/
780
1.85
63.8
2360
79.7Hirth HM 504-A2 Hoffmann
185-123
Klemm
35
70.4 /71.3 / A
/
/
17.03.2020 Seite 25 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
540
1.93
48.6
2280
76.0Continental A-65-8 Sensenich
76C-46
Luscombe
8A
68.0 /56.9 / D
/
/
544
1.88
48.6
2300
76.0Continental A-65-8F Universal
74A-50
Luscombe
8A
68.0 /61.2 / D
/
/
57148.4
2150
76.0Continental A-65-8F McCauley
1B90/CM7447
Luscombe
8A
68.0 /60.5 / D48.4
2150 /
/
572
1.77
66.8
2475
76.0Continental C-90-8F Evra
N 177S
Luscombe
8A
68.0 /62.9 / D
/
/
635
1.8
66.8
2400
76.8Continental C-90-12F McCauley
1B90/CM7154
Luscombe
8F
68.5 /63.9 / C
/
/
600M&D Flugzeugbau GmbH & Co. KG MD-TJM&D Flugzeugbau GmbH & Co. K
JS-MD 3
// -
/
/
This aircraft type conforms with the provisions of Article 6.1 of Regulation 216/2008 without the need to comply with the Standards of ICAO Annex 16, Volume I, Chapter 10, by virtue of being a self-sustaining powered sailplane.
920
1.88
120.5
2700
82.0Lycoming O-320-D2A Sensenich
74DM6S8-0-62
M.Dätwyler
MD3-160
// C120.5
2700 /
/ 74.4
450
1.715800
65.0Rotax 914 UL Arplast
Ecoprop GL 170/3Original
MAGNI GYRO Srl
M16 Tandem Trainer
// D
5800 /
/
Prop.pitch: 12° 45'Rotor: 2 Bl. 28 ft
64.8
450
1.715500
65.0Rotax 914 UL Arplast
ECO GL 170/3 LFlorian Raboud J-RO AlpineGyro
MAGNI GYRO Srl
M24 Orion
// D
5500 /
/
Prop.pitch: 12° 45'TOP limit: 111hp@5500RPM
64.8
1380
2.358
161.9
1940
87.8Argus Motorenwerke As 10C/3 Schwarz
Me P7 Nabe:9-70-102-A-1-
Messerschmitt
ME 108 B
78.4 /73.2 / D176.6
2000 /
/
800
1.85
111.4
2570
80.1Lycoming O-340-A1A Hartzell
HC-82XG1B
Meteor
FL 55 B
70.7 /70.4 / B
/
/
900
1.88
133.7
2700
81.7Lycoming O-360-A1A McCauley
2D36C14-BRobin (modifiziert)
Meteor
FL 55 CM
72.0 /67.8 / C
/
/
580 76.0Aerotechnik CZ Mikron III AE 1 Stuecker
64A
Moravan
E 114
// -
/
/
Considered to comply with requirements by virtue of early TC date without the need to determine ist noise level.Lärmklasse A
1247
2.15
137.7
2300
86.4Continental E-185-3 Hartzell
HC-12X20
Navion
NA17(L-17A)
76.6 /80.2 / A
/
/
1247
2.13
167.1
2600
86.4Continental E-225-8 Hartzell
HC-A2V20-4Frankfurter 2x FTF 60
Navion
NAVION A (L-17B)
76.6 /75.1 / B
/
/
17.03.2020 Seite 26 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
380
1.3
18.2
2327
76.0Koenig SC430 F+E Fischer + Entw.
Faltbar
Neukom
ELFE S4A TOP
// D18.2
2327 /
/ 62.3
1050
2.01
100.3
2280
83.9Regnier 4L00 Hoffmann
HO 42HM-200S 160
Norecrin
II
74.0 /67.5 / D
/
/
HO 42HM-200 S160
1050
2.01
100.3
2280
83.9Regnier 4L00 Hoffmann
HO-42-200515
Norecrin
II
74.0 /67.5 / D
/
/
1820
2.21
193.5
1925
88.0Lycoming GO-480-B1A6 Piaggio
P1033-G4/D4
Piaggio Aero Industries S.p.A.
FW-149-D
80.0 /73.0 / D
/
/
1820
2.2
193.5
1925
88.0Lycoming GO-480-B1A6 Piaggio
P1033-G4/D4Frankfurter
Piaggio Aero Industries S.p.A.
FW-P149-D
80.0 /69.0 / D
/
/
1820
2.3
196.8
1925
88.0Lycoming GO-480-B1A6 Hartzell
HC-A3MV20-1F/MV9333N-3Gillet/Frankfurter FTF60
Piaggio Aero Industries S.p.A.
FW-P149-D
// D204.3
2182 /
/ 74.1
610
1.78
66.8
2475
76.2Continental C-90-14F MT-Propeller
MT 178R 120-2C
Piel
CP 301 A
68.1 /64.9 / C
/
/
610
1.77
66.8
2475
76.2Continental C-90-14F Hoffmann
HO 14-183 110
Piel
CP 301 A
68.1 /66.3 / B
/
/
610
1.7
74.9
2510
76.2Continental O-200-A McCauley
1A100/MCM6758
Piel
CP 301 E
68.1 /63.6 / C
/
/
1920
2.59
179.3
1880
88.0Walter Motoren AS-410-A2 Argus
L-22
Pilatus
P2-05/06
80.0 /71.2 / D
/
/
1575
2.2
179.3
1925
88.0Lycoming GO-435-C2A Hartzell
HC-83V20-2C1
Pilatus
P3-03,-05
// D182.6
1990 /
/ 81.5
1900
2.36
410.3
2200
88.0Pratt & Whitney PT6A-25A Hartzell
HC-B3TN-2
Pilatus
PC-7
80.0 /73.0 / D410.3
2200 /
/
2700
2.36
410.3
2200
88.0Pratt & Whitney PT6A-25A Hartzell
HC-B3TN-2
Pilatus
PC-7
80.0 /79.2 / B
/
/
2350
2.44
521.7
2000
88.0Pratt & Whitney PT6A-25C Hartzell
HC-D4N-2A/D
Pilatus
PC-7 MKII
// D521.7
2000 /
/
Version Propeller HC-D4N-2E: Gemäss Gerätekennblatt F56-25 ist min. pitch bei -2A 14°, bei -2E 16°. Sonst identisch. Für -2E no acustical change
75.8
2700
2.44
522.0
2000
88.0Pratt & Whitney PT6A-25C Hartzell
HC-D4N-2A
Pilatus
PC-7 MKII
// D522.0
2000 /
/
mit Niederdruck-Reifen
78.1
2850
2.44
522.0
2000
88.0Pratt & Whitney PT6A-25C Hartzell
HC-D4N-2A
Pilatus
PC-7 MKII
// D522.0
2000 /
/
mit Hochdruck-Reifen, Version Propeller HC-D4N-2E: Gemäss Gerätekennblatt F56-25 ist min. pitch bei -2A 14°, bei -2E 16°. Sonst identisch. Für -2E no acustical change
78.6
17.03.2020 Seite 27 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
2350
2.438
671.1
2000
88.0Pratt & Whitney PT6A-62 Hartzell
HC-D4N-2A/D9512A
Pilatus
PC-9 (M)
// D708.4
2000 /
/ 78.6
3200
2.442
671.1
2000
88.0Pratt & Whitney PT6A-62 Hartzell
HC-D4N-2A/D9512A
Pilatus
PC-9 (M)
// C708.4
2000 /
/ 84.6
2200
2.43
708.2
1996
88.0Pratt & Whitney PT6A-62 Hartzell
HC-D4N-2A
Pilatus
PC-9*
80.0 /72.8 / D708.2
1996 /
/
3100
2.67
1193.0
2000
85.0Pratt & Whitney PT6A-68B Hartzell
HC-E5A-2/E9193B(K)
Pilatus
PC-21
// D1193.0
2000 /
/ 79.0
3100
2.67
1193.0
2000
85.0Pratt & Whitney PT6A-68B Hartzell
HC-E5A-2/E9193B(K)
Pilatus
PC-21
// D1193.0
2000 /
/
with External Smoke Generators
82.3
3600
2.67
1193.0
2000
85.0Pratt & Whitney PT6A-68B Hartzell
HC-E5A-2/E9193B(K)
Pilatus
PC-21
// D1193.0
2000 /
/
Underwing Fuel Tanks
82.3
3780
2.67
1193.0
2000
85.0Pratt & Whitney PT6A-68B Hartzell
HC-E5A-2/E9193B(K)
Pilatus
PC-21
// C1193.0
2000 /
/
Underwing Fuel Tanks
83.5
550
0
48.6
2300
76.0Continental A-65 Diverse
Festprop.
Piper
J3C
68.0 /67.9 / B
/
/
553
1.83
48.6
2300
76.0Continental A-65-8 Sensenich
43K10107
Piper
J3C
68.0 /67.9 / B
/
/
553
1.83
48.6
2300
76.0Continental A-65-1 Sensenich
W72CK-42
Piper
J3C
68.0 /67.9 / B
/
/
553
1.78
48.6
2300
76.0Continental A-65-1 Hoffmann
HO 17-178 100
Piper
J3C
68.0 /67.9 / B
/
/
553
1.83
66.8
2475
76.0Continental C-90-12F Hoffmann
Ho 14-183 100
Piper
J3C
68.0 /64.9 / C
/
/
553
1.8
66.8
2475
76.0Continental C-90-12F McCauley
1B90/CM7146
Piper
J3C
68.0 /64.9 / C
/
/
553
188
48.6
2300
76.0Continental A-65-8 McCauley
1B90/CM7443
Piper
J3C
68.0 /67.9 / B
/
/
580
1.78
66.8
2475
Continental C-90-12F MT-Propeller
MT 178R110-2C
Piper
J3C
68.0 /64.9 / C
/
/
580
1.88
67.1
2475
76.0Cont./Rolls-Royce C-90-14F Sensenich
76 AK-2-40Liese Typ D76(-2)
Piper
J3C
// C67.1
2475 /
/ 69.2
580
1.83
66.8
2475
Continental C-90-12F MT-Propeller
MT 183R118-2C
Piper
J3C
68.0 /64.9 / C
/
/
17.03.2020 Seite 28 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
580
0
63.8
2525
76.0Continental C-85-8 Diverse
Festprop.
Piper
J3C
68.0 /66.0 / C
/
/
580
0
66.8
2475
76.0Continental C-90-8F Diverse
Festprop.
Piper
J3C
68.0 /64.9 / C
/
/
580
1.8
74.9
2750
76.0Continental O-200-A MT-Propeller
183R100-2C
Piper
J3C
68.0 /68.1 / A
/
/
580
1.88
74.9
2560
76.0Continental O-200-A Diverse
Festprop.
Piper
J3C
68.0 /66.1 / B
/
/
580
1.83
66.8
2475
76.0Continental C-90-12F MT-Propeller
MT 183R100-2C
Piper
J3C
68.0 /64.9 / C
/
/
580
1.8
74.9
2750
76.0Continental O-200-A Diverse
Festprop.
Piper
J3C
68.0 /68.1 / A
/
/
580
1.83
66.8
2475
Continental C-90-12F Sensenich
W72GK-48
Piper
J3C-65/L-4.
68.0 /64.9 / C
/
/
580
1.83
66.8
2475
Continental C-90-12F MT-Propeller
MT 183R100-2C
Piper
J3C-65/L-4.
68.0 /64.9 / C
/
/
580
1.83
66.8
2475
76.0Continental C-90-12F Sensenich
W72GK-50
Piper
J3C-65/L-4.
68.0 /64.9 / C
/
/
580
1.83
66.8
2475
Continental C-90-14F Sensenich
W72GK-48
Piper
J3C-65/L-4.
68.0 /64.9 / C
/
/
795
1.88
100.3
2600
80.0Lycoming O-290-D2 Sensenich
M74DM
Piper
PA-12
70.6 /68.6 / C
/
/
795
1.88
100.3
2600
80.0Lycoming O-290-D2 McCauley
1A170/DM 7445
Piper
PA-12
70.6 /68.6 / C
/
/
748
1.88
111.4
2620
79.1Lycoming O-320-A2B Sensenich
74DM6-0-56
Piper
PA-16
70.0 /70.0 / B
/
/
750
1.88
100.3
2450
79.1Lycoming O-290-D2 Sensenich
M74DM52
Piper
PA-16
70.0 /64.5 / D
/
/
680
1.82
66.8
2475
77.8Continental C-90-8F Sensenich
W72GK-50
Piper
PA-18
69.1 /65.4 / C
/
/
680
1.88
66.8
2475
77.8Continental C-90-14F Sensenich
76AK-2-42
Piper
PA-18
69.1 /65.4 / C
/
/
680
1.75
66.8
2475
77.8Continental C-90-8F McCauley
1A101/DCM6948
Piper
PA-18
69.1 /60.8 / D
/
/
680
1.93
66.8
2475
77.8Continental C-90-8F Sensenich
M76-AK
Piper
PA-18
69.1 /64.8 / C
/
/
17.03.2020 Seite 29 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
680
1.88
93.2
2600
77.8Lycoming O-290-D Sensenich
74DM6-0-52
Piper
PA-18-125
69.1 /65.1 / C
/
/
680
1.88
100.3
2600
77.8Lycoming O-290-D2 Sensenich
74DM6-0-52
Piper
PA-18-135
69.1 /65.0 / C
/
/
794
1.88
111.4
2690
80.0Lycoming O-320-A2B Sensenich
74DM6-0-56MEIGA/Wülsag
Piper
PA-18-150
70.6 /63.1 / D
/
/
794
1.88
111.4
2700
80.0Lycoming O-320-A2B Sensenich
M74DM6-0-56
Piper
PA-18-150
70.6 /65.6 / D111.4
2700 /
/
794
1.88
111.4
2620
80.0Lycoming O-320-A2B Sensenich
74DM6-0-50Balmer
Piper
PA-18-150
70.6 /66.7 / C
/
/
794
1.88
111.4
2700
80.0Lycoming O-320-A2B Sensenich
M74DM-0-50; -52; -54
Piper
PA-18-150
70.6 /66.6 / C
/
/
794
1.7
111.8
2700
80.0Lycoming O-320-A2B Hoffmann
HO4/23AHM-A170 105
Piper
PA-18-150
// D111.8
2700 /
/ 70.2
794
1.88
111.4
2700
80.0Lycoming O-320-A2B Sensenich
74DM6-0-58
Piper
PA-18-150
70.6 /65.6 / D111.4
2700 /
/
794
1.88
119.5
2700
80.0Lycoming O-320-B2B Sensenich
74DM6-0-56
Piper
PA-18-150
70.6 /64.6 / D
/
/
794
1.88
112.0
2700
80.0Lycoming O-320-A2A Sensenich
M74 DM-0-52Gomolzig 74-0201
Piper
PA-18-150
// D112.0
2700 /
/ 69.1
794
1.88
111.4
2700
80.0Lycoming O-320-A2B Sensenich
74DM6-0-60
Piper
PA-18-150
70.6 /65.6 / C111.4
2700 /
/
795
1.88
111.4
2700
80.0Lycoming O-320-A2B Sensenich
74DM6-0-50MécanAir
Piper
PA-18-150
70.6 /67.6 / C
/
/
907
1.88
111.4
2700
81.8Lycoming O-320-A2B Sensenich
M74DM-0-50; -52; -54
Piper
PA-18-150
72.1 /66.6 / D
/
/
907
2.08
111.4
2700
81.8Lycoming O-320-B1A McCauley
1A175/GM8244
Piper
PA-18-150
// -111.4
2700 /
/
By virtue of the date of type certification this aircraft type is in accordance with the provisions of Article 1b of the regulation on the emission of aircraft (VEL, SR 748.215.3) without the need to comply with the Standards of ICAO Annex 16, Volume I.
794
1.88
119.5
2700
80.0Lycoming O-320-D2A Sensenich
74DM6-0-56
Piper
PA-18-150/160
70.6 /64.6 / D
/
/
907
1.88
119.5
2700
81.8Lycoming O-320-B2B Sensenich
74DM6-0-56
Piper
PA-18-150/160
72.1 /66.4 / D
/
/
793
1.7
133.7
2700
79.9Lycoming O-360-A2A Hoffmann
HO4/27HM-170120
Piper
PA-18-180
70.6 /64.3 / D133.7
2700 /
/ 65.6
17.03.2020 Seite 30 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
794
1.83
134.2
2700
80.0Lycoming O-360-C1G MT-Propeller
MTV-14-B/183-301aLiese V76-PA18
Piper
PA-18-180
// C134.2
2700 /
/ 72.1
794
2.08
133.7
2700
Lycoming O-360-A2A McCauley
1A200/FA8243
Piper
PA-18-180
70.6 /74.0 / A
/
/
794
1.93
133.7
2680
80.0Lycoming O-360-A2A Sensenich
76EM8S5-0-55
Piper
PA-18-180
70.6 /68.0 / C
/
/
794
1.7
133.7
2700
80.0Lycoming O-360-A1F6 Hoffmann
HO4/27HM-170125MEIGA/Wülsag
Piper
PA-18-180
70.6 /62.9 / D133.7
2700 /
/
906
1.93
133.7
2700
81.8Lycoming O-360-A3A Sensenich
76EM8-0-52
Piper
PA-18-180 (USA STC)
// D133.7
2700 /
/ 68.3
907
1.93
133.7
2700
81.8Lycoming O-360-A3A Sensenich
76EM8S5-0-55Gomolzig
Piper
PA-18-180 (USA STC)
// D133.7
2700 /
/ 68.3
794
1.7
133.7
2700
80.0Lycoming O-360-A4A Hoffmann
HO4/27HM-170....MécanAir
Piper
PA-18-180M
70.6 /61.4 / D
/
/
794
1.7
134.2
2700
80.0Lycoming O-360-A3A Hoffmann
HO4/27HM-170 110Gomolzig PA18-606500
Piper
PA-18-180M
// D134.2
2700 /
/ 65.9
794
1.7
134.2
2700
80.0Lycoming O-360-A3A Hoffmann
HO4/27HM-170 110MécanAir
Piper
PA-18-180M
// D134.2
2700 /
/ 68.1
794
1.7
134.2
2700
80.0Lycoming O-360-A3A Hoffmann
HO4/27HM-170-125MécanAir
Piper
PA-18-180M
// D134.2
2700 /
/ 69.2
907
1.7
133.7
2700
81.8Lycoming O-360-A4A Hoffmann
HO4/27HM-170 120MécanAir
Piper
PA-18-180M
72.1 /61.4 / D
/
/
680
1.88
66.8
2475
77.8Continental C-90-8F McCauley
1B90/CM7150
Piper
PA-18
69.1 /62.1 / D
/
/
680
1.88
66.8
2475
77.8Continental C-90-8F McCauley
1B90/CM7150Frankfurter
Piper
PA-18
69.1 /58.6 / D
/
/
680
1.88
66.8
2475
77.8Continental C-90-14F McCauley
1B90/CM7146Frankfurter
Piper
PA-18
69.1 /58.6 / D
/
/
681
1.88
67.1
2475
77.8Continental C-90-14E Sensenich
M76AK-2-42Liese D76-2
Piper
PA-18
// D67.1
2475 /
/ 67.4
680
1.93
66.8
2475
77.8Continental C-90-8F Sensenich
M76AK2
Piper
PA-19
69.1 /66.4 / C
/
/
680
1.88
66.8
2475
77.8Continental C-90-8F Sensenich
M76AK2Frankfurter
Piper
PA-19
69.1 /58.6 / D
/
/
680
1.88
66.8
2475
77.8Continental C-90-14F Sensenich
M76AK2Frankfurter
Piper
PA-19
69.1 /58.6 / D
/
/
17.03.2020 Seite 31 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
750
1.88
80.0
2600
79.1Lycoming O-235-C1B Sensenich
M76-AM2
Piper
PA-22-108
70.0 /68.2 / B
/
/
885
1.88
100.3
2550
81.5Lycoming O-290-D2 Sensenich
M74DM
Piper
PA-22-135
71.8 /65.8 / D
/
/
907
1.88
111.4
2610
81.8Lycoming O-320-A Sensenich
M74DM6-0-56
Piper
PA-22-150
72.1 /70.8 / B
/
/
1588
1.82
111.4
2700
88.0Lycoming O-320-A3A Hartzell
HC-82XL-2C
Piper
PA-23
80.0 /77.0 / C
/
/
1724
1.82
119.5
2630
88.0Lycoming O-320-B1A Hartzell
HC-82XG-2B
Piper
PA-23-160
80.0 /72.0 / D
/
/
794
1.88
112.0
2700
80.0Lycoming O-320-A2B Sensenich
(M)74DM6-()-52Liese V-76
Piper
PA-18-150
// D112.0
2700 /
/ 68.7
794
1.88
112.0
2700
80.0Lycoming O-320-A2B Sensenich
(M)74DM6-()-56Liese V-76
Piper
PA-18-150
// D112.0
2700 /
/ 68.7
794
1.88
112.0
2700
80.0Lycoming O-320-A2B Sensenich
(M)74DM6-()-54Liese V-76
Piper
PA-18-150
// D112.0
2700 /
/ 70.0
794
1.88
112.0
2700
80.0Lycoming O-320-A2B Sensenich
(M)74DM6-()-54Gomolzig PA18-606500
Piper
PA-18-150
// D112.0
2700 /
/ 67.4
794
1.88
112.0
2700
80.0Lycoming O-320-A2B Sensenich
(M)74DM6-()-56Gomolzig Typ 3/PA18
Piper
PA-18-150
// D112.0
2700 /
/ 66.2
472.5
1.675350
65.0Rotax 912 UL Pipistrel
VarioAkrapovic Titanium
Pipistrel
Sinus
// D
5350 /
/ 61.2
472.5
1.66500
65.0Rotax 503 UL DCDI 2V Pipistrel
Caliber 2 (Wood)
Pipistrel
Taurus
// D
6500 /
/ 65.0
600
1.745800
70.8Rotax 912 ULS2 Woodcomp
SR3000Original
Pipistrel
Virus SW
// A
5800 /
/ 70.8
600
1.75800
70.8Rotax 912 ULS2 MT-Propeller
MTV-33-1-A/170-200Original
Pipistrel
Virus SW
// A
5800 /
/ 70.8
1030
1.82
119.5
2700
83.6Lycoming O-320-B2A Hartzell
HC-82XL-1D
Procaer
F 15
73.7 /72.3 / B
/
/
1120
1.82
133.7
2700
84.8Lycoming O-360-A1A Hartzell
HC-92ZK-8D
Procaer
F 15 B
74.9 /72.9 / C
/
/
472.5
1.6955200
65.0Rotax 912 ULS GT Propellers
GT-164
Remos
G-3/600
// D
/
/ 58.5
1429
2.1342450
88.0Franklin 6A8-215-9BF Hartzell
HC-D2MV20-3-
Republic Aviation Corporation
RC-3 (Seabee)
79.0 /78.0 / B
2450 /
/
17.03.2020 Seite 32 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
2000
2.91
330.9
1800
85.0Pratt & Whitney R-985-AN-14B MT-Propeller
5406/A1C1-6Original
Rimowa Flugzeugwerke AG
Junkers F13
// D330.9
1800 /
/ 81.7
400
1.78
48.6
2300
76.0Continental A-65-8F Hoffmann
HO-14-178-100
Roesgen
EPR 301
68.0 /66.0 / C
/
/
860
1.9
108.1
2700
81.1Continental O-300-A McCauley
1A170/DM7649Balmer
S.A.I.
KZ VII
// D108.1
2700 /
/ 71.8
860
1.9
108.4
2420
81.1Continental C-145-2 Koppers
F200/00-74E
S.A.I.
KZ VII
71.5 /72.0 / A
/
/
860
1.9
108.4
2700
81.1Continental O-300-A Hoffmann
HO-30-190-12Balmer
S.A.I.
KZ VII
71.5 /73.5 / A
/
/
860
1.9
108.4
2520
81.1Continental C-145-2 Hoffmann
HO-30-190-12
S.A.I.
KZ VII
71.5 /72.4 / A
/
/
860
1.9
108.1
2700
81.1Continental O-300-A Hoffmann
HO-30-190-12Balmer
S.A.I.
KZ VII
// C108.1
2700 /
/ 72.4
860
1.9
108.4
2520
81.1Continental C-145-2 McCauley
1A170/DM7649
S.A.I.
KZ VII
// -
/
/
Lärmklasse A
1205
1.88
133.7
2700
85.9Lycoming O-360-A1A McCauley
2D36C14/78KM-4
Saab
91 D
76.1 /77.2 / A
/
/
1205
1.8
148.9
2700
85.9Lycoming IO-360-C1C Hoffmann
HO-V123K/180
Saab
91 D
76.1 /76.2 / A
/
/
670
1.78
66.8
2460
77.5Continental C-90-14F Evra
D11-28-1BMécanAir
Sipa
903
68.9 /64.9 / C
/
/
670
1.77
66.8
2500
77.5Continental C-90-14F Hoffmann
HO-14-178-120
Sipa
903
68.9 /68.0 / B
/
/
670
1.78
66.8
2475
77.5Continental C-90-14F Evra
D11-28-1B
Sipa
903
68.9 /70.1 / A
/
/
670
1.775
66.8
2320
77.5Continental C-90-14F Evra
D11-28-1BSAB
Sipa
903
// D66.8
2320 /
/ 68.4
770
1.99
104.3
2200
79.5Renault 4P05 Hoffmann
HO-34HM-198SAndere
SNCAN
STAMPE SV4A
70.3 /61.9 / D
/
/
770
1.99
104.3
2200
79.5Renault 4P05 Hoffmann
HO-34HM-L98S
SNCAN
STAMPE SV4A
70.3 /71.2 / A
/
/
825
1.98
103.0
1900
80.5Renault 4P03 Merville
745Bornand DBO-01
SNCAN
STAMPE SV4C
// D103.0
1900 /
/ 69.6
825
1.98
104.3
2200
80.5Renault 4P03 Poncelet
HL 2011
SNCAN
STAMPE SV4C
71.0 /71.0 / B
/
/
17.03.2020 Seite 33 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
1100
2.42
164.1
2075
84.6Continental W670-6A Evra
HL 21552
Socata
MS 317
74.7 /70.9 / C
/
/
1100
2.42
164.1
2075
84.6Continental W670-6A Evra
120-55-B7
Socata
MS 317
74.7 /70.9 / C
/
/
1590Argus Motorenwerke AS-10 C3B MT-Propeller
MT 256 R 140-6ABOriginal
Socata
MS 500
// -
/
/
LK: A
1590
2.55
Moteurs Salmson 9-ABC Helices Pignolo
M-DA 255/260Original
Socata
MS 502
// -
/
/
LK: A
1490
2.09
172.8
2550
88.0Lycoming O-540-E4B5 Hartzell
HC-C2YK-1BFGomolzig Maule 606 050
Socata
MS 505
// C172.8
2550 /
/ 84.3
1590Argus Motorenwerke AS-10 C3B MT-Propeller
MT 256 R 140-6APOriginal
Socata
MS 505
// -
/
/
LK: A
1590Argus Motorenwerke AS-10 C3B Hoffmann
HO 82-256B 114Original
Socata
MS 505
// -
/
/
1590
2.6
226.9
1950
88.0Jacobs R-755A2 Evra
130-38-29
Socata
MS 505
80.0 /73.9 / D
/
/
1590
2.09
172.8
2550
88.0Lycoming O-540-E4B5 Hartzell
HC-C2YK-1BFGomolzig Maule 606 050
Socata
MS 505
// C172.8
2550 /
/ 84.3
1800
2.13
171.2
2500
88.0Potez 6D02 Hartzell
HC-B3Z22-7
Socata
MS 733
80.0 /77.7 / C
/
/
1724
1.88
134.2
2700
88.0Lycoming IO-360-B1D Hartzell
HC-C2YK-2RB/7666A-2
STOL Aircraft.
UC-1 TWIN BEE
// D134.2
2700 /
/ 78.8
485
1.65
48.6
2200
76.0Continental A-65 Merville
693 B
Sud Aviation
GY-20
68.0 /63.3 / C
/
/
515
1.8
48.6
2200
76.0Continental A-65 McCauley
1B90/CM7150
Sud Aviation
GY-20-1
68.0 /63.3 / C
/
/
720
1.88
105.0
2700
78.6LOM M332AK MT-Propeller
MT 188L115-6AZLiese Beech 35
Tatra
T-131 PA Jungmann
// C105.0
2700 /
/ 71.5
870
1.88
111.4
2700
81.3Lycoming O-290-D2B Sensenich
M74DM56
Uetz
U3M PELIKAN
71.6 /71.0 / B
/
/
999
1.82700
83.2Lycoming IO-320-B1A Hoffmann
HO-V72L2/180DULiese 76/150
Uetz
U4M PELIKAN
73.3 /75.8 / A
2700 /
/
1000
1.88
111.4
2700
83.2Lycoming O-320-A2B McCauley
1C172/MGM7460
Uetz
U4M PELIKAN
73.3 /75.9 / A
/
/
17.03.2020 Seite 34 von 35FOCA Noise Annex II/
FlugzeugherstellerMuster
Motor
Schalldämpfer
PropellerherstellerMuster Leistung [kW]
Drehz. [1/min]
MTOM [kg] PegelKap.6 / Kap. 10
[dB(A)]
GrenzwertKap.6 / Kap. 10
[dB(A)]
Geb.-klasseProp.-
durchm. [m]
Start- / Dauer-
Start- / Dauer-
1000
1.82
111.4
2700
83.2Lycoming O-320-A2B Hartzell
HC-C2YL-1B
Uetz
U4M PELIKAN
73.3 /72.9 / B
/
/
700
2.03
148.9
2600
78.2Franklin 6A-350-C1 Hartzell
HC-C2YF-4
Wolf Hirth
HI-27 MK II
69.3 /69.4 / A
/
/
1316
2.4
161.0
2050
87.1WSK AI-14 R Vpered Moscow
B530-A35Original
Yakovlev Design Bureau
YAK-18A
// C191.0
2350 /
/ 80.8
17.03.2020 Seite 35 von 35FOCA Noise Annex II/
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