Annex II Propellerflugzeuge, Motorsegler und Tragschrauber ......American Champion Aircraft Corp 7ECA 66.0/ C70.0/ / / 750 1.88 111.4 2700 Lycoming O-320-A2B McCauley 79.1 Frankfurter

Propellerflugzeuge, Motorsegler und Tragschrauber bis 8'618kg MTOM

Annex II

Mühlestrasse 2, 3096 Bern (Schweiz) Telefon +41 31 325 8039/40 Fax +41 31 325 9212

Eidgenössisches Departement für Umwelt, Verkehr, Energie und Kommunikation UVEK

Bundesamt für Zivilluftfahrt

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


7ECA

70.0 /66.0 / C

/

/

750

1.88

111.4

2700

79.1Lycoming O-320-A2B McCauley

1A170/7448Frankfurter


7GCB

70.0 /68.0 / C

/

/

612

1.782490

76.3Rolls-Royce O-200-A MT-Propeller

MT 178R 110-2C


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


1A100/MCM6758

Binder

CP301S "SMARAGD"

69.1 /67.3 / B

/

/

680

1.83

66.8

2475


F-H2LC1418311

Binder

CP301S "SMARAGD"

69.1 /70.3 / A

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


HO-23A-188125MécanAir

Bücker

131

// C111.8

2700 /

/ 70.8

670

1.88

111.8

2700


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


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


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


140

68.8 /70.4 / A

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[dB(A)]

Geb.-klasseProp.-

durchm. [m]

Start- / Dauer-

Start- / Dauer-

660

1.879

67.0

2350


M76-AK


140

68.8 /65.3 / C

/

/

660

1.8

63.8

2500


1A90/CF7150


140

68.8 /70.4 / A

/

/

660

1.75

74.9

2750

77.3Cont./Rolls-Royce O-200-A Sensenich

M69CK52


140

68.8 /69.0 / A

/

/

660

1.8

80.0

2600

77.3Lycoming O-235-K2A Sensenich

72CK-0-56


140

68.8 /70.4 / A

/

/

680

1.8

66.8

2475


1B90/CM7146


140 A

69.1 /66.5 / C

/

/

998

1.952450

83.2Lycoming O-360-A4M Sensenich

76EM8S5-0-60


170 A

73.3 /66.1 / D

2450 /

/

998

1.82

126.6

2700

83.2Lycoming O-340-A1A Hartzell

HC-A2XL-1


170 A

73.3 /71.6 / B

/

/

998

1.952450

83.2Lycoming O-360-A3A Sensenich

76EM8S5-0-60


170 B

73.3 /66.1 / D

2450 /

/

998

1.88

133.7

2700


HC-C2YK-1


170 B

73.3 /71.9 / B

/

/

998

1.93

109.6

2700


1A170/DM7653Liese 2 x D76


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


170,-A,-B

// D109.6

2700 /

/ 73.2

1000

1.93

108.4

2580


1A170/DM7653


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[dB(A)]

Geb.-klasseProp.-

durchm. [m]

Start- / Dauer-

Start- / Dauer-

520

1.725800



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



ELA Aviacion S.L

ELA 10 Eclipse

// D

5800 /

/

Prop.pitch: 22.5°

62.3

572

1.8

66.8

2475


1A90/CF7144

Ercoupe

415 C

68.0 /68.7 / A

/

/

635

1.8

66.8

2450


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


HO-14-178-120

Experimental

AERO 101

68.0 /70.4 / A

/

/

580

1.93

66.8

2280


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


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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


ARPLAST Ecoprop

Experimental

BX-2

// D60.4

2551 /

/ 64.4

550

1.75500


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


SR3000/3Rotax/Aerotec

Experimental

BX-2

// D73.0

5225 /

/ 64.0



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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.



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[dB(A)]

Geb.-klasseProp.-

durchm. [m]

Start- / Dauer-

Start- / Dauer-

590

1.6

73.5

5500


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


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


HC-C2YK-1

Experimental

GLASAIR RG

71.5 /70.5 / B134.2

2700 /

/

862

1.88

133.7

2700


HC-C2YK-1MécanAir

Experimental

GLASAIR RG

71.5 /69.8 / B133.7

2700 /

/

862

1.88

128.2

2500


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[dB(A)]

Geb.-klasseProp.-

durchm. [m]

Start- / Dauer-

Start- / Dauer-

544

1.78

56.0

2288


IVO-PropellerSkystar

Experimental

KiTFOX IV-1200 Speedster

// D56.0

2288 /

/

Prop. Einstellung auf 9°

65.9

544

1.734

58.8

2420


IVO-Propeller

Experimental

KiTFOX IV-1200 Speedster

// D58.9

2420 /

/ 64.8

500

1.752420


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


175DWAMSkystar

Experimental

KITFOX 5

// D59.6

2420 /

/ 66.2

703

1.75600


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


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


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


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


HO-02-136B75

Experimental

KOLIBRI MB2

68.0 /62.1 / D

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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 /

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


MTV 7-A/152-106Dyn-Aero MMOMOE 101

Experimental

Dyn-Aero MCR-01

// C58.0

2420 /

/ 66.9

490

1.52

60.5

5800


MTV 6-A/152-106Chabord EV1

Experimental

Dyn-Aero MCR-01

// C60.5

5800 /

/ 67.0

490

1.52

60.5

5800



Experimental

Dyn-Aero MCR-01

// C60.5

5800 /

/ 67.0



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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



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


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


MTV 7-A/152-106Eigenbau

Experimental

PULSAR XP

// D59.6

2420 /

/ 61.9

505

1.75500


VAR2Aerodesigns Pulsar XP

Experimental

PULSAR XP

// D

5500 /

/ 64.6

505

1.52

59.6

2420


MTV 7-A/152-106Eigenbau

Experimental

PULSAR XP

// D59.6

2420 /

/ 62.6



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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


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


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


HO-11-137B85

Experimental

TIPSY N. MK II

68.0 /62.0 / D

/

/

300

1.37

32.4

2900


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


MTV-1-F

Experimental

VARI EZE

68.0 /63.3 / C75.9

2750 /

/

550

1.53

75.9

2750


MTV-1-F

Experimental

VARI EZE

68.0 /64.1 / C75.9

2750 /

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


Experimental

Votec 322

// D231.0

2500 /

/ 68.7

950

1.952500

82.5Lycoming YAEIO-580-EXP MT-Propeller


Experimental

Votec 322

// D

2500 /

/ 68.7

950

2.032500

77.9Lycoming AEIO-540-X MT-Propeller


Experimental

Votec 322

// D

2500 /

/ 72.8

950

1.95

240.0

2650

82.5Lycoming AEIO-540-C1B MT-Propeller


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


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


HC-C2YL-1BRobin (modifiziert)

Falco

F8L

70.9 /70.2 / B

/

/

820

1.82

111.4

2700


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


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

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


A35

76.0 /67.5 / D

/

/

1225

2.23

137.7

2300

86.1Continental E-185-11 Beech

215-109


C35

76.3 /72.0 / C

/

/

1236

2.23

137.7

2300


215-107


D35

76.5 /72.6 / C152.8

2600 /

/

1327

2.134

137.9

2300


A2V20-4MEIGA/Wülsag


D35

// A152.8

2600 /

/ 86.3

1250

2.13

137.7

2300


HC-A2X20-4A1


F35

76.7 /69.8 / D

/

/

1350

2.13

137.7

2300


215-107


G35

78.0 /68.8 / D

/

/

965

1.93

134.2

2700


76EM8S5-0-56Gomolzig JOB15-606500

Job

15-180/2

// D134.2

2700 /

/ 68.9

965

1.93

134.2

2700


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


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


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


1B90/CM 7152Liese Jodel D11

Jodel

D11-2

// D66.8

2500 /

/ 67.0

620

1.8

66.8

2500


D 11 28 1BLiese Jodel D11

Jodel

D11-2

// D66.8

2500 /

/ 67.0



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


74FK49

Jodel

D112

68.3 /60.2 / D

/

/

620

1.8

63.8

2400


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


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


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


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


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


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 /

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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


Holzprop.

Jodel

DR 1051

70.0 /66.7 / C

/

/

780

1.74

78.0

2650


Festprop.

Jodel

DR 1051 M

70.4 /68.6 / B

/

/

700

1.76

73.5

2600


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


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

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[dB(A)]

Geb.-klasseProp.-

durchm. [m]

Start- / Dauer-

Start- / Dauer-

540

1.93

48.6

2280


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


N 177S

Luscombe

8A

68.0 /62.9 / D

/

/

635

1.8

66.8

2400


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


74DM6S8-0-62

M.Dätwyler

MD3-160

// C120.5

2700 /

/ 74.4

450

1.715800


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


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


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


HC-12X20

Navion

NA17(L-17A)

76.6 /80.2 / A

/

/

1247

2.13

167.1

2600


HC-A2V20-4Frankfurter 2x FTF 60

Navion

NAVION A (L-17B)

76.6 /75.1 / B

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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


HO 14-183 110

Piel

CP 301 A

68.1 /66.3 / B

/

/

610

1.7

74.9

2510


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


HC-D4N-2A

Pilatus

PC-7 MKII

// D522.0

2000 /

/

mit Niederdruck-Reifen

78.1

2850

2.44

522.0

2000


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[dB(A)]

Geb.-klasseProp.-

durchm. [m]

Start- / Dauer-

Start- / Dauer-

2350

2.438

671.1

2000


HC-D4N-2A/D9512A

Pilatus

PC-9 (M)

// D708.4

2000 /

/ 78.6

3200

2.442

671.1

2000


HC-D4N-2A/D9512A

Pilatus

PC-9 (M)

// C708.4

2000 /

/ 84.6

2200

2.43

708.2

1996


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


HC-E5A-2/E9193B(K)

Pilatus

PC-21

// D1193.0

2000 /

/

with External Smoke Generators

82.3

3600

2.67

1193.0

2000


HC-E5A-2/E9193B(K)

Pilatus

PC-21

// D1193.0

2000 /

/

Underwing Fuel Tanks

82.3

3780

2.67

1193.0

2000


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


43K10107

Piper

J3C

68.0 /67.9 / B

/

/

553

1.83

48.6

2300


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


Ho 14-183 100

Piper

J3C

68.0 /64.9 / C

/

/

553

1.8

66.8

2475


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


MT 183R118-2C

Piper

J3C

68.0 /64.9 / C

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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


MT 183R100-2C

Piper

J3C-65/L-4.

68.0 /64.9 / C

/

/

580

1.83

66.8

2475


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


M74DM52

Piper

PA-16

70.0 /64.5 / D

/

/

680

1.82

66.8

2475


W72GK-50

Piper

PA-18

69.1 /65.4 / C

/

/

680

1.88

66.8

2475


76AK-2-42

Piper

PA-18

69.1 /65.4 / C

/

/

680

1.75

66.8

2475


1A101/DCM6948

Piper

PA-18

69.1 /60.8 / D

/

/

680

1.93

66.8

2475


M76-AK

Piper

PA-18

69.1 /64.8 / C

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


74DM6-0-52

Piper

PA-18-135

69.1 /65.0 / C

/

/

794

1.88

111.4

2690


74DM6-0-56MEIGA/Wülsag

Piper

PA-18-150

70.6 /63.1 / D

/

/

794

1.88

111.4

2700


M74DM6-0-56

Piper

PA-18-150

70.6 /65.6 / D111.4

2700 /

/

794

1.88

111.4

2620


74DM6-0-50Balmer

Piper

PA-18-150

70.6 /66.7 / C

/

/

794

1.88

111.4

2700


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


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


M74 DM-0-52Gomolzig 74-0201

Piper

PA-18-150

// D112.0

2700 /

/ 69.1

794

1.88

111.4

2700


74DM6-0-60

Piper

PA-18-150

70.6 /65.6 / C111.4

2700 /

/

795

1.88

111.4

2700


74DM6-0-50MécanAir

Piper

PA-18-150

70.6 /67.6 / C

/

/

907

1.88

111.4

2700


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


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



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


76EM8-0-52

Piper

PA-18-180 (USA STC)

// D133.7

2700 /

/ 68.3

907

1.93

133.7

2700


76EM8S5-0-55Gomolzig

Piper

PA-18-180 (USA STC)

// D133.7

2700 /

/ 68.3

794

1.7

133.7

2700


HO4/27HM-170....MécanAir

Piper

PA-18-180M

70.6 /61.4 / D

/

/

794

1.7

134.2

2700


HO4/27HM-170 110Gomolzig PA18-606500

Piper

PA-18-180M

// D134.2

2700 /

/ 65.9

794

1.7

134.2

2700


HO4/27HM-170 110MécanAir

Piper

PA-18-180M

// D134.2

2700 /

/ 68.1

794

1.7

134.2

2700


HO4/27HM-170-125MécanAir

Piper

PA-18-180M

// D134.2

2700 /

/ 69.2

907

1.7

133.7

2700


HO4/27HM-170 120MécanAir

Piper

PA-18-180M

72.1 /61.4 / D

/

/

680

1.88

66.8

2475


1B90/CM7150

Piper

PA-18

69.1 /62.1 / D

/

/

680

1.88

66.8

2475


1B90/CM7150Frankfurter

Piper

PA-18

69.1 /58.6 / D

/

/

680

1.88

66.8

2475


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


M76AK2

Piper

PA-19

69.1 /66.4 / C

/

/

680

1.88

66.8

2475


M76AK2Frankfurter

Piper

PA-19

69.1 /58.6 / D

/

/

680

1.88

66.8

2475


M76AK2Frankfurter

Piper

PA-19

69.1 /58.6 / D

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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


(M)74DM6-()-52Liese V-76

Piper

PA-18-150

// D112.0

2700 /

/ 68.7

794

1.88

112.0

2700


(M)74DM6-()-56Liese V-76

Piper

PA-18-150

// D112.0

2700 /

/ 68.7

794

1.88

112.0

2700


(M)74DM6-()-54Liese V-76

Piper

PA-18-150

// D112.0

2700 /

/ 70.0

794

1.88

112.0

2700


(M)74DM6-()-54Gomolzig PA18-606500

Piper

PA-18-150

// D112.0

2700 /

/ 67.4

794

1.88

112.0

2700


(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


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


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 /

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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


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


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


HO-30-190-12Balmer

S.A.I.

KZ VII

// C108.1

2700 /

/ 72.4

860

1.9

108.4

2520


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


D11-28-1BMécanAir

Sipa

903

68.9 /64.9 / C

/

/

670

1.77

66.8

2500


HO-14-178-120

Sipa

903

68.9 /68.0 / B

/

/

670

1.78

66.8

2475


D11-28-1B

Sipa

903

68.9 /70.1 / A

/

/

670

1.775

66.8

2320


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

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[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

/

/



Motor

Schalldämpfer


Drehz. [1/min]


[dB(A)]


[dB(A)]

Geb.-klasseProp.-

durchm. [m]

Start- / Dauer-

Start- / Dauer-

1000

1.82

111.4

2700


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


Documents

Annex II Propellerflugzeuge, Motorsegler und Tragschrauber ......American Champion Aircraft Corp 7ECA 66.0/ C70.0/ / / 750 1.88 111.4 2700 Lycoming O-320-A2B McCauley 79.1 Frankfurter