SSP-401 - TEXTRON LYCOMING CERTIFICATED AIRCRAFT ENGINES

2700. IOO/IOOI.I,. 8.50: I Same as O-360-A2D but with MA-4-5AA carburetor ...... HR 200'170. HS 2001100). .... Corben-Fettcs. Globe Special (Globe GC- I B). 30 ...
3MB taille 33 téléchargements 191 vues
CERTIFICATED

AIRCRAFT ENGINES

MAY 2001

SSP-401

Lycoming 652 Oliver Street Williamsport, PA 17701 U S A. 57013234181

-

TABLE OF CONTENTS PISTON CERTIFICATED ENGINES (4)FourCylinderSeries............................................................................. (6)SixCylinderSeries..............................................................................l4 (8)EightCylinderSeries.............................................................................28

1

PISTON ENGINE INSTALLATIONS (4) Four Cylinder Installations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 (6) Six Cylinder Installations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 TURBOCHARGED............................................................................41 GEARED...................................................................................42 HELICOPTER...............................................................................44 MTEGRALACCESSORYDRIVE.............................................................. 45 INTEGRAL ACCESSORY - GEARED . . . . _. . . . . . . . . . . . . . . _. . . . . . . . . . . . . _ . . . . . . . . . . . . . . . . . . . . . . . .45 (8) Eight Cylinder Installations . . . . . . . . . . . . ,_. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .46 CODES

* Indicate new additions.

MODEL DESIGNATION BREAKDOWN: Example: AEIO-540-LlB5D 08 6) 0 Prefixes:

0 Suffkes:

A AE G H I L M 0 s T v

L

-

1 B 5 D

-

-

Acrobatic (DRY SUMP) Acrobatic Engine Geared Horizontal Helicopter Fuel Injected Left Hand Rotation Crankshaft Drone Opposed Cylinders Supercharged Turbocharged Vertical Helicopter

* Counterweight .,

.

2.

On 0 & IO-540 models - the #5 as the 4’ character indicates one fifth and one sixth order counterweights.

3.

On 4 cylinder models - the #6 as the 4’h suffix character one sixth and one eighth order indicates counterweights.

4.

On 6 cylinder models - the #6 as the 4’h suffix character indicates one sixth and five third order counterweights.

@ Cylinder Cubic Inch Displacement:

235, 290, 320, 340, 360 “” 435,480,540 720 541

:

,’

Applications:

1. On VO-540 models - the #3 as the 4’h suffix character indicates six third order counterweights.

The prefix of our example engine indicates an acrobatic engine with opposed cylinder that is fuel injected.

Cubic Inch Displacement

Indicates change in Power Section and Rating from Original Design Indicates Nose Section Indicates Accessory Section Indicates Counterweight Application Indicates Dual Magneto

No. of Cylinders :’.. ., , :!: .,.-‘.s .‘: ” 4 ’ ,. ’ 6 8 6 with integral iccessory

Engine Mounts: Conical - Straight mounts parallel to crankshaft. Dynafocal - Mounts- set at a specified angle to the crankshaft with Type 1 (30”) and Type 2 (18’) being different angles for four cylinder engines and Type 1 (3 1”) and Type 2 (20”) for six cylinder engines..

NOTE: Slick Magnetos are FAA approved for use on many engine models; reference latest edition of Service Instruction No. 1443

i

PISTON

- (4) FOUR CYLINDER

SERIES

Model

HP

T/Ot RPM

Fuel

C.R.

O-235-C I

II5

2800

80

6.75: I

Type 2 prop. flange, fixed or constant speed

-I5

115

2800

80

6.75: I

Same as -C I with Retard Breaker Magnetos

-15

0-235~CIC

II5

2800

80

6.75: I

Same as-Cl but with Slick Magnetos ’

-15

O-235-C2A

115

2800

80

6.75: I

Same as -Cl

-15

O-235-C2B

1 5

2800

80

6.75: I

Same as -C2A

0-235-C2C

I 5

2800

80

6.75: I

Similar to -C2A

O-235-El

I 5

2800

80

6.75: I

Same as -C I but has provision

I 5

2800

80

6.75: I

Same as C I B but has provision

for controllable

prop.

- 15

O-235-E2A

I15

2800

80

6.75: I

Same.as -C2A

but has provision

for controllable

prop.

- 5

O-235-E2B

I15

2800

80

6.75: I

Same as -C2B but has provision

for controllable

prop.

- 5

O-235-Fl

125

2800

100/1001.1.

9.70: I

Similar to -Cl

O-235-F I B

125

2800

IOO/IOOI.I.

9.70: I

Simiiar to C I B but higher power and camp. ratio

-15

O-235-F2A

125

2800

lOO/lOO1.1.

9.70: I

Similar to -C2A

but higher power and camp. ratio

-15

O-235-F2B

125

2800

IOO/IOOI.I.

9.70: I

Similar to -C2B but higher power and camp. ratio

-15

O-23541

125

2800

lOO/1~JOl~l.

9.70: I

Same as -F I but with provision

for controllable

prop.

-15

O-235~GIB

125

2800

IOO/IOOI~I.

9.70: I

Same as -F 1B but has provision

for controllable

prop.

-15

O-23542A

125

2800

IOO/IOOI.I.

9.70: I

Same as -F2A

but has provision

for controllable

prop.

- I5

O-235-G2B

125

2800

IOO/IOOI.I.

9.70: I

Same as -F2B but has provision

for controllable

prop.

- I5

O-235-H2C

I I5

2800

80

6.75: I

Same as C2C

but with Type 1 dynafocal mounts

-15

O-235-J2A

125

2800

IOO/IOOI.I.

9.70: I

Same as -F2A

but with Type 1 dynafocal mounts

-15

O-235-J2B

125

2800

IOO!Ifjf~l.l.

9.70: I

Same as -F2B but with Type 1 dynafocal mounts

-15

O-235-K2A

II8

2800

IOOIIOOI.I.

8.50: I

Same as -F2A but with 20” BTC timing, lower camp. ratio and lower power

-I 5

O-235-K2B

118

2800

IOO/IOOI.I.

8.50: I

Same as -F2B but with 20” B’I‘C timing, lower camp. ratio and lower power

-15

0-235-K2(‘

118

2800

10011001.1.

8.50: I

Same as -K2A

-15

.

O-2.35I2A

I I8

2800

100il00I.I.

8.50: I

Same as -J2A but with 20” BTC timing, lower camp. ratio and lower power

-15

.

o-235-l.2C

1 I8

2800

10011001.1.

8.5O:l

Same as -L2A

-15

O-235-M I

I18

2800

I~J~I/IOOI.I.

8.50: I

Similar to -L2A but has provision for controllable prop. and has AS-I 27, Type 2 prop. flange.

-15

0-235-MZ(.

I18

2800

IijO/lOOl.l.

8.50: I

Similar to -MI but has AS-127, Type I prop. Range and Slick Magnetos

-15

0

0-235-Cl .

O-235-El

0

B

B

ES/N Suffix

Description

+ 1 ake-( )ft. I

but has AS-127, Type I prop. flange with -I 200 series Magnetos

-15

but with Slick Magnetos

-15

for controllable

prop.

-15

- 5

but higher power and camp. ratio

but with Slick Magnetos

but with Slick Magnetos

PISTON

- (4) FOUR CYLINDER

Model

HP

T/Ot RPM

O-235-M3C

II8

2800

100/1001.1. 8.50: I

O-235-N2A

II6

2800

IOO/IOOLL

O-235-N2C

II6

2800

O-235-P I

II6

O-235-P2A

Fuel

SERIES

C.R.

ES/N Suffix

Description Similar to -Ml but has Slick Magnetos and uses 7/l 6 in. prop. bolts instead of 3/8 in. bolts

-15

8.lO:l

Same as -L2A

but lower camp. ratio and power

-15

IOO/IOOI.L

8.lO:l

Same as -L2C

but lower camp. ratio and power

-15

2800

IOO/IOOL.L

8.lO:l

Same as -Ml

II6

2800

IOO/IOOI.L.

8.lO:l

Similar to -Pl but has AS-127, Type I prop. flange

-15

o-235-P2C

II6

2800

IOO/IOOI.I.

8.lO:l

Same as -M2C

but lower camp. ratio and power

-15

o-235-P3C

I I6

2800

IOO/IOOI.I.

8.lO:l

Same as -M3C

but lower camp. ratio and power

-15

0-290-D

130

2800

80

6.50: I

Solid tappets. hydro control

-21

127

2800

80

6.50: I

Same as 0-290-D

-21

O-290-D2

140

2800

80

7.50: I

Hydraulic

O-290-D2A

140

2800

80

7.50: I

Same as -D2 but new crankcase for controllable

O-290-D2B

140

2800

80

7.00: I

Same as -D2,25”

O-290-D2C

140

2800

80

7.00: I

Same as -D2B

with Retard Breaker Magnetos

-2 I

0-320-A

IA

IS0

2700

80

7.00: I

Controllable prop, 25” spark advance, Bendix S4LN-20 and S4LN-2 I Magnetos

-27

0-320-A

IB

I50

2700

80

7.00: I

Same as -A I A with straight riser in oil sump and -32 carburetor

-27

O-330-A2A

I50

2700

80

7.00: I

Same as -A I A but fixed pitch propeller

-27

0-3-‘0-ATB *

I50

2700

80

7.00: I

Same as -A2A -32 carburetor

with straight riser in oil sump and

-27

O-3-‘0-A’C

I50

2700

80

7.00: I

Same as -A2B

with Retard Breaker Magnetos

-27

0-320-A2D

I50

3700

80

7.00: I

Same as -E3D but with conical mounts and 0-320-A sump and intake pipes

-27

o-320-/43/l

IS0

2700

80

7.00: I

Same as -A I A but uses 7116 in. dia. prop. bolts

-27

0-320-A3B

IS0

2700

80

7.00: I

Same as -A3A -32 carburetor

except for straight riser in oil sump and

-27

0-320-A3C

I50

2700

80

7.00: I

Same as -A3B

except for Retard Breaker Magnetos

-77

O-320-B I A

160

2700

10011001 I.

8.50: I

Same as -A I A but high camp. ratio

-39

0-320-B I B

160

2700

10011001.1. 8.50: I

Same as -B I A except for straight riser in oil sump and -32 carburetor

-39

Same as -B I A fixed pitch propeller

-39

Same as -BZA -32 carburetor

-39

.

0-290-I

I

O-320-B2A

I60

2700

100!1001.1.

8.50:

O-320-B2B

160

2700

101)!1001.1.

8.50: I

t Take-Off:

I

-15

but lower camp. ratio and power

.

-21

tappets, 18” spark advance prop.

spark advance and lower CR.

except for straight riser in oil sump and

-2 I -21

0

.

.

0

PISTON - (4) FOUR CYLINDER

.

ENGINES ES/N SUfflX

Model

HP

T/O? RPM

O-320-82(3

160

2700

IOO/IOOLL

8.50: 1

Same as -B2B except for Retard Breaker Magnetos

-39

O-320-B2D

160

2700

IOO/IOOLL

8.50: 1

Same as -D 1D except for fixed propeller and conical mounts

-39

O-320-B3A

160

2700

IOO/IOOLL

8.50: 1

Same as -BIA except for 7/16 in. prop. attaching bolts

-39

O-320-B3B

160

2700

IOO/IOOLL

8.50: 1

Same as -B 1A except for 7/l 6 in. attaching bolts and straight riser in oil sump and -32 carburetor

-39

O-320-B3C

160

2700

IOOAOOLL

8.50: I

Same as -B3B except for Retard Breaker Magnetos

-39

0-320-C I A

150

2700

80

7.00: 1

Low compression field service conversion of-B 1A

-39

0-320-C 1B

150

2700

80

7.00: 1

Low compression field service conversion of-B 1B

-39

O-320C2A

150

2700

80

7.00: I

Low compression field service conversion of -B2A

-39

O-320-C2B

150

2700

80

7.00: 1

Low compression field service conversion of -B2B

-39

0-320~C2C

150

2700

80

7.00: 1

Low compression field service conversion of -B2C

-39

O-320~C3A

150

2700

80

7.00: 1

Low compression field service conversion of -B3A

-39

O-320-C3B

150

2700

80

7.00: 1

Low compression field service conversion of -B3B

-39

0-320~C3C

150

2700

80

7.00: 1

Low compression field service conversion of -B3C

-39

0-320-D 1A

160

2700

IOO/IOOLL

8.50: 1

Same as -B3B but with Type 1 dynafocal mounts

-39

0-320-D 1B

160

2700

IOOAOOLL

8.50: 1

Same as -D 1A except for Retard Breaker Magnetos

-39

0-320-D] C

160

2700

IOO/IOOLL

8.50: 1

Same as -D2C but has provision for controllable prop.

-39

O-320-DID

160

2700

IOO/IOOLL

8.50: 1

Similar to -D 1A but has horizontal carburetor and induction housing and has Slick Magnetos

-39

O-320-Dl F

160

2700

IOO/IOOLL

8.50: 1

Same as -El F except has high compression pistons

-39

O-320-D2A

160

2700

IOO/IOOLL

8.50: 1

Same as -Dl A but with fixed pitch prop. and 3/8 in. attaching bolts

-39

O-320-D2B

160

2700

IOO/IOOLL

8.50: 1

Same as -D2A except for Retard Breaker Magnetos

.-39

O-320-D2C

160

2700

IOO/IOOLL

8.50: 1

Same as -D2A except for -1200 series Magnetos

-39

O-320-D2F

160

2700

IOO/IOOLL

8.50: 1

Same as -E2F except has high compression pistons

-39

O-320-D2G

160

2700

IOO/IOOLL

8.50: 1

Same as -D2A but with Slick Magnetos, 7/16 in. instead of 318 in. prop. flange bolts

-39

O-320-D2H

160

2700

IOO/IOOLL

8.50: 1

Same as -D2G but with 0-320-B sump and intake pipes and has provision for AC type fuel pump

-39

O-320-D2J

160

2700

IOO/IOOLL

8.50: 1

Similar to -D2G but has (2) Slick impulse coupling Magnetos and an unmachined governor pad on front of crankcase

-39

Fuel

Description

C.R.

.

i- Take-Off. 3

PISTON - (4) FOUR CYLINDER

Model

HP

T/Ot RPM

O-320-D3G

160

2700

0-320-E 1A

150

2700

80

0-320-E 1B

150

2700

0-320-E 1C

150

O-320-El F

Fuel

C.R.

ENGINES

Description

IOO/IOOLL 8.50: 1

ES/N Suffix

Same as -D2G but with 3/S in. prop. attaching bolts bolts and has provisions for fuel pump

-39

7.00: 1

Same as -A3B but with Type 1 dynafocal mounts

-27

80

7.00: 1

Same as -E 1A except for Retard Breaker Magnetos

-27

2700

80

7.00: 1

Same as -E 1A but has -1200 series Magnetos

-27

150

2700

80

7.00: 1

Same as -E 1C but with prop. governor drive on left front of crankcase

-27

0-320-E 1J

150

2700

80

7.00: 1

Same as -E 1F but has Slick Magnetos

-27

O-320-E2A

1501 140

27001 2450

80

7.00: 1

Same as -E I A but with fixed pitch prop. and uses 318 in. attaching bolts and has alternate rating of 140 HP at 2450 RPM

-27

O-320-E2B

150

2700

80

7.00: 1

Same as -E2A except for Retard Breaker Magnetos

-27

O-320-E2C

1501 140

27001 2450

,80

7.00: 1

Same as -E2A but has -1200 series Magnetos

-27

O-320-E2D

150

2700

80

7.00: 1

Similar to -E2A but with Slick Magnetos, O-235 front main bearing and 7/l 6 in. prop. flange bushings

-27

O-320-E2F

150

2700

80

7.00: 1

Same as -E 1F but with fixed pitch propeller

-27

O-320-E2G

150

2700

80

7.00: 1

Same as -E2D but has 0-320-A sump and intake pipes -27

O-320-E2H

150

2700

80

7.00: 1

Same as -E2D but equipped with S4LN-20 and -2 1 Magnetos

-27

O-320-E3D

150

2700

80

7.00: 1

Same as -E2D but uses 3/8 in. instead of 7116 in. prop. flange bushings

-27

O-320-E3H

150

2700

80

7.00: 1

Same as -E3D but equipped with S4LN-20 and -2 I Magnetos

-27

0-320-H 1AD

160

2700

IOOAOOLL 9.00: 1

Integral accessory section crankcase, front mounted fuel pump, external mounted oil pump and D4RN3000 impulse coupling dual Magneto

-76

0-320-H 1BD

160

2700

IOO/~OOLL 9.00: I

Same as -H 1AD but with D4RN-3200 Retard Breaker dual Magneto

-76

O-320-H2AD

160

2700

I OO/IOOLL 9.00: 1

Same as -H 1AD but with fixed pitch propeller

-76

O-320-H2BD

160

2700

IOO/IOOLL 9.00: 1

Same as -HZAD but with D4RN-3200 Retard Breaker dual Magneto

-76

Same as -H2AD but uses 3/8 in. instead of 7116 in. prop. flange bushings

-76

Same as -H3AD but with D4RN-3200 Retard Breaker

-76

O-320-H3AD

160

2700

~OO/~OOLL9.00: 1

O-320-H3BD

160

2700

IOO/IOOLL 9.00: 1

.

dual Magneto 10-320-A 1A

150

2700

80

7.00: I

Same as O-320-El

B but with rear Rendix fuel

injection and Type 2 dynafocal mount\ t Take-Off. 4

-55

0

PISTON

.

- (4) FOUR CYLINDER

Model

HP

T/O-I RPM

Fuel

C.R.

IO-320-A2A

150

2700

80

7.00: I

10-320-B I A

160

2700

10-320-B I B

160

10-320-B I C

SERIES ES/h’ Suffix

Description Same as -A I A but with fixed pitch prop. and 3/8 in. prop. flange bushings

-55

IOO/IOOI.I. 8.50: I

Same as 0-320-D I A but with Type 2 dynafocal mounts and rear mounted Bendix fuel injector

-55

2700

10011001.1. 8.50: I

Same as -B I A but has AN fuel pump drive

-55

160

2700

IOO/IOOI.I.

8.50: I

Same as -B I A but has adapter for mounting injector straight to the rear

10-320-B I D

160

2700

I OO/IOOI.I.

8.50: I

Same as -B IC but with -1200 series Retard Magnetos

-55

10-320-B I E

160

2700

IOO~IOOIA.

8.50: I

Same as -D I C but with rear mounted horizontal injector

fuel

-55

IO-320-B2A

160

2700

10011001.1.

8.50: I

Same as -B I A but with fixed pitch prop. and 318 in. prop. flange bushings

-55

10-320-C I A

160

2700

100/1001.1.

8.50: I

Same as -B I A except converted for use with turbocharger, long reach spark plugs, piston cooling oil jets, vented fuel nozzles, two S4LN-2 I impulse coupling Magnetos and AN fuel pump drive

-55

10-320-C I B

160

2700

100/1001.1.

8.50: I

Same as -CIA but with fuel injector mounted straight to the rear and 24 volt system standard

-55

10-320-D I A

160

2700

10011001.1.

8.50: I

Same as O-320-D2C except has Bendix RSA-SAD1 fuel injector, provision for controllable pitch prop. and 716 in. prop. flange bushings

-55

10-320-D I B

160

2700

10011001.1.

8.50: I

Same as -D I A but with prop. governor drive on left front of crankcase

-55

10-320-D I C

160

2700

10011001.1.

8.50: I

Same as-D I B but with Slick Magnetos, 24 volt system and 100 amp alternator standard

-55

10-320-E I A

I50

2700

80

7.00: I

Same as 0-320-A3B

-55

10-320-E I B

IS0

2700

80

7.00: I

Same as -E I A but with Slick Magnetos

-55

IO-3?0-E2A

I50

2700

80

7.00: I

Same as -E I A but with fixed pitch prop. and 3/8 in. prop. flange bushings

-55

IO-320-E2B

I50

2700

80

7.00: I

Same as O-320-A2D fuel injector

but with Bendix RSA-SAD1

-55

10-320-F I A

I 60

2700

l00/l00l.l

8.SO: I

Same as-C I A but with Type I dynafocal mounts

-55

-55

fuel

except has Bendix fuel injector

LIO-320-B

IA

60

2700

10011~101.1.

8.50: I

Similar to 10-320-B IA but has left hand rotation crankshaft

-66

LIO-320-C

IA

I 60

2700

100~1001.1

8.SO: I

Similar to IO-320-Cl crankshaft

-66

AIO-320-A

IA

160

2700

100/1001.1.

8.SO: I

Acrobatic engine with performance IO-320-DI A

i Take-Off 5

A but has left hand rotation

similar to

-65

PISTON

- (4) FOUR CYLINDER

ENGINES

HP

T/Ot RPM

Fuel

160

2700

IOO/IOOLL

8.50: 1

Same as -A I A but has impulse coupling

AIO-320-A2A

160

2700

IOO/IOOI.I.

8.50: I

Same as -A I A but with fixed pitch prop.

AIO-320-A2B

160

2700

I OO/I OOLL

8.50: I

Same as -A2A

Model AIO-320-A

IB

C.R.

ES/N Suffix

Description

but has impulse coupling

Magneto

-65 -65

Magneto

-65

AIO-320-B

IB

160

2700

IOO/IOOLL

8.50: I

Similar to -Al B but with front mounted fuel injector

-65

AIO-320-C

IB

160

2700

IOO/IOOI.I.

8.50: I

Similar to -BIB but the fuel injector is vertically mounted on the bottom of the sump

-65

160

2700

IOO/IOOI.I.

8.50: I

Same as IO-320-Dl kit

-55

It60

2700

IOO/IOOI.L.

8.50: I

Same as -DI B but with fixed pitch prop.

-55

AEIO-320-D

IB

AEIO-320-D2B

B but is equipped

with Acrobatic

AEIO-320-E

IA

I 50

2700

80

7.00: I

Same as.IO-320-El kit

with Acrobatic

-55

AEIO-320-El

B

I 50

2700

80

7.00: I

Same as 10-320-E I B but is equipped with Acrobatic kit

-55

AEIO-320-E2A

I50

2700

80

7.00: I

Same as IO-320-E2A kit

but is equipped

with Acrobatic

-55

AEIO-320-E2B

I50

2700

80

7.00: I

Same as IO-320-E2B kit

but is equipped with Acrobatic

-55

0-340-A 0-340-A

170 170

2700 2700

IWIOOI~I. I~~J/I~~I.I,

8.50: I 8.50: I

Controllable propeller Same as -A I A except for Retard Breaker Magnetos

-30 -30

O-340-A2A

170

2700

IOO/IOOI.I.

8.50: I

Same as -A I A but fixed pitch propeller

-30

0-340-B

160

2700

80

7.15: I

Low compression

-A I A

-30

160

2700

80

7.15:l

Low compression

-A2A

-30

IA IB

IA

O-340-B2A

A but is equipped

-36

0-360-A

A

180

2700

10011001.1.

8.50: I

Dynafocal

0-360-A

AD

180

2700

IOO/IOOI.I.

8.50: I

Same as -A I A but with D4LN-3000 dual Magnetos

impulse coupling

-36

mounts

0-360-A

IC

I 80

2700

IOO/IOOI.I.

8.50: I

Similar to -A I A but has horizontal induction housing, Bendix PSH-5BD pressure carburetor and Retard Breaker Magnetos

-36

0-360-A

ID

I 80

2700

100/1001.1.

8.50: I

Same as -A I A except for Retard Breaker Magnetos

-36

O-360-A I t-

I 80

2700

IOO/IOOI.I.

8.50: I

Same as .-A I A with - I200 series Magnetos

-36

O-360-A II6

I 80

2700

1()(Jil(J()I

8.50: I

Same as -A I I-’ but has (I ) sixth and ( I ) eighth order counterweights

-36

0-360-A

I x0

2700

Iwlc10l.l.

8.50: I

Same as -A I F6 but with D4LN-3000 coupling dual Magnetos

-36

I x0

7 700

100/1001 I

8.50:

Similar to -A I F but-has horizontal induction housing

I I-61)

( )-ihO-A I(;

1.

I

+ I AC-( jt.1 6

0

impulse

carburetor

and

-36

0

PISTON - (4) FOUR CYLINDER

0

0

0

SERIES

Model

HP

T/O? RPM

0-360-A lG6

180

2700

IOO/IOOLL

8.50: 1

Same as -A 1G but has (1) sixth and ( 1) eighth order counterweights

-36

O-360-AlG6D

180

2700

IOO/IOOLL

8.50: 1

Same as -A 1G6 but with D4LN-3000 impulse coupling dual Magneto

-36

0-360-A

H

180

2700

100/100LL

8.50: 1

Same as -A 1G but with prop. governor drive on left front of crankcase and -2 1, -204 Magnetos

-36

0-360-A

H6

180

2700

IOO/IOOLL

8.50: 1

Same as -A 1H but has (1) sixth and (1) eighth order counterweights

-36

0-360-A 1LD

180

2700

IOO/IOOLL

8.50: 1

Similar to -A 1A but with D4LN-3000 impulse coupling dual Magneto and has prop. governor drive on left front of crankcase

-36

0-360-A 1P

180

,270O ~OO/IOOLL 8.50: 1

Same as -C 1G except dynafocal mounts

-36

O-360-A2A

180

2700

IOO/IOOLL

Same as -Al A but fixed pitch propeller

-36

O-360-A2D

180

2700

IOOAOOLL 8.50: 1

Same as -A2A except for Retard Breaker Magnetos

-36

O-360-A2E

180

2700

IOO/IOOLL

Same as -A2D with provision for AN fuel pump drive

-36

O-360-A2F

180

2700

IOOAOOLL 8.5O:l

Same as -A2A with -1200 series Magnetos

-36

O-360-A2G

180

2700

IOO/IOOLL

Same as -Al G but fixed pitch propeller

-36

O-360-A2H

180

2700

100/1OOLL 8.50: 1

Same as -AIH

-36

O-360-A3A

180

2700

IOOAOOLL

8.50: 1

Same as -A2A but has 6 special long bushings in prop. flange

-36

O-360-A3AD

180

2700

IOO/IOOLL

8.50: 1

Same as -A3A but with D4LN-3000 impulse coupling dual Magneto

-36

O-360-A3D

180

2700

IOO/IOOLL

8.50: 1

Same as -A3A except for Retard Breaker Magnetos

-36

O-360-A4A

180

2700

lOO/lOOLL

8.50: 1

Same as -A3A but has solid crankshaft

-36

O-360-A4AD

180

2700

IOO/IOOLL

8.50: 1

Same as -A4A but with D4LN-3000 impulse coupling dual Magneto

-36

O-360-A4D

180

2700

IOO/IOOLL

8.5O:l

Similar to -A4A except for Retard Breaker Magnetos, (2) Magneto drive isolators and -A2A propeller flange bushings

-36

O-360-A4G

180

2700

IOO/IOOLL

8.50: 1

Same as -A2G but has -A4A crankshaft with -AZG propeller flange bushings

-36

O-360-A45

180

2700

IOO/IOOLI.

8.50: 1

Same as -A4G but has -2 I and -204 Magnetos

-36

O-360-A4K

180

2700

IOO/IOOLL

8.50: 1

Same as -A4J but with Slick Magnetos

-36

O-360-A4M

180

2700

I OO/IOOLL

8.50: 1

Same as -A4A but with Slick Magnetos

-36

O-360-A4N

180

2700

I ooil OOLL

8.50: 1

Same as -A4M but has an unmachined governor pad on front of crankcase and -A2G propeller flange bushings

-36

Fuel

C.R.

Description

8.50: 1

8.50: 1

8.50: 1

t Take-Off. 7

but fixed pitch propeller

ES/N Suffix

PISTON - (4) FOUR CYLINDER

SERIES

ESM SUfflX

Model

HP

T/O? RPM

O-360-A4P

180

2700 IOO/IOOLL 8.50:1

Sameas-A4M except for propeller flange bushings

-36

O-360-A5AD

180

2700 IOOAOOLL 8.5O:l

Sameas -A4AD but hasstandardlength propeller flange bushings

-36

0-360-B 1A

168

2700

80

7.20:1

Sameas -Al A but low compressionratio

-36

0-360-B I B

168

2700

80

7.20:1

Sameas -B 1A except for Retard Breaker Magnetos

-36

O-360-B2A

168,

2700

80

7.20:1

Sameas -B 1A except for fixed pitch propeller

-36,

O-360-B2B

168

2700

80

7.20:1

Sameas -B2A except for Retard Breaker Magnetos

-36

O-360-B2C

168

2700

80

7.20:1

Sameas -B2A except has 10-360-A crank and rods

-36

0-360-C I A

180

2700 IOO/IOOLL 8.50:1

Sameas -Al A but conical rubber mounts

-36

0-360~ClC

180

2700 IOO/IO~LL

Sameas -C I A except for Retard Breaker Magnetos

-36

0-360-C I E

180

2700 IOO/IOOLL 8.50:1

Sameas -C 1A but with Slick Magnetos

-36

0-360-C 1F

180

2700 IOO/IOOLL 8.50:1

Sameas -A 1G with conical mounts and Slick Magnetos

-36

0-360-C 1G

180

2700 IOO~IOOLL 8.50:1

Sameas -C 1A but with propeller governor drive on letI front of crankcase

-36

O-360-C2A

180

2700 IOO/I'OOLL 8.50:1

Sameas -C 1A but fixed pitch propeller

-36

O-360C2B

180

2700 IOO/IOOLL 8.5O:l

Sameas -C 1A but fixed pitch propeller and horizontal pressurecarburetor and has helicopter rating

-36

0-36OC2C

180

2700 IOO/IOOLL 8.50:1

Sameas -C2A except for Retard Breaker Magnetos

-36

O-360-C2D

180

2700 IOO/IOOLL 8.50:1

Sameas -C2B except for Retard Breaker Magnetos

-36

O-360C2E

180

2700 IOO/IOOLL 8.50:1

Sameas -C2A but with.Slick Magnetos

-36

O-360C4F

180

2700 IOOAOOLL 8.50:1

Sameas -C 1F except has solid crankshaft and no provision for propeller governor

-36

0-360-C4P

180

2700 IOOAOOLL 8.50:1

Sameas-A4M except for propeller fiange bushings and conical mounts

-36

0-360-D 1A

168

2700

80

7.20:1

Sameas -B 1A but conical rubber mounts and -1200 series Magnetos

-36

O-360-D2A

168

2700

80

7.20:I

Sameas -B2A but conical rubber mounts

-36

O-360-D2B

168

2700

80

7.20:1

Sameas -D2A except for Retard Breaker Magnetos

-36

0-360-E 1A6D

180

2700 .IOO/IOOLL 9.00: 1

Integral accessorysection crankcase,front mounted fuel pump, external oil pump, DPRN-3000 impulse coupling dual Magneto and counterweighted crankshaft

-i7

0-360-F 1A6

180

2700 100/100LL

Similar to 0-360-A serieswith new sump for nose wheel clearance,rear HA-6 carburetor, has (1) sixth and (1) eighth order counterweightsand has prop. governor drive on.left front of crankcase

-36

Fuel

C.R.

8.5O:l

8.50:1

Description

t Take-Off. 8

0

0

PISTON

Model 0-360-G

1A6

O-360-J2A

I

0

- (4) FOUR CYLINDER

HP

T/Ot RPM

180

2700

IOO/IOOLI.

145

2700/ 2400

IOO/IOOI.I. 8.50: I

Fuel

ES/N Suffix

Description

CR. 8.50: I

SERIES

Same as -Fl A6 but with a machined pad on right front of crankcase

-36

Similar to 0-360-CIC except has O-320-B2C prop. flange bushings, lightweight cylinders and lower power setting

-36

-36

HO-360-A

IA

180

2700

IOO/IOOI.I,

8.50: I

Same as O-360-A2D but with MA-4-5AA and Type 2 dynafocal mounts

HO-360-B

IA

180

2900

IOO/IOOI~I.

8.50: I

Same as O-360-C2D

HO-360-B

IB

180

2900

IO&OOI.I.

8.50: I

Same as -B I A but with two (2) S4LN-200

HO-360-C I A

180

2700

100/1001.1,

8.50: I

Similar to O-360-C2D except uses HA-6 carburetor in place of the PSH-5HD carburetor

-36

10-360-A 1A

200

2700

IOO/IOOI.I.

8.70: I

Bendix fuel injection, tuned induction

-5 I

10-360-A I B

200

2700

lOO/lOOl.l.

8.70: I

Same as -A I A but has -1200 series impulse coupling Magnetos

-5 I

10-360-A I B6

200

2700

IOO/IOOI.I.

8.70: I

Same as -A I B but has (I ) sixth and (I ) eighth order counterweights

-5 I

10-360-A

200

2700

I OO/IOOI,I-

8.70: I

Same as -A I B6 but has (I) Bendix D4LN-3000 impulse coupling dual Magneto

-5 I

10-360-A

200

2700

lOO/lOOl.l.

8.70: I

Same as -A I A but with -I 200 series Magnetos

-5 I

10-360-A

200

2700

if~(J/lOfJl.l.

8.70: I

Same as -A I B but has S4LN-2 I impulse coupling and S4LN-204 Magnetos

-5 I

10-360-A I D6

200

2700

IOO/IOOI.I.

8.70: I

Same as -Al B6 but with propeller governor drive on left front of crankcase

-5 I

10-360-A I D6D

200

2700

lf~O/lOOl.l.

8.70: I

Same as -A I D6 but has (I) Bendix D4LN-3000 impulse coupling dual Magneto

-5 I

IO-360-A2A

200

2700

Il~OilOOl.l.

8.70: I

Same as -A I A but fixed pitch propeller

-5 I

IO-360-A2B

200

2700

IOO/IO(II.I.

8.70: I

Same as -A2A

-5 I

IO-360-A2C

200

2700

IOO/IOOI.I.

8.70: I

Same as -A I C but has fixed pitch propeller

-5 I

IO-360-A3H6

200

2700

I O~!/lOOl.l.

8.70: I

Same as -A I B6 with propeller 120” clockwise

-5 I

IO-360-.43H61>

‘00

2700

Iof~/looI.I.

8.70: I

Same as -Al B6D with propeller rotated 120” clockwise

IO-36CJ-A3D6D

100

2700

10011001.1.

8.70: I

Same as -A I D6D but with propeller rotated 120” clockwise

I x0

2700

100/1001 I.

8.5fJ: i

Same as O-360-A I D except for Simmonds 530 Fuel Injection System

-5 I

I Xi)

2700

lOO/lO~Jl I.

8.50: I

Same as -B I A except for Bendix Fuel Injection System

-5 I

.

IO-360-B 113 + I a!,1.

7.30: I

-B I A6 with flange propeller PSD-78D carburetor

-33

GSO-480-B2G6

340

3400

100/1001,1,

7.30: I

Same as -B2C6

with Retard Breaker Magnetos

-33

GSO-480-B2H6

340

3400

100/1001.1.

7.30: I

Same as -B2D6

with Retard Breaker Magnetos

-33

0-480-l**.

340

3400

100/1001.1.

7.30: I

Like Beech version of-B I B6 (Horizontal carburetor under engine) with -22 and --23 Magnetos

-33A

-44

-IA

elbow and carburetor

-33

shaft and downdraft

IGSO-480-A

I A6

340

3400

lOO/lOOl.l.

7.30: I

Simmonds Fuel Injection version of-B

IGSO-480-A

I B6

340

3400

100/1001.1.

7.30: I

Same as -A I A6 except for Retard Breaker Magnetos

-44

IGSO-480-A

I C6

340

3400

10011001.1.

7.30: I

Same as -A I A6 except for horizontal and throttle body

-44

IGSO-480-A

I D6

340

3400

lOO/lOOl.l.

7.30: 1

Conversion

IGSO-480-A

I E6

340

3400

10011001.1.

7.30: I

Same as -A I D6 except for air inlet housing mounts, injector 35” forward of vertical and has Retard Breaker Magnetos

-44

IGSO-480-A

I F3

340

3400

10011001.1.

7.30: I

Same as -A I F6 except Torsional been modified

-44

IGSO-480-A

F6

340

3400

I00/I00I.I.

7.30: I

Same as -A I C6 except for Retard Breaker Magnetos

-44

IGSO-480-A

G6

340

3400

I (JO/I 001.1.

7.30: I

Similar to -A I E6 but has -1200 series Magnetos and has fuel flow modulator removed

-44

330

3400

10011001.1.

7.30: I

IGSO-480-A

-44

250 735

2s75!’ 2400

I00/l001.1.

8.50: I

Two sixth order counterweights

0-480-i 0-540-A

IA

** Suffix “A” afier the model dash number indicates engine was supplied priming system. 17

of-B

I B6

air inlet housing

I A6 to Bendix fuel injection

Damper System has

I A6 but with -22 and -23 Magnetos

without

-44

magnetos, carburetor,

-40

ignition

harness and

PISTON

Model

HP

TlOt RPM

- (6) SIX CYLINDER

Fuel

C.R.

SERIES ES/N suf-lix

Description

0-540-A

I A5

2501 235

25151 2400

100/1001.1.

8.50: I

Same as -A I A but one fifth and one sixth order counterweights

-40

0-540-A

I B5

2501 235

25151 2400

10011001.1,

8.50: I

Same as -A I A5 except for short propeller studs and two impulse Magnetos

-40

0-540-A

c5

2501 235

25751 2400

loo/l 001.1~

8.50: I

Same as -A I A5 except for two impulse Magnetos

0-540-A

D

2501 235

25151 2400

IOO/IOOI.I.

8.50: I

Same as -A I B5 except for two sixth order counterweights with Retard Breaker Magnetos

-40

0-540-A

D5

2501 235

2515f 2400

10011001,1~

8.50: I

Same as -A I B5 except for Retard Breaker Magnetos

-40

O-540-A2B

2501 235

25751 2400

IOO/IOOI.I.

8.50: I

-A I A with short propeller governor studs and propeller locating bushing, relocate 60’ counterclockwise

-40

0-540-A3D5

250

2575

100/1001.1.

8.50: I

Special Navy “Aztec”, same as -A 1D5 except for provision for propeller de-icing and chrome barrels, 24 volt system standard

-40

O-540-A4A5

2501 235

2575/ 2400

IOO/IOOI.I.

8.50: I

Same as -A I A5 but with more effective weights for use with Hartzell “compact”

counterpropeller

-40

O-540-A4BS

2501 235

2575/ 2400

IOO/IOOI.I.

8.50: I

Same as -A I B5 but with more effective weights for use with Hartzell “compact”

counterpropeller

-40

O-540-A4C5

2501 235

25751 2400

10011001.1.

8.50: I

Same as -A IC5 but with more effective weights for use with Hartzell ‘compact”

counterpropeller

-40

O-540-A4D5

2501 235

25751 2400

100/1001.1.

8.50: I

Same as -A I D5 but with more effective weights for use with Hartzell “compact”

counterpropeller

-40

0-540-B 1A5

235

2575

80

7.20: I

Same as -A I D5 but low compression

0-540-B I B5

235

2575

80

7.20: I

Same as -B I A5 but with impulse coupling Magnetos and a field conversion of -A I A5, -A I B5 or -A lC5 to low compression

-40

0-540-B

235

2575

80

7.20: I

-B I A5 with - I200 series Magnetos

-40

O-540-B2A5

335

2575

80

7.20: I

Same as -B I A5 but does not have provision controllable propeller

O-540-B2B5

235

3575

80

7.20: I

Same as -B2A5

but with impulse coupling

0-540-B2C5

335

2575

80

7.30: I

Same as -B2B5

but with -1200 series Magnetos

O-540-B4A5

235

2575

80

7.20: I

Same as -B I B5 but with more effective weights for use with Hartzell “compact”

counterpropeller

-40

0-540-R4B5

235

2575

80

7.20: I

Same as -B I B5 but with more effective weights for use with Hartzell “compact”

counterpropeller

-40

0-540-D

250

2575

l00~l00l.l.

8.50: i

Same as -A I D5 but with Bed-type

260

2700

IOO~IOOLI

8.50: I

Same as -A4D5

I D5

I A5

O-540-E4A5

governor

a

-40 .

f ‘l’ake-Off. I8

-40

ratio

for

Magnetos

mounts

except for higher speed and rating

-40

-40 -40

-30 -40

PISTON-(6)SIXCYLINDERSERIES

0 . ,

0

. a

Model

HP

TlOt RPM

O-540-E4B5

260

2700

IOOAOOLL 8.50: 1

O-540-E4C5

260

2700

IOO/IOOLL

0-540-F I A5

260

2800

0-540-F] B5

260

0-540-G 1A5

Fuel

C.R.

Description

ES/N SUfflX

Same as -E4A5 but with impulse coupling Magnetos with integral feed-thru capacitors

-40

8.50: I

Same as -E4B5 but has -1200 series Magnetos

-40

lOOllOOLL

8.50: 1

Same as -A I A5 except for special studs for front end mounting

-40

2800

IOO/IOOLL

8.50: I

Same as -F 1A5 except for new style crankcase and Retard Breaker Magnetos

-40

260

2700

IOO/IOOLL

8.50: 1

Similar to -E4C5 except has stiffer crankshaft and -A 1D5 counterweights

-40

260

2700

IOO/IOOLL

8.50: 1

Same as -G 1A5 but does not have provision for controllable propeller

-40

0-540-H I A5

260

2700

IOO/IOOLL

8.50: I

Similar to -G I A5 but has piston cooling oil jets and -21 and -20 Magnetos

-40

0-540-H I A5D

260

2700

IOOAOOLL 8.50: I

Same as -HI A5 but equipped with D6LN-3000 impulse coupling dual Magneto system along with the dual Magneto accessory housing and related drive system

-40

0-540-H 1B5D

260

2700

IOO/IOOLL

8.50: I

Same as -H 1A5 but equipped with D6LN-3200 dual Magneto system, dual Magneto accessory housing, gear train and related parts

-40

O-540-H2A5

260

2700

IOO/IOOLL

8.50: I

Same as -HI A5 but with fixed pitch propeller

-40

O-540-H2A5D

260

2700

IOO/IOOLL

8.50: 1

Same as -H2A5 but equipped with D6LN-3000 impulse coupling dual Magneto system along with the dual Magneto accessory housing and related drive system

-40

O-540-H2B5D

260

2700

IOO/IOOLL

8.50: I

Same as -H2A5 but equipped with D6LN-3200 dual Magneto system, dual Magneto accessory housing, gear train and related drive system

-40

0-540-J lA.5D

235

2400

IOO/IOOLL

8.50: 1

Similar to -A4A5 except for rating, speed, D6LN3000 impulse coupling dual Magneto and various items of weight reduction

-40

0-540-J I B5D

235

2400

IOO/IOOLL 8.50: 1

Same as -J 1A5D but with D6LN-3200 Retard Breaker dual Magneto

-40

0-540-JlC5D

235

2400

IOO/IOOLL

8.50: I

Same as -J I A5D but with rear mounted HA-6 horizontal carburetor

-40

0-540-J 1D5D

235

2400

IOO/IOOLL

8.5O:l

Same as -JICSD but with D6LN-3200 Retard Breaker dual Magneto

-40

O-540-J2A5D

235

2400

IOO/IOOLL

8.50: I

Same as -J lA5D but with fixed pitch propeller

-40

O-540-J2B5D

235

2400

IOO/IOOLL

8.50: 1

Same as -J I B5D but with fixed pitch propeller

-40

O-540-J2C5D

235

2400

IOO/IOOLL

8.50: 1

Same as-J lC5D but with fixed pitch propeller

-40

t Take-Off. I9

PISTON - (6) SIX CYLINDER

SERIES

Model

HP

T/O? RPM

O-540-J2D5D

235

2400 IOOAOOLL 8.50:1

Sameas-J 1D5D but with fixed pitch propeller

-40

O-540-J3A5

235

2400 ~OO/~OOLL 8.50:1

Sameas -J3A5D but has Slick 625 1 (impulse coupling) and 6250 Magnetos

-40

O-540-J3A5D

235

2400 IOO/~OOLL 8.50:1

Sameas -J I A5D but has heavier counterweights for use with Hartzell extendedhub controllable propeller

-40

O-540-J3C5D

235

2400 IOO/IOOLL 8.50:1

Sameas -J 1C5D but has heavier counterweights for use with McCauley controllable propeller

-40

O-540-L3C5D

235

2400 IOOAOOLL 8.50:1

Similar to -J3C5D except for long reach spark plugs, high pressurefuel pump, piston cooling oil jets and turbocharger scavengepump

-40

10-540-A lA5

290

2575 IOO/IOOLL 8.70:1

High compressiontuned induction, Retard Breaker Magnetos, Bendix fuel injector

-48

10-540-B 1A

290

2575 IOOAOOLL 8.70:1

Sameas -A 1A5 except for updraft exhaust cooling

-48

10-540-B 1B5

290

2575 IOO/IOOLL 8.70:1

Sameas -B 1A5 except for Simmondsfuel injector

-48

10-540-B 1C5

290

2575 IOO/IOOLL 8.70:1

Sameas -B 1A5 except it hasexternal servo bleed in fuel injection system

-48

10-540-C1B5

250

2575 IOO/IOOLL 8.50:1

Sameas O-540-AlD5 but with Bendix fuel injector

-48

10-540-c 1c5

250

2575 IOOAOOLL 8.50:1

Sameas -ClB5 but has AN fuel pump

-48

IO-540-C2C

250

2575 IOO/IOOLL 8.50:1

Conversion of O-540-A2B to Bendix fuel injection and AN fuel pump drive

-48

IO-540~C4B5

250

2575 IOOAOOLL 8.50:1

Sameas -C 1B5 but with more effective counterweights for use with Hartzell “compact” propeller

-48

IO-540~c4c5

250

2575 ~OOAOOLL 8.50:1

Sameas -C4B5 but has AN fuel pump drive

-48

IO-540~C4D5

250

2575 IOOAOOLL 8.50:1

Sameas -C4D5D except hastwo Magnetos

-48

IO-540~C4D5D

250

2575 ~OO/~OOLL 8.50:1

Sameas -C4B5 but with D6LN-3000 impulse coupling -48 Magneto

IO-540-D4A5

260

2700 1OO/IOOLL 8.50:1

Sameas O-540-E4A5 but with Bendix fuel injection

-48

IO-540-D4B5

260

2700 IOO/IOOLL 8.50:1

Sameas -D4A5 but has-1200 series impulse coupling Magnetos

-48

IO-540-D4C5

260

2700 ~OO/IOOLL 8.50:1

Same as -D4B5

but with Retard Breaker Magnetos

-48

10-540-E1A5

290

2575 ~OO/IOOLL 8.70:1

Sameas -BlC5

but with piston cooling oil jets

-38

10-540-E] B5

290

2575 IOO/IOOLL 8.70:1

Same as -El A5 but with -1200 series Magnetos

-48

10-540-E1C5

290

2575 IOO/IOOLL 8.70:1

Same as -El B5 with RSA-IOEDl

fuel in.jector

-48

10-540-G 1A5

290

2575 IOO/IOOLL 8.70:1

Same as -Al A5 but with piston cooling oil jets

-4%

10-540-G1B5

290

2575 IOO/IOOI.I. 8.70:I

Similar to -G I A5 but has -1200 series Vagnetos RSA-1 OED I fuel injector

Fuel

C.R.

ES/N Suffix

Description

0

I

.

t Take-Off.

20

and

JX

.

0

PISTON

.

SERIES ES/N Suffix

HP

TlOt RPM

CS

290

2575

IOO/IOOI.I. 8.70: I

Same as -G I B5 but has impulse Magnetos and 38I /2” injector adapter

-48

IO-540-G

D5

290

2575

IOO/IOOLI. 8.70: I

Same as -G 165 but has straight injector inlet

-48

IO-540-G

E5

290

2575

IOO/IOOI.I. 8.70: I

Same as -G I A5 but has -1200 series Magnetos

-48

10-540-G I F5

290

2575

IOO/IOOLL

8.70: I

Same as -G I E5 but with (2) impulse coupling

IO-540-J4A5

250

2575

I 0011 OOLI.

8.50: I

Same as -C4B5 except conversion for use with turbocharger - long reach spark plugs, piston cooling oil jets, AN fuel pump drive, vertical fuel nozzles and - I2qO series Magnetos

-48

10-540-K I A5

300

2700

IOO/IOOI.I.

8.70: I

Similar to -G IA5 but has -1200 series Magnetos, RSA- I OEDI injector, large crankshaft and 38-l/2’ fuel injector adapter

-48

10-540-K I A5D

300

2700

IOO/IOOI.I.

8.7O:l

Same as -Kl A5 but with D6LN-3000 coupling dual Magneto

-48

10-540-K IB5

300

2700

IOO/IOOI.I,

8.70: I

Similar to -KIAS but has two impulse coupling Magnetos and straight injector adapter

-48

10-540-K I BSD

300

2700

IOO/IOOI.I.

8.70: I

Same as -K I B5 but with D6LN-3000 dual Magneto

-48

10-540-K I C5

3001 290

2700/ 2575

IOO/IOOI.I.

8.70: I

Similar to G I A5 but has -K I A5 rotating system

-48

10-540-K I D5

300

2700

100/1001.1.

8.70: I

Same as -K I A5 but has -200 series Magnetos, flange fuel injector and straight injector inlet

-48

10-540-K I ES

300

2700

10011001.1.

8.70: I

Similar to -KIC5

-48

10-540-K I E5D

300

2700

10011001.1.

8.70: I

Same as -Kl E5 but with D6LN-3000 dual Magneto

10-.540-K I F5

300: 290

27001 2575

10011001I

8.70: I

Same as -G I B5 but with -K series rotating system

-48

10-540-K I FSD

300

2700

100/1001.1.

8.70: I

Same as -K I F5 but with D6LN-3000 dual Magneto

-48

10-540-K IGS

300

2700

Iowl1lol.l.

8.70: I

Same as -K I A5 but has diaphragm type fuel pump and -48 drive

10-540-K IGSD

300

2 100

10011001.1.

8.70: I

Same as -K I A5D but has diaphragm type fuel pump and drive

-48

10-540-K I IJS

300

2700

10011001.1.

8.70: I

Same as --K I B5 but has diaphragm type fuel pump and drive

-48

10-540-K

300

2700

IOWIOOI I.

8.70: I

Same as -K I F5 but has diaphragm type fuel pump and drive

-48

300

2700

I0lvl00l.1

8.70: I

Same as -K I F5D but has diaphragm type fuel pump and drive

-48

Model

~ ’

- (6) SIX CYLINDER

Fuel

Description

C.R.

Mags.

impulse

impulse coupling

but has -1200 series impulse Mags. impulse coupling

Retard Breaker

-48

-48

I

. J5

10-540-K I J5D

t Take-Off. 21

PISTON

- (6) SIX CYLINDER

SERIES

Model

HP

T/Ot RPM

Fuel

10-540-K I KS

300

2700

IOO/IOOI.I.

8.70: 1

Similar to -K I A5 except modified Acrobatic kit

IO-540K2A5

300

2700

IOO/IOOLL

8.70: I

Same as -K I A5 except has different

10-540-L I A5

300

2700

IOO/IOOLI.

8.70: I

Similar to -K I A5 but with front air inlet and Retard Magnetos

-48

IO-540-Ll

A5D

300

2700

IOO/IOOLL

8.70: I

Same as -Ll A5 but with D6LN-3000 dual Magneto

-48

IO-540-Ll

BSD

300

2700

100/1001~1.

8.70: I

Similar to -Ll A5D except for a modified oil sump

-48

10-540-L I c5

300

2700

IOO/IOOI.I.

8.70: I

Same as -Ll A5 but has diaphragm drive

-48

10-540-M I A5

300

2700

I OO/IOO~I.

8.70: I

Similar JO -K I A5 but has Retard Breaker Magnetos and up exhaust heads

-48

10-540-M I A5D

300

2700

lOO/lOOl.l.

8.70: I

Same as -Ml A5 but with D6LN-3200 dual Magneto

-48

10-540-M I BSD

300

2700

IOO/IOOLL

8.70: I

Similar, to -M I A5D but with RSA-I OEDI fuel injector, automotive type fuel pump, D6LN-3000 impulse coupling Magneto and straight fuel injection adapter

-48

10-540-M I C5

300

2700

IOWIOOLI

Same as -MI A5 except has impulse Magneto

-48

IO-540-M2A5D

300

2700

I OO/lOOL.L.

8.70: I

Similar to -Ml A5 but has D6LN-3000 Retard Breaker dual Magneto and provision for fixed pitch propeller

-48

10-540-N I A5

260

2700

IOO/IOOI.I.

8.50: I

Similar to -D4A5 but with 0-540-G I A5 crankcase and -48 crankshaft and -K I A5 counterweight assembly

10-540-P I A5

290

8.70: I

Same as -G I B5 but has larger oil pump and is suitable for turbocharging

-48

10-540-R I A5

260

2700

I OO/IOOI.I.

8.50: I

Similar to -N I A5 except converted for use with turbocharger, long reach spark plugs, piston cooling oil jets, AN fuel pump, vented fuel nozzles ,and -I 200 series Magnetos

-48

3001

2700: 2575

1OOilOOl.l

8.70: I

Same as -PI A5 but with -K series rotating system

-48

290

260

2700

I00i1001.1.

8.50: I

Similar to -D4B5 but has D6LN-3000 coupling dual Magneto and horizontal injector

-48

10-540-S I A5

IO-‘Jo-l: + I ‘il\r-oi’l

I AI)

C.R.

8.70: I _-

260

2700

10011001.1.

8.70: 1

Same as -T4B5D

260

2700

I00/100I.I

8.50: I

Identical to -T4ASD

260

2700

10011001.1. 8.50: I

;trri

2700

10011001.1

8.70: I

ES/N Suffix

Description to use with an

propeller

bushings

impulse coupling

type fuel pump and

Retard Breaker

impulse rear inlet fuel

except for fuel drain boss location Retard

Same as --L I A5 but with up-exhaust cylinder heads and D6LN-3000 impulse coupling dual Magneto 17

-48

I

\

except has two Slick Magnetos

Same as -‘1‘4B5D but has Bendix D6LN-3200 Breaker Magneto

-48

-48 -48

.

-48

-48

0

PISTON-(6)SIXCYLINDERSERlES

0

Model

HP

T/O? RPM

10-540-U 1B5D

300

2700

IOO/IOOLL 8.70: 1

Same as -U 1A5D but has diaphragm type fuel pump and drive

-48

IO-540-V4A5

260

2700

IOO/IOOLL 8.50: 1

Same as -V4A5D except has two Slick Magnetos

-48

IO-540-V4A5D

260

2700

IOO/IOOLL 8.50: I

Same as -T4B5D except for front mounted fuel injector

-48

10-540-W 1A5

235

2700

IOOAOOLL 8.70: I

Same as -W lA5D except has two Slick Magnetos

-48

IO-540-W1A5D

235

2400

IOO/IOOLL 8.50: 1

Similar to O-540-JlA5D except is equipped with IO540-V4A5D sump, intake pipes and fuel injection system

-48

IO-540-W3A5D

235

2400

IOO/IOOLL 8.50: 1

Same as -WIASD but has heavier counterweights for use with Hartzell propeller

-48

IO-540-AA1 A5

250

2425

IOO/IOOLL 7.30: I

Similar to -S I A5 except for compression ratio

-48

IO-540-AA 1B5

270

2700

IOO/IOOLL 7.30: 1

Same as -AA 1A5 except has impulse Magneto and higher rating

-48

IO-540-AB IA5

230

2400

IOO/IOOLL 8.50: I

Similar to -WlA5 except has different counterweights, two Slick impulse Magnetos, bottom mounted injector and 230 H.P. rating

-48

IO-540-AC 1A5*

300

2700

IOO/IOOLL 8.70: 1

Top induction, down exhaust, impulse coupled Magneto and Precision Airmotive fuel in~jection

-48

VO-540-A 1A

305

3300

80

7.30: I

Low compression vertical PS-7BD carburetor

-43

VO-540-A2A

305

3300

80

7.30: 1

Same as -A 1A but with spring coupling accessory drive

-43

VO-540-B 1A

305

3200

80

7.30: I

Same as -A 1A except MAd-AA

-43

VO-540-B 1B

305

3200

80

7.30: I

Same as -B 1A except for Retard Breaker Magnetos and less fuel pump drive and hydraulic pump drive

-43

VO-540-B 1B3

305

3200

80

7.30: 1

Same as -B 1B except for six 3’d order counterweights

-43

VO-540-B 1C

305

3200

80

7.30: i

Same as -B 1A except for Retard Breaker Magnetos

-43

VO-540-B 1D

305

3200

80

7.30: 1

Same as -B 1C except for two MA-6-AA carburetors

-43

VO-540-B 1E

305

3200

80

7.30: I

Retrofit kit of-B 1A with two MA-6-AA carburetors

-43

VO-540-B 1F

305

3200

80

7.30: i

Same as -BlB

-43

VO-540-B 1H3

305

3200

80

7.30: 1

Same as -B 1B3 but with -I 200 series Magnetos

-43

VO-540-B2A

305

3200

80

7.30: I

Same as -B 1A but with spring coupling accessory drive

-4;

VO-540-B2C

305

3200

80

7.30: I

Same as -B 1C but with spring coupling accessor> drive

-43

VO-540-B2D

305

3200

80

7.30: I

Same as -B 1D but with spring coupling acceswr> Drive

-.I ;

Fuel

C.R.

ES/N Suffix

Description

t Take-Off. 23

carburetor

but has fuel and hydraulic pump drives

PISTON - (6) SIX CYLINDER

SERIES

Model

HP

T/O? RPM

Fuel

C.R.

VO-540-B2E

305

3200

80

7.30:I

Sameas-B 1E but with spring coupling accessory drive

-43

VO-540-B2G

305

3200

80

7.301

Sameas-B2D but with -1200 series Magnetos

-43

VO-540-C1A

315

3200 IOO/IOOLL 8.70:I

High compressionaltitude engine with two (2) MA6-AA carburetors,Retard Breaker Magnetos. Same as-B I D except for compressionratio and power

-43

vo-540-c I B

315

3200 IOO/IOOLL 8.70:1

Retrofit kit of-B 1E with high compressionpiston and -43 higher power

vo-540-c I c3

305

3200 IOO/IOOLL 8.70:I

Sameas-B 1B3 except it has high compressionpistons -43 and two MAd-AA carburetors

VO-540-C2A

315

3200 IOO/IOOLL 8.70:1

Sameas-C 1A but with spring coupling accessory drive

-43

VO-540-C2B

315

3200 IOO/IOOLL 8.70:1

Sameas-C I B but with spring coupling accessory drive

-43

VO-540-C2C

315

3200 IOO/IOOLL 8.70:I

Sameas -C2A except for -1200 series Magnetos

-43

o-540-9, -9A

305

3200 IOO/IOOLL 8.70:I

Military version of VO-540-C2A

-43

HIO-540-A I A

290

2575 IOOAOOLL 8.70:I

Similar to IO-540-KlA5 but has lower rating and speed,no provision for propeller governor and has front mounting padsmachined and studded

-48

IGO-540-A 1A

350

3400 100/100LL

8.70:I

High compressiontuned induction, Retard Breaker Magnetos,Bendix fuel injector

-49

IGO-540-A I B

350

3400 100/100LL

8.70:I

Same’as-Al A except for low tension ignition system -49

IGO-540-A 1C

350

3400 IOO/IOOLL 8.70:I

Similar to -A I A but equipped with RSA- 10DB1 fuel injector, RG-9080-J7fuel pump, S6RN-1208 and - 1209Magnetosand a Prestolite 24V-100A AN drive alternator

-49

IGO-540-B I A

350

3400 100/100LL

Sameas-A 1A except for updraft exhaust cooling

-49

IGO-540-B I B

350

3400 IOO/IOOLL 8.70:1

Sameas-B I A except for low tension ignition system

-49

IGO-540-B 1C

350

3400 100/100LL

Sameas-B I A except it has external servo bleed in fuel injection system

-49

IVO-540-A I A

305

3200 IOO/IOOLL 8.70:1

Similar to VO-540-C 1A but has Bendix RSA- 1OADI fuel injector

-60

TIO-540-A 1A

310

2575 IOO/IOOLL 7.30:I

Similar to 10-540-ElA5 but has turbocharger -61 (TE0659), RSA- IOAD I fuel injector and -1200 series Magnetos

TIO-540-A I B

310

2575 IOO/IOOLL 7.30:1

Sameas -A 1A but has density controller with faster temperatureresponse

-61

TIO-540-A I C

310

2575 IOO/IOOLL 7.30:1

Similar to -A I B but hasrevised controller setting

-61

8.70:I

8.70:1

Description

t Take-Off. 24

ES/N SUfflX

.

PISTON Model

a

HP

T/Ot RPM

- (6) SIX CYLINDER

Fuel

C.R.

TIO-540-C

1A

250

2575

IOO/IOOI.I> 7.20: 1

TIO-540-E

1A

260

2575

IOO/IOOI.I.

TIO-540-G

1A

250

2575

TIO-540-H

1A

270

TIO-540-K

1AD

TIO-540-S

1AD

SERIES ES/N Suffix

Description IO-540-J4A5 equipped with TE0659 turbocharger and low compression pistons

-61

7.20: I

Same as -C 1A but has higher rating and impulse coupling Magneto

-61

IOO/IOOI.L

8.50: 1

Same as ---C1A but high compression

-61

2575

IOO/IOOI.I.

7.20: 1

Same as -E 1A except for horsepower setting

-61

250

2575

IOO/IOOI.I,

8.00: I

Similar to -C 1A but with D6LN-3200 Retard Breaker dual Magneto, pressure controller, provision for cabin pressurization, rear mounted fuel injector, turbocharger mounted to rear of engine and higher compression ratio

-6 1

300

2700

IOO/IOOI.I.

7.30: I

Similar to IO-540-M2AD with front air inlet, provision for controllable propeller, a manually controlled TE0659 turbocharger and D6LN-3000 impulse coupling Magneto

-61

,

TIO-540-AA1

AD

270

2575

IOO/IOOU

8.00: I

Similar to -K 1AD but has a different controller system and has provision for a rear mounted propeller governor

-6 1

TIO-540-AB

1AD

250

2575

IOO/IOOIL

8.00: I

Same as --AA 1AD but has bottom mounted fuel injector, a relocated turbocharger and a D6LN-3000 impulse coupling Magneto

-61

TIO-540-AB

1BD

250

2575

I OO/IOOLI.

8.00: 1

Similar to -AB I AD except has propeller governor mounted on the accessory housing and the turbo scavenge pump moved to the vacuum pump pad and more effective counterweights for McCauley prop.

-61

350

2500

lOO/lOOl.l.

7.30: 1

Similar to -U2A but has (2) Garrett instead of RotoMaster turbocharger, (2) intercoolers, (1) wastegate and Slick Magnetos

-61

TiO-540-AE2A

TIO-540-AF

1A

270

2575

IOO/IOOI.I.

8.00: 1

Similar to -AA I AD but has Slick Magnetos, different turbocharger and an intercooler

-6 1

TIO-540-AF

1B

270

2575

~ooi~oo~.~.

8.00: I

Similar to -AFI A except incorporates exhaust guides

-61

TIO-540-AG

IA

270

2575

lOO/IOOI.I.

8.00: I

Similar to -AA 1AD except it has two Slick Magnetos and a relocated -AFl A turbocharger

-61

I-IO-540-Al1

I A*

300

2500

IOO/IOOI.I.

7.30: 1

Similar to TIO-540-A engines except down exhaust heads, two Slick pressurized Magnetos, sloped conttoller and relocated -AF 1A turbocharger

-61

310

2500

I ooiioo~.~.

7.30: I

Similar to -W2A except sloped controller relocated turbocharger

and a new

-61

235

2400

10011001.1.

8.00: 1

Similar to -AC 1A except has a relocated turbocharger bottom mounted fuel injector and a lower rating

-61

-l-IO-S40-A’A

3 IO

‘575

I 001IO01I.

7.30: I

Same as -A 1A but with propeller 3-blade propeller

flange bushings for

-61

1 IO-540-A’(3

7 IO

2575

I00/1001 I

7.3(J: i

Same as -A I B but with propeller 3-blade propeller

flange bushings for

-61

‘I‘IO-540-AK

+ I &e-off:

I A*

oil cooled

PISTON - (6) SIX CYLINDER

SERIES ES/N Suffix

Model

HP

TlOt RPM

TIO-540-A2C

310

2575

IOOIIOOI.I. 7.30: I

Same as -A I C but with propeller 3-blade propeller

flange bushings for

-61

TIO-540-F2BD

325

2575

IOO/IOOI,I. 7.30: I

Similar to -A2B but incorporates Breaker dual Magneto system

D6LN-3200

Retard

-61

TIO-540-J2B

350

2575

IOO/IOOI.L

7.30: I

Same as -J2BD but has S6LN- 1208 (Retard Breaker) and S6LN- 1209 Magnetos

-61

TIO-540-J2BD

350

2575

IOO/IOOLL

7.30: I

Similar to -F2BD turbocharger

-61

TIO-540-N2BD

350

2575

IOO/IOOLL

7.30: I

Identical to -J2BD except turbocharger half inch to the left

TIO-540-R2AD

3501 340

2575/ 2500

IOO/IOOLI.

7.30: I

Similar to -J2BD except has provision and has a variable pressure controller

TIO-540-T2AD

330

2400

I OO/IOOLL

7.30: I

Same as -J2BD except for a modified transition and lower rating

TIO-540-U2A

350

2500

IOO/IOOLL 7.30: I

TIO-540-V2AD

360

2600

IOO/IOOLL

TIO-540-W2A

360

2600

IOO/IOOLL 7.30: 1

Similar -VZAD but with Slick 6261 (impulse coupling) and 6260 pressurized Magnetos, a different controller system and without either induction air cooler or cabin bleed

-61

AEIO-540-D4A5

260

2700

100/1001.1. 8.50: I

Same as IO-540-D4A5 kit

but is equipped

with Acrobatic

-48

AEIO-540-D4B5

260

2700

100/1001.1.

5.50: I

Same as IO-540-D4B5 kit

but is equipped

with Acrobatic

-48

AEIO-540-D4C5

260

2700

100/1001.1.

8.50: 1

Same as IO-540-D4C5 kit

but is equipped

with Acrobatic

-48

AEIO-540-D4D5

260

2700

100/1001.1.

8.50: I

Same as -D4A5

AEIO-540-L

I B5

300

2700

10011001.1.

8.70: I

Same as -Ll B5D but has Slick 625 I (impulse coupling) and 6250 Magnetos

-48

AEIO-540-L

I B5D

300

2700

10011001.1.

8.70: I

Same as IO-540-Ll batic kit

-48

IGSO-540-A

IA

380

3400

100/1001.1.

7.30: I

Supercharged Bendix fuel injector, dry sump, crosswise accessories, high altitude Magnetos

IGSO-540-A

IC

380

3400

10011001.I.

7.30: I

Same as -A I A but with horizontal air inlet housing and -50 has external servo bleed in fuel injection system

IGSO-540-A

ID

380

3400

10011001.1.

7.30: I

Same as -A I A but has -1200 series Magnetos

-50

lGS0-540-A

IE

380

3400

10011001.1.

7.30: I

Same as -A I C but has - I200 series Magnetos and no venr tlow restriction

-50

IGSO-540-A

IF

380

3400

100/1001.1.

7.30: I

Same as -Al D but with fuel flow modulator

-50

Fuel

C.R.

7.30: I

Description

except equipped with TH08A60

shifted one-

for cabin bleed

exhaust

Similar to IO-540-AA I A5 but with intercooler customer supplied turbocharger system Similar to -J2BD except with an intercooler change in cylinder head design

except has “AN”

-61

-61

and

-61

and a

-61

fuel pump

B5D but is equipped

-61

-48

with Aero-

-50

.

t Take-Off. 26

removed

PISTON - (6) SIX CYLINDER

a

SERIES ES/N Suffix

Model

HP

T/O? RPM

Fuel

CR.

IGSO-540-Al H

380

3400

100/1OOLL

7.30: I

Same as -A 1E but with fuel flow modulator removed

-50

IGSO-540-BlA

380

3400

100/100LL

7.30: I

Same as -A I A except for updraft exhaust cooling and Simmonds fuel injector

-50

IGSO-540-B 1C

380

3400

100/100LL

7.30: I

Same as -B I A but has -1200 series Magnetos

-50

LTIO-540-K] AD

250

2575

IOO/IOOLL

8.00: 1

Similar to TIO-540-KIAD crankshaft

-68

LTIO-540-F2BD

325

2575

IOO/IOOLL

7.30: 1

Same as TIO-540-F2BD but has reverse rotation

-68

LTIO-540-J2B

350

2575

IOO/IOOLL

7.30: 1

Same as -J2BD but has S6RN-1208 (Retard Breaker) and S6RN- 1209 Magnetos

-68

LTIO-540-J2BD

350

2575

IOO/IOOLL

7.30:1

Same as TIO-540-J2BD but has reverse rotation

-68

LTIO-540-N2BD

350

2575

IOO/IOOLL

7.30: 1

Similar to TIO-540-N2BD crankshaft

but has left hand rotation

-68

LTIO-540-R2AD

3501 340

2575/ IOO/IOOLL 2500

7.30: I

Similar to TIO-540X2AD crankshaft

but has let? hand rotation

-68

LTIO-540-U2A

350

2500

IOO/IOOLL

7.30: I

Same as TIO-540-U2A but has reverse rotation

-68

LTIO-540-V2AD

360

2600

IOO/IOOLL

7.30: I

Same as TIO-540-V2AD

but has reverse rotation

-68

LTIO-540-W2A

360

2600

IOO/IOOLL

7.30:

Same as TIO-540-W2A but has left hand rotation crankshaft

-68

TIVO-540-A2A

315

3200

IOOAOOLL

7.30:

14,000,feet at 3200 RPM, turbocharger, Bendix fuel injection, vertical helicopter engine with spring coupling accessory drive

-57

TIO-54 I -A I A

310

2575

IOO/IOOLL

7.30: I

Turbocharger (T- 1823) i%el injected (RSA- 1OAD l), crosswise accessories, integral accessory section, wet sump

-59

TIO-541-E1A4

380

2900

IOO/IOOLL

7.30: I

Similar to -A I A but has compressor drive, larger redesigned cylinder head, RSA- IODB 1 injector and higher rating

-59

TIO-54 1-E 1B4

380

2900

I OO/IOOLL

7.30: I

Same as -E I A4 but has no provision for cabin pressurization

-59

TIO-54 I -E 1C4

380

2900

IOO/IOOLL

7.30: I

Same as -El A5 but has T I 879 turbocharger

-59

TIO-54 I -E I D4

380

2900

IOOAOOLL

7.30: I

Same as -E 184 but has T 1879 turbocharger

-59

TIGO-541-DIA

450

3200

IOOAOOLL

7.30: 1

Turbocharged (T 18A2 I ), fuel injected (RSA- 1ODB 1), off-set reduction gear, torquemeter, crosswise accessories, integral accessory section, wet sump

-62

TIGO-54 I -D I B

450

3200

IOO/IOOLL

7.30: I

Similar to --DIA but with integral wastegate turbocharger and low drag cylinder heads

-62

TIGO-541-EIA

425

3200

IOO/IOOLL

7.30: I

Same as -D I A except for rating

-62

TIGO-54 1-G 1AD

450

3200

IOO/IOOLL

7.30: 1

Similar to -D I A but has D6RN-3200 Retard Breaker dual Magneto and intercooler and fuel head enrichment fuel injector

-62

Description

i Take-Off. 27

but has left hand rotation

PISTON - (8) EIGHT CYLINDER

SERIES

Model

HP

T/O? RPM

10-720-A 1A

400

2650

IOO/IOOLL

8.70: 1

High compression tuned induction, Bendix fuel injector and AN fuel pump drive

-54

10-720-A 1B

400

2650

IOO/IOOLL

8.70: 1

Same as -Al A but equipped with S8LN-1208 and - 1209 Magnetos

-54

10-720-A 1BD

400

2650

IOO/IOOLL

8.70: 1

Same as -Al B but with D8LN-3200 Retard Breaker dual Magneto

-54

10-720-B 1A

400

2650

IOO/IOOLL

8.70: 1

Same as -A 1A but with updraft exhaust cooling and rear air inlet

-54

10-720-B 1B

400

2650

IOO/IOOLL

8.70: 1

Same as -BIA but equipped with S8LN-1208 and - 1209 Magnetos

-54

10-720-B 1BD

400

2650

~OOI/OOLL 8.70: 1

Same as -B 1B but with D8LN-3200 Retard Breaker dual Magneto

-54

10-720-C 1B

400

2650

IOO/IOOLL

8.70: 1

Same as -A 1B but has up-exhaust cylinder heads

-54

10-720-C 1BD

400

2650

IOOAOOLL

8.70: 1

Same as -C 1B but with D8LN-3200 Retard Breaker dual Magneto

-54

10-720-D 1B

4001 375

2650/ IOO/IOOLL 8.70: 1 2500

Similar to -A 1B but has rear air inlet

-54

IO-720-Dl BD

4001 375

26501 IOO/IOOLL 8.70: I 2500

Same as -Dl B but with D8LN-3200 Retard Breaker dual Magneto

-54

10-720-D 1C

4001 375

26501 IOO/IOOLL 8.70: 1 2500

Same as -D 1B but has 38- I /2” fuel injector adapter

-54

10-720-D 1CD

4001 375

26501 IOOAOOLL 8.70: I 2500

Same as -D 1C but with D8LN-3200 Retard Breaker dual Magneto

-54

Fuel

C.R.

Description

t Take-Off. 28

ES/N Suffix 0

.

PISTON O-235-C I

.

Bede Aircraft. MIS (I 18). Center Est Aeronautique (CEA). (GY-100-I 15). S.O.C.A.T.A. Rallye Club (I 15). Daetwyler. Trainer (MCD-100). Beagle Aircraft. Pup ( 15). Glosair. Victa Ah-tourer (I 15). Robin. (DR-400-2 + 2). Aero Boero. I 15.

O-235-C2C.

.

American

O-23S-H2C..

..

O-23S-J2B

,

Yankee Trainer (TR-2).

Robin. (DR 3001125 Petit Prince). Robin. (DR 3001125 Petit Prince).

O-235-K2C.

. Robin. (DR-400). Bellanca Aircraft.

O-23S-L2A

0-23S-L2C..

Aviation.

Citabria (7ECA).

Piper Aircraft. Tomahawk II (PA-38-I 12). Robin. (DR 400/120 Petit Prince). R-3 I IO. S.O.C.A.T.A. Ral1y.e I IOST. Orca. SAli- I. _.

_.

Grumman. AAIC. Cessna Aircraft. Cessna 153. I52 Aerobat. Piper Aircraft. Tomahawk (PA-38-I 12). Robin. (DR 4OOi2 + 2. HR 200’170. HS 2001100). Beech Aircraft. Skipper 77. Taylorcraft. Model l--2 I,

O-23S-M I

Gyroflug.

O-23S-N2A

Slingsby. .f67A. Aeromot. Paulistina P-56 Daetwyler. MD3-I 15. Shenyang. HU-I Seagull.

O-235-NtC

0-235-PI

Dauphin (DR-22 I), Petit Prince (DR-3 15) Sitar, Bagheera

Robin. (DR 3001108. DR 315 Cadet), Robin Club (R-2100). Grob. Cl 15. MFI. BA-I4 Starling. Aristek. AK-235 Paulistinha.

O-23%J2A

-

Super

Piper Aircraft. Super Cub (PA- 18 “I 05”). Colt (PA-22 “I 08”). Neiva. Paulistinha (L-6). Partenavia. Oscar (P-66).

.......

O-235-C2A

0

INSTALLATIONS

Piper Aircraft. Super Cruiser (J5C, PA-12) Cub (PA-l I), Family Cruiser (PA-14) Cub (PA-18 “105’) Clipper (PA-16) Pacer (PA-20 “I 15”) (PA-20s “I IS”). Intermountain Mfg. Co. Call Air (A). McKenzie Flying Service. McKenzie-Cessna (I 20 and 140). Champion Aircraft. Citabria (7ECA). Scheibe. Sperling (SF-23C). Scintex Aviation. Scintex (CP- I3 I5-C3).

l O-235-C I B

- (4) FOUR CYLINDER

.

Speed Canard Av,is (PA-FS-28)

Cessna Aircraft. ISliA I52 Aircorp. B2L Bushmaster. Enaer. Avton Ltviano. General Avia. Pinguino. Melbourne. Mamba Grob. G I 15. _,

Grob. GI I5 79

PISTON O-235P2A

.

0-290-D

. . .

.Gyroflug.

INSTALLATIONS

Speed Canard.

Military (L-2lA), Super Cub (PA-18 “125”), . . . . . Piper Aircraft. Pacer (PA-20 “125”, PA-20s “I 25’), Tri-Pacer (PA-22).

O-290-D2

Piper Aircraft. Super Cub (PA-l 8 “135”), Agriculture PA-20s “135”), Trainer Military (L2 I B), Tri-Pacer Intermountain Mfg. Co. Call Air (A4). Beagle. Alpha (-5). . . . . . . . . . . . . . Corben-Fettes.

O-290-D2A O-290-D2B.

Globe Special (W-I

Agriculture

(PA-I8A-125),

(PA- I8A “I 35”), Pacer (PA-20 “I 35”, (PA-22 “I 35”, PA-22s “I 35”).

A).

Champion Aircraft. Sky-Trac (7GC), DX-ER (7HC). Oberlerchner. Oberlerchner (JOB-l 5-35).

O-290-D2C.

. .

O-320-Al A

O-320-Al

- (4) FOUR CYLINDER

.

Champion

Aircraft.

Sky-Trac

(7GCO), DX-ER (7HC).

Piper Aircraft. Tri-Pacer (PA-22 “150”, PA-22s “IOO”), Apache (PA-23), Doyn Aircraft. Doyn-Cessna ( 170. l70A, 170B). Mooney Aircraft. Mark (20A). Dinfia. Ranquel (I A-46). Simmering-Graz Pauker. Flamingo (SGP-M-222). Aviamilano. Scricciolo (P- 19). Vos Helicopter Co. Spring Bok. B .

Pawnee (PA-25).

Piper Aircraft. Tri-pacer (PA-22 “ l50”, PA-22s “I 50”), Apache (PA-23). Doyn Aircraft. Doyn-Cessna (I 70, l70A, 1708). S.O.C.A.T.A. Horizon (Gardan).

O-320-A2A

Piper Aircraft. Tri-Pacer (PA-22 “I 50”, PA-22s “I 50”), Agriculture Cub (PA-l 8 “I 50”), Caribbean (PA-22 “I SO”), Pawnee (PA-25). Intermountain Mfg. Co. Call Air Texas (A-5, A-5T). Lake Aircraft. Colonial (C-l ). Rawdon Bros. Rawdon (T-I, T- 15, T- I5D). Shinn Engineering. Shinn (2 150-A). Dinfia. Ranquel (I A)46). Neiva. (I PD-5802). Sud. Gardan-Horizon (GY-80). LaVerda. Falco (F8L Series II, America). Malmo. Vipan (MFI-IO). Kingsford Smith. Autocrat (SCRM- 153).

O-320-A2B

.Aero Commander. 100. Piper Aircraft. Tri-Pacer (PA-22 Cub (PA- I8 “ 150”). Champion Aircraft. Challenger Agriculture (7GCBA). Beagle. Pup (I 50). Artic. Interstate S I B2. Robinson. R-22.

0-320-A2C

Varga. Kachina 2 I50A. Robinson. R-22. Cicare. Cicare AC;.

O-320-.421)

Bcllanca

0-320-A3-2

Piper Aircraft. Doyn Aircraft. Corben-Fettcs.

Aircraft.

Citabria

“I 50”, PA-22S (7(&I,

I50 (7GCAA),

7GCB,

Citabria

Apache (PA-23). Doyn-Cessna ( 170. l70A. I70B). Globe Special (Globe GC- I B).

30

“I 50”), Cherokee 7KC),

Citabria

150s (7GCBC).

(PA- I8A “I 50”) Super

(PA-28

“I 50”), Super

(7GCAA,

7GCRC),

PlSTON - (4) FOUR CYLINDER

0

INSTALLATIONS

0-320-A3B ............

Piper Aircraft. Apache (PA-23). Doyn Aircraft. Doyn-Cessna (I 70, 170A, 170B). Teal II. TSC (I A2).

0-320-Bl A ............

. Piper Aircraft. Apache (PA-23 “160”). Doyn Aircraft. Doyn-Cessna (170, 170A, 170B). Malmo. Vipan (MFI-IO).

O-320-Bl B . . . . . . . . . . . .

. Piper Aircraft. Doyn Aircraft.

Apache (PA-23 “160”). Doyn-Cessna (170, 170A, 170B).

O-320-B2A ............

. Piper Aircraft.

Tri-Pacer (PA-22 “160”, PA-22s “160”).

O-320-B2B ............

. Piper Aircraft. Tri-Pacer (PA-22 “160”, PA-22s “160”). Beagle. Airedale (D5-160). Fuji-Heavy industries. Fuji (F-200). Uirapuru. Aerotec 122.

O-320-B2C . . . . . . . . . . . .

. Robinson. R-22.

0-320-B2D . . . . . . . . . . . . . . . . . . Maule. MX-7- 160. O-320-B3A..................

Piper Aircraft. Doyn Aircraft.

Apache (PA-23 “160”). Doyn-Cessna (170, 170A, 170B).

O-320-B3B . . . . . . . . . . . . . . . . . . Piper Aircraft. Apache (PA-23 “160”). Doyn Aircraft. Doyn-Cessna (170, 170A, 1708). Sud. Gardan (GY80- 160). O-3204

A . . . . . . . . , . . . . . . . . . Piper Aircraft. Apache (PA-23 “I 60”). Riley Aircraft. Rayjay (Apache).

0-320X1 B . . . . . . . . . . . . . . . . . . Piper Aircraft.

Apache (PA-23 “160”).

O-320-C3A . . . . . . . . . . . . . . . . . . Piper Aircraft.

Apache (PA-23 “160”).

O-320-C3B . . . . . . . . . . . . . . . . . . Piper Aircraft.

Apache (PA-23 “160”).

O-320-DlA

. . . . . . . . . . . . . . , . . . Sud. Gardan (GY-80). Gyroflug. Speed Cancard. Grob. G 115.

O-320-Dl F . . . . . . . . . . . . . . . Slingsby. T67 Firefly. O-320-D2A . . . . . . , . . . . . . . . . . . Piper Aircraft. Cherokee (PA-28s “160”). Robin. Major (DR400-140B), Chevalier (DR-360), (R-3 140). S.O.C.A.T.A. Tampico TB9. Slingsby. T67C Firefly. Daetwyler. MD-3- 160. Nash Aircraft Ltd. Petrel. Aviolight. P66D Delta. General Avia. Pinguino. O-320-D2B . . . . . . . . . . . . . . . . . . Beech Aircraft. Musketeer (M-23). Piper Aircraft. Cherokee (PA-28 “I 60”) O-320-D2J

.

. . . . . . . . . . . . Cessna Aircraft.

O-320-D3G . . . . . . O-320-EIA O-320-ElC .

.

.

. . . . Piper Aircraft.

Skyhawk 172. Warrior II, Cadet (PA-28- 16 I ).

. . . . . Grob. G115. .. . .. . .

M.B.B. (Messerschmitt-Boelkow-Blohm). 31

Monsun (H( )-ZOQ HI

PISTON - (4) FOUR CYLINDER

INSTALLATIONS

O-320-El F . . . . . . . . . . . . . . . . . . M.B.B. Monsun (BO-209-B). O-320-E2A . . . . . . . . . . . . . . . . . Piper Aircraft. Cherokee (PA-28 “140”, PA-28 “150”). Robin. Major (DR-340) Sitar, Bagheera (GY-100-135). S.O.C.A.T.A. Super Rallye (MS-886), Rallye Commodore (MS-892). Siai-Marchetti. (S-202). F.F.A. Bravo (AS-202/l 5). Partenavia. Oscar (P66B), Bucker (13 1 APM). Aeromot. Paulistina P-56. Pezetel. Koliber 150. O-320-E2C . . . . . . . . . . . . . . . . . . Beech Aircraft. Musketeer 111(M-23111). M.B.B. Monsun (BO-209-B). O-320-E2D . . . . . . . . . . . . . . . . Cessna Aircraft.

Cardinal (172-1, 177).

O-320-E2F . . . . . . . . . . . . . . . . M.B.B. Monsun (BO-209-B), Wassmer Pacific (WA-5 1). O-320-E2C . . . . . . . . . . . . . . . . . . American Aviation Corp. Traveler. O-320-E3D..................

Piper Aircraft. Cherokee (140). Beech Aircraft. Sport.

. . . . . . . . . . . . . Cessna Aircraft. Skyhawk 172. Partenavia. P-66C.

O-320-H2AD

IO-320-Bl A .................

Piper Aircraft.

Twin Comanche (PA-30).

IO-320-BIG

.................

Hi. Shear. Wing.

IO-320-BID

.................

Ted Smith Aircraft.

Aerostar.

IO-320X1 A .................

Piper Aircraft.

IO-320-Dl A .................

M.B.B. Monsun (BO-209-C).

IO-320-DIB

.................

M.B.B. Monsun (BO-209-C).

IO-320-El A .................

M.B.B. Monsun (BO-209-C).

IO-320-El B .................

BeIIanca Aircraft.

IO-320-E2A .................

Champion Aircraft.

IO-320-E2B .................

Belianca Aircraft.

IO-320-Fl A .................

CAAR Engineering. Carr Midget.

LIO-320-Bl

A ...............

Piper Aircraft.

Twin Comanche (PA-39).

LIO-320-Cl

A ...............

Piper Aircraft.

Twin Comanche (PA-39).

AIO-320-Bl

B ...............

M.B.B. Monsun (BO-209-C).

AEIO-320-Dl AEIO-320-D2B

B .............. ..............

Twin Comanche (PA-30 Turbo).

Slingsby. T67M Firefly. Hundustan Aeronautics Ltd. HT-2.

AEIO-320-E IA ..............

Bellanca Aircraft. Champion Aircraft.

AEIO-320-E

Bellanca Aircraft. Champion Aircraft.

I

Citabria.

Decathalon (SKCAB-CS). 32

PlSTON - (4) FOUR CYLINDER AEIO-320-E2B.

.

. . Bellanca Aircraft. Champion Aircraft.

Decathalon Twin.

O-340-Al A

.

.

0-360-A I A . .

.

..

Riley Aircraft.

Riley

INSTALLATIONS

(SKCAB).

Beech Aircraft. Travel Air (95, B-95). Piper Aircraft. Comanche (PA-24). Intermountain Mfg. Co. Call Air (A-6). Lake Aircraft. Colonial (C-2, LA-4, 4A or 4P). Doyn Aircraft. Doyn-Cessna (I 70B, 172, I72A, I72B). Mooney Aircraft. Mark “20B” (M-20B). Earl Horton. Pawnee (Piper PA-25). Dinfia. Ranquel (I A-5 I ). Neiva. ( I PD-590 I ). Regente. (N-59 I). Wassmer. Super 4 (WA-SOA), Sancy (WA-40), Baladou Sud. Gardan

(GY-

(WA-40)

Pariou

(WA-40)

180).

Bolkow. (207). Partenavia. Oscar (P-66). Siai-Marchetti. (S-205). Procaer. Picchio (F-15-A). S.A.A.B. Safir (9 I-D). Malmo. Vipan (MF- I OB). Aero Boero. AB- 180. Beagle. Airedale (A- 109). DeHavilland. Drover (DHA-3MK3). Kingsford-Smith. Bushmaster (55-6). Aero Engine Service Ltd. Victa (R-2). O-360-AIAD.. O-360-Al D

S.O.C.A.T.A. Tabago TB-IO. .

Piper Aircraft. Comanche (PA-24). Lake Aircraft. Colonial (LA-4, 4A or 4P). Doyn Aircraft. Doyn-Beech (Beech 95). Mooney Aircraft. Master “21” (M-20E), Statesman (M-20(3). Dinfia. Querandi (I A-45). Wassmer. (WA-50). Malmo. Vipan (MFI-IO). Cessna Aircraft. Skyhawk. Doyn Aircraft. Doyn-f’iper

(PA-23

Mark

“2OB”,

” 160”).

O-360-Al F6

Cessna Aircraft.

O-360-Al F6D

Cessna Aircraft. Cardinal Teal Ill. I‘SC (IA3)

O-360-AlG6..

Afro Commander.

O-36%AlG6D

Beech Aircraft.

Duchess 76

O-360-A I H6

Piper Aircraft.

Seminole

0-360-A I LD

Wassmer. Europa WA-52

0-360-A I f’

Aviat. f-fusky

0-360-A2A

Center Est Aeronautique. Regcntc (DR-253). S.O.C.A.T.A. Rallye Commodore (MS-893). Societe Aeronautique Normande. Mousquetaire Bolkow. Klemm (K I - 107C). Partenavia. Oxar (P-66j. Beagle. Husky (DS-I 80) (J I -IJ).

Cardinal. 177.

(PA-44)

33

(D- 140)

“2OD”,

(M20B,

M2OC),

Mooney

PISTON-

(4) FOUR CYLINDER

INSTALLATIONS

O-360-A2D

.................

Piper Aircraft. Comanche (PA-24) Cherokee “C” (PA-28 “I 80”). Mooney Aircraft. Master “2 I” (M-20D), Mark “2 I” (M-20E).

O-320-A2E

.................

Std. Helicopter.

O-360-A2F

.................

Aero Commander. Lark (I 00). Cessna Aircraft. Cardinal.

O-360-A2C

.................

Beech Aircraft.

O-360-A3A

.................

C.A.A.R.P.S.A.N. (M-23111). Societe Aeronautique Normande. Jodel (D-140C). Robin. Regent (DR400/ I 80) Remorqueur (DR400/ I 80R). R-3 I 70. S.O.C.A.T.A. Rallye l80GT, Sportavia Sportsman (RS- 180). Norman Aeroplace Co. NAC-I Freelance. Nash Aircraft Ltd. Petrel.

O-360-A3AD

...............

Sport.

S.O.C.A.T.A. TB-IO. Robin. Aiglon (R-l 180T).

O-360-A4A

.................

Piper Aircraft.

O-360-A4D

..................

Varga.

O-360-A4C

..................

Beech Aircraft.

O-360-A4K

..................

Grumman American. Tiger. Beech Aircraft. Sundowner 180.

O-360-A4M

.................

Piper Aircraft. Archer II (PA-28 “18.‘). Valmet. PIK-23.

O-360-A4N

..................

Cessna Aircraft.

O-360-A4P.

.................

O-360-ASAD.

...............

O-360-B2C. O-360-CIA

................. ..................

Kachina.

Seabird

Aviation.

Intermountain Bcllanca

0-360-Cl

F ..................

Maule.

O-360-C2B.

.................

I72 (Optional).

C. ltoh and Co. Fuji FA-200.

E ..................

..................

Musketeer Custom III.

Penn Yan. Super Cub Conversion.

0-360-Cl

0-360-Cl