311.2712.255

285.0211.221

596.2923.476

365.1314.375

182.567.188

63.802.512

673.5426.518

24.639625.84 22.619

574.53

5.668143.98

3.91299.36

91.313.595

535.7521.093

682.8226.883

176.736.958

53.842.119

162.776.408

ENGINE MOUNT REARSURFACE

REAR MOUNT PLATE

PROP HUB

MUFFLER CAN BE TRIMMED PER INSTALLATION

9.843250

17.717450

9.252235

27510.827

4.921125

4.331110

4.921125

6.496165

8.858225

8.858225

27510.827

219.088.625

REAR MOUNT PLATE AND PROP HUBALL OTHER COMPONENTS NOT SHOWN FORCLARITY

FRONT VIEW LOOKING AFT

ALL DIMENSIONS IN PARENTHESES ARE MILLIMETER

REVISIONSREV. DESCRIPTION BY DATE

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

E

F

E

F

REV

1051

0120

D

FINISH

10510120SHEET 1 OF 1

LAYOUT FOR ENGINE CONFIGS

UNLESS OTHERWISE SPECIFIED:

REVDWG. NO.

DSIZE

Description:

Viking AircraftEngines

NAME DATE

Q.A.

MFG APPR.

ENG APPR.

CHECKED

DRAWN

STOCK SIZE

MATERIAL

INTERPRET GEOMETRICTOLERANCING PER:

DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL

PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OFEGGENFELLNER AIRCRAFT. ANYREPRODUCTION IN PART OR AS AWHOLE WITHOUT THE WRITTEN PERMISSIONOF EGGENFELLNER AIRCRAFT. IS PROHIBITED.

.03

.010

.5.5