PROPRIETARY AND CONFIDENTIAL: THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF LANCAIR INTERNATIONAL, INC. REPRODUCTION IN PART OR AS A WHOLE WITHOUT THE WRITTEN PERMISSION OF LANCAIR INTERNATIONAL, INC. IS PROHIBITED. INITIAL RELEASE. CENTER OF THE ENGINE PROP FLANGE IS AT BL (BUTT LINE) 0 AND 3.25" UNDER CANOPY LEDGE CANOPY OPENING ON FUSELAGE USED TO LEVEL AND A REFERENCE WATERLINE 41.5" BETWEEN FIREWALL AND PROP FLANGE MEASURE HEIGHT OF COMPLETELY EXTENDED STRUT AND FULL TIRE. CLEARANCE BETWEEN PROP AND GROUND AT LEAST 1/2" WITH STRUT AND TIRE DEFLATED NOSE GEAR 0-3 RAKE FORWARD 34" STRUT FULLY EXTENDED TIRE INFLATED PER ASME Y14M - 1994. ALL DIMS IN INCHES UNLESS OTHERWISE NOTED. TOLERANCES .XXX .005 .XX .01 .X .025 FRACTIONS 1/32 ANGLES 30' NOTES: 1. ALL DIMENSIONS EXCEPT ENGINE ANGLES WERE TAKEN DIRECTLY FROM A LEGACY FIXED GEAR. 2. THE AIRCRAFT DOES NOT SIT LEVEL IN NORMAL CONDITION (NOSE HIGH). 3. ENGINE IS 1.5 DOWN AND 1.5 TO THE RIGHT COMPARED WITH LEVEL AIRCRAFT. MATERIAL: PART NUMBER SHEET SIZE FINISH: DEBURR & REMOVE SHARP EDGES FIRST USED ON: LEGACY FIXED GEAR ENGINE MOUNT REFERENCE DRAWING 3 CAD FILE: \\Lindbergh\shared files- lii\Graphics - Paint Schemes - Line Art - 3D Models\Legacy\AutoCAD Line Art\ Legacy FG, Side Profile, Lines

PROPRIETARY AND CONFIDENTIAL: THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF LANCAIR INTERNATIONAL, INC. REPRODUCTION IN PART OR AS A WHOLE WITHOUT THE WRITTEN PERMISSION OF LANCAIR INTERNATIONAL, INC. IS PROHIBITED. PART NUMBER CAD FILE: \\Lindbergh\Shared Files- LII\Graphics - Paint Schemes - Line Art - 3D Models\Legacy\AutoCAD Line Art\ Legacy, Top Profile, Lines