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Rans S-19 VENTERRA Manual

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S-19 VENTERRA
TEXT MANUAL
Serial Number:
Registration Number:
COPYRIGHT ©
RANS DESIGNS
4600 HWY 183 Alt
HAYS, KANSAS, USA 67601
785-625-6346
www.rans.com

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Summary of Contents for Rans S-19 VENTERRA

  • Page 1 S-19 VENTERRA TEXT MANUAL Serial Number: Registration Number: COPYRIGHT © RANS DESIGNS 4600 HWY 183 Alt HAYS, KANSAS, USA 67601 785-625-6346 www.rans.com...
  • Page 4 RANS S-19 VENTERRA Text Manual TEXT MANUAL INDEX GENERAL INFO ........................00 GETTING STARTED ........................01 EMPENNAGE (TAIL) GROUP ....................02 WING ASSEMBLY ........................03 FLAP AND AILERON ASSEMBLY .....................04 FUSELAGE – CENTER SECTION .....................05 FUSELAGE – FORWARD SECTION ..................06 FUSELAGE - TAILCONE......................07 FUSELAGE – SYSTEMS......................08 MAIN &...

  • Page 5: Table Of Contents

    RANS S-19 VENTERRA Text Manual 00 - GENERAL INFO HOW TO ASSEMBLE YOUR S-19 ASSEMBLY MANUAL............00-1 REVISION FORM ........................00-4 TECHNICAL SUPPORT ......................00-6 AIRCRAFT TOOL LIST......................00-7 HAND TOOLS...........................00-7 POWER TOOLS ........................00-7 LUBRICANTS, ADHESIVES & TAPES..................00-7 CLECO FASTENERS .......................00-8 DRILL BIT, REAM SIZES & COUNTERSINK CUTTERS ............00-8 TOOLS AND MATERIALS NEEDED FOR CASTING LEAD BALLAST WEIGHTS ....00-8...
  • Page 6 RANS S-19 VENTERRA Text Manual MANDATORY TEST FLIGHT PROVING PHASE ..............00C-1 PURPOSE OF THE FLIGHT TEST PERIOD................. 00C-1 DURATION OF MANDATORY FLIGHT TEST PERIOD............00C-2 FLIGHT TEST AREA ......................00C-2 OTHER LIMITATIONS DURING THE FLIGHT TEST PERIOD..........00C-3 AIRCRAFT FLIGHT LOG....................... 00C-3 REPAIRMAN’S CERTIFICATION ..................

  • Page 7: General Info

    RANS S-19 VENTERRA Text manual 00-1 GENERAL INFO HOW TO ASSEMBLE YOUR S-19 ASSEMBLY MANUAL Your manual is ready for assembly: Place the TEXT manual in the larger 3 ring binder. Place the PARTS and FIGURES manuals in the smaller 3 ring binders. Every page has a section number then a page number within that section.
  • Page 8 RANS S-19 VENTERRA Text manual 00-2 Designed for 1 ¼” Insertable Tabs 04/01/2011...
  • Page 9 RANS S-19 VENTERRA Text manual 00-3 Labels for the exterior of each manual may be made from self-stick labels. The format below may be used. RANS RANS RANS S-19 S-19 S-19 TEXT PARTS FIGURE MANUAL MANUAL MANUAL Use the revision form on the next page to record any manual revisions sent to you by RANS.

  • Page 10: Revision Form

    RANS S-19 VENTERRA Text manual 00-4 REVISION FORM Revision # Pages Description Date Affected Original Original Issue 04/01/2011 04/01/2011...

  • Page 11: Technical Support

    RANS S-19 VENTERRA Text manual 00-5 RANS Designs 4600 Highway 183 Alternate Hays, KS 67601 Technical Support (785) 625-0069 actech@rans.com Parts Department (785) 625-6346 parts@rans.com When calling Technical Support or the Parts Department please have the following ready: • Aircraft Model •...
  • Page 12 RANS has taken care to provide clear, comprehensive, and straightforward instructions for assembly, maintenance, and operation by reference to manuals alone. In the event a question arises for which no answer seems apparent, feel free to contact RANS headquarters. Physical and mailing address:...RANS Designs...

  • Page 13: Aircraft Tool List

    RANS S-19 VENTERRA Text manual 00-7 AIRCRAFT TOOL LIST The following is a list of tools that will be helpful when assembling your RANS S-19. HAND TOOLS Pliers Safety Wire Pliers Needle Nose Pliers Vise Grip Pliers Needle-Nose Vise Grip Pliers...

  • Page 14: Cleco Fasteners

    RANS S-19 VENTERRA Text manual 00-8 CLECO FASTENERS The following are considered minimum quantities. 3/32” (Cadmium / Silver) 1/8” (Copper) 5/32” (Black) 3/16” (Brass / Gold) DRILL BIT, REAM SIZES & COUNTERSINK CUTTERS ® A Unibit Step Drill ranging from 1/4” to 3/4” and conventional bits ranging from 1/8” to 3/8”...

  • Page 15: Inventory, Preparation And Workspace

    RANS S-19 VENTERRA Text Manual 00A-1 INVENTORY, PREPARATION AND WORKSPACE TAKE INVENTORY: You must complete an inventory within 60 days of receiving your kit. We check and re-check and are 99.9% certain that if we say we shipped it, we did. The first task in building your kit is to inventory the parts using the packing list provided.
  • Page 16 RANS S-19 VENTERRA Text Manual 00A-2 PLEASE READ: We highly recommend that you completely read the manual cover to cover before beginning assembly of your aircraft. This will help to eliminate costly mistakes and considerably speed up your build time. As you read through the Assembly Manual, follow along in the Parts and Figure Drawings Manual.
  • Page 17 RANS S-19 VENTERRA Text Manual 00A-3 CLECOS: The tool list calls out the minimum quantity required. You may wish to purchase more. These are temporary fasteners that will be used to hold things together while fitting and drilling. A pair of Cleco pliers is required to install and remove the clecos.
  • Page 18 00A-4 HAVE FUN! A RANS aircraft is almost as much fun to build as it is to fly and with a little care and planning, your ship could be a show stopper...Send us and the magazine's pictures of your work in progress or your finished plane.

  • Page 19: Aircraft Registration

    RANS S-19 VENTERRA Text Manual 00B-1 AIRCRAFT REGISTRATION Introduction: All aircraft of U.S. registry are required to have the following documentation onboard. For aircraft registered in other countries contact your National Aviation Authority. Certificate of Airworthiness Registration Operating Limitations Weight and Balance Information NOTE: The bold letters above spell out AROW.

  • Page 20: Affidavit Of Ownership Form

    RANS S-19 VENTERRA Text Manual 00B-2 To avoid confusion with the numbers one and zero, the letters I and O are not to be used. An N-Number may not begin with zero. You must precede the first zero in an N-Number with any number 1 through 9.

  • Page 21: Registering Your Aircraft

    RANS S-19 VENTERRA Text Manual 00B-3 REGISTERING YOUR AIRCRAFT After you have written the Aircraft Registry requesting an "N" number, you will receive a form letter giving your number assignment. You will also receive a blank Aircraft Registration Form. (Sample Enclosed.) Complete the Application for Aircraft Registration (Form 8050-1) and return it to the Aircraft Registry along with the $5.00...

  • Page 22: I Feel I Am Ready For Inspection By The Faa Inspector, What Do I

    RANS S-19 VENTERRA Text Manual 00B-4 MY AIRCRAFT IS COMPLETED, ALL MARKING AND PLACARDS ARE IN PLACE. WHAT ELSE MUST I DO TO MY AIRCRAFT BEFORE I AM READY FOR MY PRE- CERTIFICATION INSPECTION? Included in your manual is a weight and balance sheet. This will need to be completed before the inspection.

  • Page 23: Final Inspection

    RANS S-19 VENTERRA Text Manual 00B-5 6. The area over which you will be testing. (Request an area encompassing a 25 mile radius for day VFR operations. Exclude congested areas and airways, but try to include nearby airports even if a few miles beyond the 25 mile radius.
  • Page 24 RANS S-19 VENTERRA Text Manual 00B-6 (4) Instruments—for poor condition, mounting, marking, and (where practicable) improper operation. (5) Flight and engine controls—for improper installation and improper operation. (6) Batteries—for improper installation and improper charge. (7) All systems—for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment.
  • Page 25 RANS S-19 VENTERRA Text Manual 00B-7 (3) Linkages, trusses, and members—for undue or excessive wear fatigue, and distortion. (4) Retracting and locking mechanism—for improper operation. (5) Hydraulic lines—for leakage. (6) Electrical system—for chafing and improper operation of switches. (7) Wheels—for cracks, defects, and condition of bearings.
  • Page 26 RANS S-19 VENTERRA Text Manual 00B-8 (3) Bonding and shielding—for improper installation and poor condition. (4) Antenna including trailing antenna—for poor condition, insecure mounting, and improper operation. (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation.

  • Page 27: Sample Checklist For A Condition Inspection

    RANS S-19 VENTERRA Text Manual 00B-9 SAMPLE CHECKLIST FOR A CONDITION INSPECTION AC90-89 APPENDIX 1 AIRCRAFT IDENTIFICATION: TYPE/SN ENGINE MODEL/SN _________________ “N” NUMBER PROPELLER MODEL/SN __________________ A/F TOTAL TIME ENGINE TOTAL TIME ____________________ OWNER PROPELLER TOTAL TIME ________________ BUILDER INSPECTOR...
  • Page 28 RANS S-19 VENTERRA Text Manual 00B-10 WING ATTACH POINTS FLYING/LANDING WIRES/STRUTS FOR SECURITY CORROSION FLIGHT CONTROL PLACARDS INSPECT FIREWALL FOR DISTORTION AND CRACKS INSPECT RUDDER PEDALS AND BRAKES FOR OPERATION AND SECURITY INSPECT BEHIND FIREWALL FOR LOOSE WIRES AND CHAFFING LINES...
  • Page 29 RANS S-19 VENTERRA Text Manual 00B-11 ENGINE: PERFORM COMPRESSION TEST #1 CHANGE OIL AND FILTER (CHECK FOR METAL) INSPECT IGNITION HARNESS FOR CONDITION AND CONTINUITY CHECK IGNITION LEAD CIGARETTES FOR CONDITION/CRACKS CLEAN AND GAP SPARK PLUGS CHECK MAGNETO TIMING/POINTS/OIL SEAL/DISTRIBUTOR...
  • Page 30 RANS S-19 VENTERRA Text Manual 00B-12 ELECTRICAL SYSTEM CHECK COOL DOWN PERIOD/ENGINE SHUT DOWN PERFORM OIL, HYDRAULIC, AND FUEL LEAK CHECK PAPERWORK: AIRWORTHINESS DIRECTIVES RECORD FINDINGS AND SIGN OFF INSPECTION AND MAINTENANCE IN LOGBOOKS 04/01/2011...

  • Page 31: Numbering And Placards

    RANS S-19 VENTERRA Text Manual 00B-13 NUMBERING AND PLACARDS WHAT ARE THE SPECIAL REQUIREMENTS AS FAR AS ATTACHING NUMBERS AND PLACARDS TO HOMEBUILT AIRCRAFT? DISPLAY OF MARKS LOCATION OF MARKS ON FIXED WING (Reference is FAR Part 45.23) AIRCRAFT (Reference is FAR Part 45.25)

  • Page 32: Identification Plate

    RANS S-19 VENTERRA Text Manual 00B-14 IDENTIFICATION PLATE The identification plate containing these (Reference is FAR Part 45.11) essential elements must be of fireproof material and must be secured in such a In addition to affixing the aircraft’s manner that it will not likely be defaced or...

  • Page 33: Aircraft Instrument Markings & Cockpit Placards

    RANS S-19 VENTERRA Text Manual 00B-15 AIRCRAFT INSTRUMENT MARKINGS & COCKPIT PLACARDS Your reference is FAR Part 91.9 Civil Aircraft Operating Limitations and Marking Requirements GENERAL To insure that each person operating an aircraft does so within the operating limitations prescribed for it, the FAA requires that there is available in it a current Flight Manual, appropriate instrument marking and placards, or any combination thereof.

  • Page 34: Airspeed Instrument Markings

    RANS S-19 VENTERRA Text Manual 00B-16 AIRSPEED INSTRUMENT MARKINGS The airspeed indicator should be marked with a red radial line to establish the never- exceed speed. (Vne). The takeoff and any pre-cautionary range should be marked with a yellow arc. The normal range is marked with a green arc.

  • Page 35: Flight Maneuver Placard

    RANS S-19 VENTERRA Text Manual 00B-17 FLIGHT MANEUVER PLACARD For non-acrobatic category airplanes, there should be a placard in front of and in clear view of the pilot stating: “No acrobatic maneuvers, including spins, approved.”. For acrobatic category airplanes, there should be a placard in clear view of the pilot listing the approved acrobatic maneuvers and the recommended entry airspeed for each.

  • Page 36: Operating Limitations

    RANS S-19 VENTERRA Text Manual 00C-1 OPERATING LIMITATIONS MANDATORY TEST FLIGHT PROVING PHASE All amateur-built sport aircraft as well as standard aircraft have federally imposed operating limitations. Upon satisfactory completion of the necessary final FAA Inspection of the aircraft and whatever ground tests may be required, the FAA inspector will issue your amateur-built “Experimental”...

  • Page 37: Duration Of Mandatory Flight Test Period

    RANS S-19 VENTERRA Text Manual 00C-2 DURATION OF MANDATORY FLIGHT TEST PERIOD For standard aircraft type engines: When an FAA approved aircraft engine/propeller combination is installed, the flight test period is usually limited to 25 hours of flight time. For automotive engines, non-FAA approved engines or propellers, or FAA approved...

  • Page 38: Other Limitations During The Flight Test Period

    RANS S-19 VENTERRA Text Manual 00C-3 OTHER LIMITATIONS DURING THE FLIGHT TEST PERIOD As a rule, the carrying of passengers or other crew members will not be permitted unless necessary to the safe operation of that aircraft. AIRCRAFT FLIGHT LOG During the flight test period, the pilot should record the aircraft flight history in an appropriate log book.

  • Page 39: Repairman's Certification

    RANS S-19 VENTERRA Text Manual 00C-4 REPAIRMAN’S CERTIFICATION The Repairman’s Certificate is applied for using the application form 8610-2, available from the local FAA offices. You should ask for this when you apply for your final inspection on your aircraft. You should also be familiar with the Appendix D of FAR part 43.

  • Page 40: Rotax ® Engine Warranty Information

    Procedure At the time of purchase the Purchaser will choose which service center he wants to use for warranty service. RANS will register with that service center. Warranty after the warranty period In case where a new engine is not put into service for some period of time after the end user purchase date, and a service or warranty issue arises, any claim for warranty consideration will be reviewed on a case by case basis.
  • Page 41 RANS S-19 VENTERRA Text Manual 01 - GETTING STARTED GETTING TO KNOW THE RANS S-19 VENTERRA..............01-1 TYPICAL HARDWARE AND DRILL SIZE TABLE*..............01-3 PAINT AND CORROSION PROTECTION ................01-4 PRIMING..........................01-4 PAINTING ..........................01-4 S-19 VENTERRA ASSEMBLY FLOW CHART.................01-5 04/01/2011...

  • Page 42: Getting Started

    Get your S-19 Venterra manuals, find the FIGURES manual, and refer to FIGURES 01– 01 thru 01–08.
  • Page 43 RANS S-19 VENTERRA Text Manual 01-2 Lay a straight edge across the ribs to insure that the ribs will lay flush with the skin. Adjust the rib flanges with padded pliers as necessary. Keep your work area clean and free from shavings. If practical, keep a blowgun handy to keep the work surface free from shavings.

  • Page 44: Typical Hardware And Drill Size Table

    RANS S-19 VENTERRA Text Manual 01-3 Typical Hardware and Drill Size Table*. Hardware Drill Size 40 APR Rivet AAPQ-41 thru 48 CCPQ-41 thru 48 AAPQ-62 thru 68 CCPQ-62 thru 68 SSPQ-62 thru 68 AVEX 1691-0410 AN3 Bolt AN4 Bolt 1/4"...

  • Page 45: Paint And Corrosion Protection

    01-4 PAINT AND CORROSION PROTECTION Painting of the S-19 Venterra is optional, but priming the steel parts of the airplane is mandatory. The information given below is only one example of how an airplane can be painted. There are many ways to do this and this may not represent the best method for your situation or climate.

  • Page 46: S-19 Venterra Assembly Flow Chart

    RANS S-19 VENTERRA Text Manual 01-5 S-19 VENTERRA ASSEMBLY FLOW CHART 04/01/2011...
  • Page 47 RANS S-19 VENTERRA Text Manual 02-1 02 - EMPENNAGE (TAIL) GROUP VERTICAL STABILIZER ASSEMBLY..................02-1 RUDDER ASSEMBLY ......................02A-1 STABILATOR ASSEMBLY ....................02B-1 ANTI-SERVO / TRIM TAB ASSEMBLY ................. 02C-1 STABILATOR BALANCING ....................02D-1 04/01/2011...

  • Page 48: Empennage (Tail) Group

    RANS S-19 VENTERRA Text Manual 02-1 EMPENNAGE (TAIL) GROUP VERTICAL STABILIZER ASSEMBLY NOTE: A 1.25” dia. x 95” long Aluminum (or PVC) Tube will be required for forming the Leading Edges of the Rudder, Flaps & Ailerons. • Vertical stabilizer assembly must be performed on a flat work surface.
  • Page 49 RANS S-19 VENTERRA Text Manual 02-2 Using cleco clamps secure the parts tightly together. The bottom edge of the spar and the bottom edge of the reinforcing angles should line up together. Transfer drill the parts #40 and cleco. Cleco the vertical stabilizer plate rear spar (KPVS0060), plate reinforcement (KPVS0078), and vertical fin hinges (KPVS0077) to the rear spar.
  • Page 50 RANS S-19 VENTERRA Text Manual 02-3 Move the front spar until the edge of top rib lines up with the edge of the skin. Check that the bottom edge of the skin has an equal amount of overhang over the bottom rib.
  • Page 51 RANS S-19 VENTERRA Text Manual 02-4 Using the Parts Drawing as a guide, rivet the skins to the vertical stabilizer frame. Trim the vertical stabilizer tip fairing (KPVS0071) to the scribe lines. Position the tip fairing inside the forward skin and over the tip bulkhead.

  • Page 52: Rudder Assembly

    RANS S-19 VENTERRA Text Manual 02A-1 RUDDER ASSEMBLY NOTE: A 1.25” dia. x 95” long Aluminum (or PVC) Tube will be required for forming the Leading Edges of the Rudder, Flaps & Ailerons. • Rudder assembly must be performed on a flat work surface. Assembly on a warped surface will result in a warped rudder •...
  • Page 53 RANS S-19 VENTERRA Text Manual 02A-2 Cut apart and profile the strips of Skin Stiffeners (KPRD0069) per FIGURE 02A- 13. Cleco to the inside of each Rudder Skin (KPRD0073). Be sure to make a Left and Right skin. Slide the Rudder Skins into the rudder jig on the outer sides of the Rudder Frame.

  • Page 54: Stabilator Assembly

    RANS S-19 VENTERRA Text Manual 02B-1 STABILATOR ASSEMBLY • Stabilator assembly must be performed on a flat work surface. Assembly on a warped surface will result in a warped stabilator • Sandbags will be required in parts of the assembly to hold the stabilator flat to the work surface •...
  • Page 55 RANS S-19 VENTERRA Text Manual 02B-2 The rear spar of the stabilator will need to be supported at the outboard ends of the spar. Cut 2 wooden blocks the appropriate height to support the ends of the spar when resting on the table. Verify that the rear spar is straight by pulling a string line across the ends of the jig and aligning the spar to it.
  • Page 56 RANS S-19 VENTERRA Text Manual 02B-3 Cut hinges to length and mark a center-line on the flange. See FIGURE 02B-25. Position the hinges and hinge doublers in the rear spar. (Make sure the center- line is visible through the holes in the spar.) Drill and cleco #40.
  • Page 57 RANS S-19 VENTERRA Text Manual 02B-4 Remove the clecos from the end rib and the Spar Attach Angle. Be careful to have the jig supported while removing the clecos as not to damage the skins. Remove the rib from the end jig.

  • Page 58: Anti-Servo / Trim Tab Assembly

    RANS S-19 VENTERRA Text Manual 02C-1 ANTI-SERVO / TRIM TAB ASSEMBLY • Anti-servo/trim tab assembly must be performed on a flat work surface. Assembly on a warped surface will result in a warped anti-servo/trim tab • Sandbags will be required in parts of the assembly to hold the anti- servo/trim tab flat to the work surface •...
  • Page 59 RANS S-19 VENTERRA Text Manual 02C-2 Cleco assembly together and place back on blocks and rivet. Bend hinge pins and cut as shown in FIGURE 02C-17. Drill stabilator rear spar and secure pin with safety wire as shown in FIGURE 02C-18.

  • Page 60: Stabilator Balancing

    RANS S-19 VENTERRA Text Manual 02D-1 STABILATOR BALANCING • Stabilator balancing must be performed on a flat work surface. • Stabilator and Anti-Servo / Trim Tab must be final painted. • Anti-Servo / Trim Tab must be installed onto Stabilator.
  • Page 61 RANS S-19 VENTERRA Text Manual 02D-2 WARNING: This procedure requires you to melt Lead to 600+ degrees and pour it into a mold. Please use the appropriate safety equipment when performing this operation. Obtain all tools and material needed for Casting Lead Ballast Weights called out in the General Section of the Text Manual.
  • Page 62 RANS S-19 VENTERRA Text Manual APPENDIX EF-38E - ENGINEERING DEPT. DRAWING NUMBERING SYSTEM.......APPENDIX-1 RIVET CROSS REFERENCE LIST ................APPENDIX-2 AN3 - AN8 AIRFRAME BOLTS.................APPENDIX-3 AN BOLT GAUGE......................APPENDIX-4 AFFIDAVIT OF OWNERSHIP ..................APPENDIX-5 ELIGIBILITY STATEMENT ..................APPENDIX-6 APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE........APPENDIX-8 04/01/2011...

  • Page 63: Ef-38E - Engineering Dept. Drawing Numbering System

    RANS S-19 VENTERRA Text Manual APPENDIX-1 EF-38E - ENGINEERING DEPT. DRAWING NUMBERING SYSTEM RANS designates parts by eight variables ( . This system consists of letters XXXX and numbers. The following is the breakdown of this system. CLASSIFICATION DWG TYPE...

  • Page 64: Rivet Cross Reference List

    RANS S-19 VENTERRA Text Manual APPENDIX-2 RIVET CROSS REFERENCE LIST DIA. RANS POP RIVET CHERRY Q SHEAR TENSILE GRIP SHEAR TENSILE GRIP 3/32 (#41) 40APR1/8 AD32ABS .031-.125 3/32 (#41) 40APR1/4 AD34ABS .126-.250 3/32 (#41) 40APR3/8 AD36ABS .251-.375 1/8 (#30) 30APR1/16 AAPQ-41 .0-.062...

  • Page 65: An3 - An8 Airframe Bolts

    RANS S-19 VENTERRA Text Manual APPENDIX-3 AN3 - AN8 AIRFRAME BOLTS AN3-AN8 CADMIUM-PLATED STEEL BOLTS (DRILLED AND UNDRILLED) A non-corrosion-resistant steel machine bolt which conforms to Specification MIL-B-6812. Cadmium- plated to Specification QQ-P-416. Available with or without single hole through shank and/or single hole through head. Examples of part members for a cadmium plated steel bolt having a diameter of 1/4"...

  • Page 66: An Bolt Gauge

    RANS S-19 VENTERRA Text Manual APPENDIX-4 AN BOLT GAUGE █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████ ████████████████ █████████████████...

  • Page 67: Affidavit Of Ownership

    RANS S-19 VENTERRA Text Manual APPENDIX-5 AFFIDAVIT OF OWNERSHIP - AC FORM 8050-88 The most current AC8050-88 is available on the FAA website as an interactive PDF file. 04/01/2011...

  • Page 68: Eligibility Statement

    RANS S-19 VENTERRA Text Manual APPENDIX-6 ELIGIBILITY STATEMENT – FAA FORM 8130-12 The most current FAA FORM 8130-12 is available on the FAA website as an interactive PDF file. 04/01/2011...
  • Page 69 RANS S-19 VENTERRA Text Manual APPENDIX-7 04/01/2011...

  • Page 70: Application For U.s. Airworthiness Certificate

    RANS S-19 VENTERRA Text Manual APPENDIX-8 APPLICATION FOR U.S. AIRWORTHINESS CERTIFICATE – FAA FORM 8130-6 The most current FAA FORM 8130-6 is available on the FAA website as an interactive PDF file. 04/01/2011...
  • Page 71 RANS S-19 VENTERRA Text Manual APPENDIX-9 04/01/2011...
  • Page 72 RANS S-19 VENTERRA Text Manual APPENDIX-10 04/01/2011...