Aeronca • Champion • Citabria

Total Page:16

File Type:pdf, Size:1020Kb

Aeronca • Champion • Citabria AERONCA • CHAMPION • CITABRIA Bearing Block ....................................................................U1-2599 .......... $81.41 Rudder Cable Pulley Bushing ............................................ U1-2636 .......... $22.80 1 Tail Surface Hinge Pin Bushing ( ⁄4” ID) ..............................U1-3737 ............ $5.64 3 CONTENTS Tail Surface Hinge Pin Bushing ( ⁄16” ID) ..........................U1-3737-1 ............ $5.07 Throttle Control Arm ...........................................................U2-715 ........$119.22 Univair carries hundreds of quality FAA-PMA Control Stick Boot ...............................................................U2-750 ..........$30.90 approved and original factory parts specifically Aeronca/Citabria Torque Tube..............................................U2-816 ........$162.34 for the Aeronca 7 and 11 series, Champion, Champion Arm ....................................................................U2-817 ........$337.81 Rudder Pedal.......................................................................U3-448 ........$137.79 Bellanca Citabria, Decathlon and Scout. We also have distributor parts such as tires, batteries, tailwheels, and more. Control Cables Control System ..................................................4 • See website for aircraft applicability Engine ...............................................................5 • Cables are priced and sold individually Fuel System .......................................................5 Frame ................................................................5 Landing Gear ....................................................6 Manuals ............................................................7 Propellers ..........................................................8 Description Part # Price Struts ................................................................8 Throttle Control, 60.0” ......................................................U1-670-2 ........$197.30 Throttle Control, 54¾” ......................................................U1-670-3 ........$210.27 Tail Section ........................................................9 Short Aileron Cable, 35.5”, Galvanized .............................. U1-2397 ..........$45.03 Windows • Windshields ...................................10 Stainless Steel ............................................................ U1-2397S ..........$75.56 Long Rudder Cable, 168.69”, Galvanized ...........................U1-2364 ........$116.26 Wings ..............................................................10 Stainless Steel ............................................................ U1-2364S ........$129.71 Many parts can be correctly identified by the Short Rudder Cable, 28.75”, Galvanized ............................ U1-2280 ........$104.84 Stainless Steel ............................................................ U1-2280S ........$151.03 nomenclature listed in this section. However, we Aileron Control Cable, 104.03”, Galvanized ........................U1-2339 ..........$89.61 suggest that you also have the correct parts Stainless Steel ............................................................ U1-2339S ........$108.36 manual for positive identification. Brake Cable and Housing Assembly .....................................1-2358 ........$124.43 Brake Cable, 113.5”, Galvanized .....................................U1-2358-2 ..........$47.43 Stainless Steel .........................................................U1-2358-2S ..........$56.23 Brake Cable Housing ......................................................... U1-2578 ..........$62.55 Down Elevator Cable, 141.88”, Galvanized ..........................U2-686 ........$143.19 Stainless Steel .............................................................. U2-686S ........$183.20 7 Citabria Down Elevator Cable, 144 ⁄16”, Galvanized ............ U2-1534 ........$175.13 Control System Stainless Steel ............................................................ U2-1534S ........$170.25 Trim Cable, 172.13”, Galvanized ..........................................U2-698 ..........$88.54 Stainless Steel .............................................................. U2-698S ..........$99.23 Description Part # Price Elevator Up Cable, Long Section: 122.38”, Short Section: 19.0” Rudder Pedal Return Spring ................................................U1-769 .......... $14.04 Galvanized Steel .............................................................U3-471 ........$348.50 Aeronca Pushrod ...............................................................U1-2341 ........$148.90 Stainless Steel .............................................................. U3-471S ........$338.89 Torque Control Tube .......................................................... U1-2383 ........$111.92 Rudder Cable, 182.875”, Galvanized ...............................U1-2496-2 ..........$57.36 Aeronca Shear Plate ..........................................................U1-2394 ............ $8.57 Rudder Cable, 184.1875”, Galvanized .............................U1-2496-3 ..........$57.43 Rudder Trim Fairlead Pulley...............................................U1-2395 ..........$14.73 Brake Cable, 72.0” ............................................................U2-776-2 ..........$81.05 Aeronca Cable Fairlead ......................................................U1-2396 .......... $23.32 Aileron Cable, 103.75” .........................................................U2-777 ..........$75.40 5 Rudder Pedal Bearing Tube ...............................................U1-2411 ..........$19.03 Trim Cable, 183 ⁄16”, Galvanized ......................................... U2-1905 ..........$78.67 Rear Rudder Pedal Spring ................................................. U1-2568 .......... $49.51 Stainless Steel ............................................................ U2-1905S ..........$78.91 Aileron Control Sector Guard ................................................1-2573 ............ $7.76 Elevator Up Cable, Long Section: 134.3125”, Short Section: 8.9375” Front Brake Cable Housing, Left ........................................ U1-2578 ..........$62.55 Galvanized ....................................................................U3-1072 ........$284.72 Stainless Steel ............................................................ U3-1072S ........$341.45 4 Price and availability subject to change without notice • Univair’s Toll Free Sales: 1-888-433-5433 AERONCA • CHAMPION • CITABRIA Carburetor Air Boxes Engine • Applicability: Citabria, Decathlon, Scout • Top of air box is NOT included Aeronca Baffles Citabria/Decathlon .......U3-1546...... $534.43 Scout (shown) ..........U3-1546-1...... $554.78 Baffle, Crankcase (Champion) • Aeronca 11B, 11C, 7DC • FAA-PMA approved • Applicability: Aeronca 7AC, 11AC • Air filter included U4-742 ...........................$51.15 Carburetor Air Box Baffle (L-16 A/B) Includes Air Filter ........U4-601-1 ......$760.84 • Applicability: Aeronca L-16-85 Air Filter Only ..................... U2-849 ......$116.61 7-582 ...........................$112.33 Air Filter Baffle (L-16 A/B) • Applicability: 1974 and later 7-583 ...........................$112.33 7GCAA, 7GCAB, 7GCBC, 7ECA • Supersedes part numbers P10-4145 and 0750038-4 All-Aluminum Cowling Air filter ......................P10-6150...... $162.00 • Applicability: Aeronca 7AC/11AC Nose Cowl .............................U4-576 .....$1,652.26 Fuselage Cowl (7AC only) ......U7-466 ........$854.35 Fuel System Top Cowl ...............................U7-473 ........$468.29 Bottom Cowl .........................U7-472 ........$401.40 Gascolator Support Engine Mounts 2-727 ......................................................$40.88 Continental Engine 7AC/11AC ..........................U4-585 ........$681.83 7EC/7FC ............................U4-884 ........$703.34 Fuel Vent Deflector Lycoming Engine 7ECA, 7GCAA, 7GCBC ......U4-1033 .....$1,628.92 • Applicability: Aeronca 7ECA, 7GCAA, 7GCBC, 7KCAB 7KCAB .......................U4-1033-10 ........$601.17 U3-1508 .......................................................$74.08 Citabria Air Induction Tube Fuel Gauge Cover U7-1475-4 ..............................$22.76 For Citabria............................U3-1389 ......$102.04 Exhaust System • Applicability: Aeronca 7AC/11AC Frame • Stacks are metalized – coated with pure aluminum sprayed at 6800°F for increased life of the stacks Description Part # Price Left Stack ..................U7-485 ......$384.81 Eyelet Bushing (Short) ............................................................276D ............ $0.48 Right Stack ................U7-486 ......$384.81 Eyelet Bushing (Long) ...............................................................581 ............ $0.16 Heat Muff ...........U3-478/479 ......$290.87 Strut and Landing Gear Fitting .............................................1-2263 ..........$29.08 Price and availability subject to change without notice • Shop online at www.univair.com 5 AERONCA • CHAMPION • CITABRIA Strut and Landing Gear Fitting ..........................................U1-2264 ..........$41.43 Oleo Shock Strut Front Landing Gear Plate .....................................................1-2265 ............ $1.99 Front Landing Gear Fitting ................................................U1-2266 ..........$41.16 Landing Gear Center Fitting .............................................. U1-2326 ..........$37.13 Fairing ..............................................................................
Recommended publications
  • Montebello Magic March 2017 Warmth of Winter’S Biggest Fly-In
    THE JOURNAL OF THE CANADIAN OWNERS AND PILOTS ASSOCIATION COPAFLIGHT MONTEBELLO MAGIC MARCH 2017 WARMTH of Winter’S BIGGEST FLY-IN COMING UP SHORT THE 850-FOOT INVITATION LOTS OF NEW CLASSIFIED ADS TEENS FLY RV-12 BASICMED VS. CAT 4 CANSO READY TO FLY #42583014 BUILDING CAREERS ON MEDICAL REFORM CELEBRATE WITH M P THE ISLAND COMPARISON FAIRVIEW JUNE 18 NAVITIMER COPA Limited Edition Breitling proudly launches the Navitimer World COPA, a 50-piece limited edition chronograph honoring the Canadian Owners and Pilots Association and perfect for global flight. The Breitling Navitimer has been a favorite among pilots and aviation enthusiasts since it was introduced in 1952 – the same year that COPA was founded. Powered by a COSC-certified selfwinding chronograph movement, this new and exclusive addition to the Navitimer series paying tribute to COPA’s contribution to general aviation features a dial and caseback showcasing the COPA logo. BREITLING.COM COPA_NavitimerGMT_8,5x11inches-BR17480.indd 1 30/05/2016 11:30 COPAFLIGHT EDITOR Russ Niles CONTENTS [email protected] 250.546.6743 GRAPHIC DESIGN Shannon Swanson DISPLAY ADVERTISING SALES Katherine Kjaer 250.592.5331 [email protected] CLASSIFIED ADVERTISING SALES AND PRODUCTION COORDINATOR Maureen Leigh 1.800.656.7598 [email protected] CIRCULATION Maureen Leigh AccOUNTING Anthea Williams ASSISTANT ADMIN Rajei Gill COPA BOARD Bernard Gervais, President and CEO 34 Executive Committee Jean Messier Feature Departments Chair, Quebec Director Bram Tilroe Western Vice-Chair, Alberta
    [Show full text]
  • Mcdonnell Douglas (Boeing) MD-83
    Right MLG failure on landing, Douglas (Boeing) MD-83, EC-FXI Micro-summary: The right main landing gear of this Douglas (Boeing) MD-83 failed immediately on landing. Event Date: 2001-05-10 at 1232 UTC Investigative Body: Aircraft Accident Investigation Board (AAIB), United Kingdom Investigative Body's Web Site: http://www.aaib.dft.gov/uk/ Note: Reprinted by kind permission of the AAIB. Cautions: 1. Accident reports can be and sometimes are revised. Be sure to consult the investigative agency for the latest version before basing anything significant on content (e.g., thesis, research, etc). 2. Readers are advised that each report is a glimpse of events at specific points in time. While broad themes permeate the causal events leading up to crashes, and we can learn from those, the specific regulatory and technological environments can and do change. Your company's flight operations manual is the final authority as to the safe operation of your aircraft! 3. Reports may or may not represent reality. Many many non-scientific factors go into an investigation, including the magnitude of the event, the experience of the investigator, the political climate, relationship with the regulatory authority, technological and recovery capabilities, etc. It is recommended that the reader review all reports analytically. Even a "bad" report can be a very useful launching point for learning. 4. Contact us before reproducing or redistributing a report from this anthology. Individual countries have very differing views on copyright! We can advise you on the steps to follow. Aircraft Accident Reports on DVD, Copyright © 2006 by Flight Simulation Systems, LLC All rights reserved.
    [Show full text]
  • Tilt Rotor Research Aircraft Familiarization Document
    '. NASA TECHNICAL NASA TMX-62.407 MEMORANDUM -PTING Y. a c NASA/ARMY TILT ROTOR RESEARCH AIRCRAFT FAMILIARIZATION DOCUMENT Prepared by .Tilt Rotor Project Office .. .. -\ Coordinated by Martin Maid .. Ames Research Center ._ I rJ - ,.. -1 and , 1-1 c. U.S. Amy Air Mobility R&D Laboratory %\\-'?. \ Moffett Field, Calif. 94035 .-, 7 / --_ ---*_ c-, : January 1975 NASMARMY XV-15 TILT ROTOR RESEARCH AIRCRAFT FAMl LIARIZATION DOCUMENT Prepared by: Tilt Rotor Research Aircraft Project Office Staff Coordinated by: Martin D. Maisel Tilt Rotor Research Aircraft Project Office Approved by : - Dean C. Borgman Deputy Manager, Technical Tilt Rotor Research Aircraft Project Office David D. Few Manager Tilt Rotor Research Aircraft Project Office 1. Report No. 2. Ganmnmt hionNo. 3. Recipient's Catalog No. TM X-62,407 4. Titlr md Subtitlo 5. Rqwn D~te NASA/ARMY XV-15 TILT ROTOR RESEARCH AIRCRAFT FAMILIARIZATION DOCUMENT 7. Author(s) 8. PerformingOrgnizrtion Report No. Prepared by Tilt Rotor Project Office Staff, A-5870 coordinated by Martin Maisel 10. Work Unit No. 9. paforming ororriatia, "and MdNI 744-01-01 NASA Ames Research Center and 11. Canmct or Grant No. U.S. Army Air Mobility R&D Laboratory Moffett Field, Calif. 94035 13. Typ of RIpon and hid &ard 12. -nuring N.m md Addnr Technical Memorandum National Aeronautics and Space Administration 1;. Sponsoring Agmcy Code Washington, D.C. 20546 16. Abmrcr , The design features and general characteristics of the NASA/Army XV-15 Tilt Rotor Research Aircraft are described. This aircraft was conceived as a proof-of-concept vehicle and a V/STOL research tool for integrated wind tunnel, flight-simulation, and flight-test investigations.
    [Show full text]
  • Large Capacity Oblique All-Wing Transport Aircraft
    f Large Capacity Oblique All-Wing Transport Aircraft Thomas L. Galloway James A. Phillips Robert A. Kennelly, Jr. NASA Ames Research Center Moffett Field, CA Mr. Mark H. Waters Thermosciences Institute, ELORET Corp. Palo Alto, CA Transportation Beyond 2000: Engineering Design for the Future September 26-28, 1995 461 INTRODUCTION Dr. R. T. Jones first developed the theory for oblique wing aircraft in 1952, and in subsequent years numerous analytical and experimental projects conducted at NASA Ames and elsewhere have established that the Jones' oblique wing theory is correct. Until the late 1980's all proposed oblique wing configurations were wing/body aircraft with the wing mounted on a pivot. With the emerging requirement for commercial transports with very large payloads, 450 - 800 passengers, Jones proposed a supersonic oblique flying wing in 1988. For such an aircraft all payload, fuel, and systems are carded within the wing, and the wing is designed with a variable sweep to maintain a fixed subsonic normal Mach number. Engines and vertical tails are mounted on pivots supported from the primary structure of the wing. The oblique flying wing transport has come to be known as the Oblique All-Wing transport (OAW). Initial studies of the OAW were conducted by Van der Velden first at U.C. Berkeley(l) in 1989 and then at Stanford in collaboration with Kroo(2) in 1990. A final document summarizing this work is given in the thesis by Van der Velden(3). Many issues regarding the design were identified in these studies, among them the need for the OAW to be an unstable aircraft.
    [Show full text]
  • Cessna 210 Back in The
    HANGAR ECHOES September 2018 cessna 210 back in the air From Michael Stephan Experimental Aircraft Association! ! Chapter 168 ! Dallas With great fanfare, I am proud to announce that Ted Harrison’s “backyard” Article Index Cessna 210 is now flying. Actually it first Ted Harrison’s 210 Cover flew on May 25. Since that day it has spent time at the avionics show having Monthly Schedule page2 some modern Garmin avionics installled Presidents Message page 3 in the center stack, including a ADS-B In/ N168TX Sold page 3 Out compliant transponder installed. Then it was off to the paint shop. The 210 Walt Aronow Page 4 spent a few weeks at GLO Custom at Don Pellegreno Page 6 Northwest Regional Airport. Induction Leaks Page 7 Ted has been in aviation most of his life. FltPlan.com Page8 As a youngster Ted learned to fly in his Local Fly Ins Page 8 Dad’s Aeronca sedan. His cut his communication teeth on a narco “coffee Project Updates Page 9 grinder” that had three crystals. Once he Tool List PG 10 learned to solo, Ted would fly from Upcoming Events PG 10 Payson AZ, where he lived, to Falcon Field (east of Pheonix) for his flight For Sale PG 11 lessons. Since every lesson consisted of a September 2018 Volume 49 Issue 9 Page 1 HANGAR ECHOES Monthly Schedule Sept 4th Chapter Meeting September 4th Board Meeting The September Chapter meeting The September BOD meeting will be held on Tues Sept will be on Tuesday Sept 4th at 4th in Farmers Branch Library Auditorium at 5:30pm.
    [Show full text]
  • ATINER's Conference Paper Series IND2013-0819
    ATINER CONFERENCE PAPER SERIES No: IND2013-0819 Athens Institute for Education and Research ATINER ATINER's Conference Paper Series IND2013-0819 Optimally Adaptive Oleo Strut Damping for Aircraft and UAV Using MR Fluid Ajinkya A. Gharapurkar Graduate Research Assistant Dept. of Mechanical and Industrial Engineering, Concordia University Canada Chandra B. Asthana Affiliate Associate Professor Dept. of Mechanical and Industrial Engineering, Concordia University Canada Rama B. Bhat Professor Dept. of Mechanical and Industrial Engineering, Concordia University, Canada 1 ATINER CONFERENCE PAPER SERIES No: IND2013-0819 Athens Institute for Education and Research 8 Valaoritou Street, Kolonaki, 10671 Athens, Greece Tel: + 30 210 3634210 Fax: + 30 210 3634209 Email: [email protected] URL: www.atiner.gr URL Conference Papers Series: www.atiner.gr/papers.htm Printed in Athens, Greece by the Athens Institute for Education and Research. All rights reserved. Reproduction is allowed for non-commercial purposes if the source is fully acknowledged. ISSN 2241-2891 23/1/2014 2 ATINER CONFERENCE PAPER SERIES No: IND2013-0819 An Introduction to ATINER's Conference Paper Series ATINER started to publish this conference papers series in 2012. It includes only the papers submitted for publication after they were presented at one of the conferences organized by our Institute every year. The papers published in the series have not been refereed and are published as they were submitted by the author. The series serves two purposes. First, we want to disseminate the information as fast as possible. Second, by doing so, the authors can receive comments useful to revise their papers before they are considered for publication in one of ATINER's books, following our standard procedures of a blind review.
    [Show full text]
  • Sequence of Design
    Sequence Or Design By Noel Becar, EAA 725 316 Del Rosa Way, San Mateo, Calif. VERALL DESIGN was discussed in an earlier article der to prove OGt strength after as much lightening of the O in this series, but no summarization was made as it design as possible has been done. was felt the subject matter was too general and too varied (D)—Reduction of parasite resistance to the mini- to be of reference value on paper. However, a quick sum- mum, even at the cost of a small increase in weight, is mary of points covered might be helpful. Overall design desirable for low horsepower designs by such means as can best be defined as, "consideration of all the pertinent full-cantilever wings and retraction of landing gear and factors entering into the obtaining of maximum perform- other power consuming drag items. ance with minimum horsepower" in the case of light Design Sequence. The first step in designing a new aircraft. As a quick check list, the following factors airplane is the decision of what type is to be built. In should be included: practically all cases, structural considerations will indi- (A)—Consideration of a higher landing speed than cate a monoplane as the best design for simplicity and might normally be specified if we do not want a plane the least drag for its size. Also, for a given area of wing, which is uncomfortable to fly in rough air,—for the prop- in order to obtain the same performance, a biplane would erty of an airplane that allows it to ride bumps com- have to have an extremely short chord which would make fortably is dependent on its landing speed.
    [Show full text]
  • T-45C Aircraft
    VIRTUAL NATOPS FLIGHT MANUAL NAVY MODEL T-45C AIRCRAFT for Microsoft Flight Simulator by IndiaFoxtEcho Visual Simulations Version 1.00 – March 2021 NOTICE – Although this manual and the simulated aircraft closerly resemble their real-world counterparts in many aspects, neither should be used as source of real-world information about the aircraft. This package is not endorsed or supported by The Boeing Company or by the United States Navy. CHANGE LOG VERSION 1.10 22-Mar-2021 - Redone external engine sounds - Replaced internal engine sound main loop sample - Fixed bug preventing setting the CRS on TACAN (Nav2) - Created "Lite" versions of all aircrafts, with simplified XML code and geometry - Implemented VR mouse collision model - Fixed environmental occlusion geometry - Fixed missing details in rear cockpit harnessing - Fixed bug causing cockpit sounds from other T-45 to play in multiplayer - Fixed formation light switch INOP - Fixed bug causing the HUD throttle indicator not to work - Fixed external lights not working after Sim Update 3 - Changed animation of retractable footstep so that automatically retracts when the canopy closes - Changed HUD ILS logic so that ILS steering bar will only show if ILS is selected on the HSI-MFD - Added TAWS Below Glideslope warning - Added TAWS Check Gear warning - Added TAWS Power Power warning INITIAL RELEASE 8-Mar-2021 WELCOME The T-45 Goshawk is a fully carrier-capable version of the British Aerospace Hawk Mk.60. It was developed as a jet flight trainer for the United States Navy and United States Marine Corps. The Hawk had not originally been designed to perform carrier operations; numerous modifications were required, such as the extensive strengthening of the airframe to withstand the excessive forces imposed by the stresses involved in catapult launches and high sink-rate landings, both scenarios being routine in aircraft carrier operations.
    [Show full text]
  • Introduction to Airplane Performance Prof. AK Ghosh Department Of
    NOC: Introduction to Airplane Performance Prof. A. K. Ghosh Department of Aerospace Engineering Indian Institute of Technology, Kanpur Module - 01 Lecture - 03 Introduction to airplane and its components (Refer Slide Time: 00:09) This is Sinus 912 aircraft which is a motor glider and its manufacturer is Pipistrel. So, we will today we will discuss about the structure and the instrument panel of this motor glider. This is an all made its construction is of composite material. This is the spinner of the aircraft having a 2 bladed propeller which is vireo. Then, it has a rotex 912 engine installed in it which is a 4 cylinder engine and it is a piston engine 4 stroke. Moving ahead we come to the wing. This is the starboard wing of the aircraft which is containing a pitot tube. This is the pitot tube which senses the pitot pressure and the static pressure from the static veins located just beneath it. It senses the dynamic pressure and gives to the pitot instruments like ASI, altimeter and vertical speed indicator. (Refer Slide Time: 00:59) Then, it has a wing span of 15 meters. For this wing contains a flaperon. Normally all aircrafts have either aileron and a flap, but in this varying motor glider the 2 control surfaces are combined in one and then that is of flaperon which consist of a flap and aileron that helps in rolling and as well as at the time of takeoff and landing. (Refer Slide Time: 01:24) So, this is the impeller section of the aircraft this is the tail section which consist of the vertical stabilizer, the horizontal stabilizer; attached to it is the moving part that is the elevator and the rudder.
    [Show full text]
  • Dirigo Flyer
    Dirigo Flyer Newsletter of the Maine Aviation Historical Society PO Box 2641, Bangor, Maine 04402 207-941-6757 1-877-280-MAHS (in state) www.maineairmuseum.org [email protected] Volume XIX No. 3 May – June 2011 Welcome to our late spring – early summer issue of the Flyer. After a rather dreary start that consisted of many days of dark, wet, IFR only weather, we have broken out of the clouds and are enjoying some warm, seasonal summer weather as this is being written. The editor had a nice flight around Mt. Desert Island the other day in a WACO biplane (traded a trip around Frenchman Bay by boat for it) in nice smooth flying conditions. I should have spent the day editing this issue but…flying took precedent. Port O’Maine Airport By Brian Wood Every year for my birthday my father would spend the day taking me any place I wanted to go. For my 14th, it was decided that we would have lunch at Portland’s Sportsman’s Grill for my favorite meal – spaghetti. After that we could go out to the airport and watch planes. After an hour watching a few Northeast DC3’s and DC6’s taxi in, things slowed down and we decided to go down to South Portland and see if we could find another airport we had heard about. It was called Port O’Maine Airport. After some searching we found it off Route One. Little did I know that I was about to receive the best birthday present ever! Port O’Maine was everything an airport should be with a long unpaved runway, two shorter ones, a windsock pond, a cement maintenance hangar full of planes in various states of disassembly, rows of small planes tied up on the grass and a wonderful terminal building.
    [Show full text]
  • Sun 'N Fun '78
    SUN 'N FUN '78 •:'X:i:. '•; IH I \,,-.(,::-:- • ••»**' sr «?*!' «--.«j *!*N*te-. ' fiiw. 4^; ••*» " ~ ,r t = ^ ^ -..-.,. .,, : 'A:. « f»: *s«7 •' , ' - t • - ^ ...v~ (Photo by Bill Ehlen) Sun 'N Fun exhibit area and campground. Show plane parking is just to the left of this view. The Piper plant is at the top left. By Jack Cox (Photos By The Author Unless Otherwise Credited) o',F THE FLY-INS I cover during the course of each day . from a Milwaukee that had not seen a day above year, Sun 'N Fun is different in one respect. When I freezing for almost a month. During the day we would get back to the office in Wisconsin, the first thing the rest meet Floridians at the airport complaining about the of the staff want is a weather report . and then they "cold." That evening we would go back to the motel, ask about the airplanes. switch on the TV, watch scenes of wintery devastation as Visit Wisconsin in January sometime and you'll under- the worst blizzard in anyone's memory plastered home stand why! country . and thank our lucky stars we were here in- Well, everything is relative, as they say. The first three stead of there!! It was easy to spot the Yankees on the days at Lakeland were sunny and pleasant, the tempera- field the next day . we were the ones with the wide ture in the low 80s on Wednesday. That night, however, smiles. a cold front roared through, dropping the daytime highs End of weather report. into the 50s for the rest of the week.
    [Show full text]
  • Annual Nd Flying Farmers and Ranchers 1
    .. , *1• JUNE, 1948 20C * CAMPAIGN TO PASS GAS TAX AMENDMENT .#...1 - b *S. D. AIR TOUR JUNE 3-4-5-6 * EXPERIMENTAL PILOT COURSE * < * ANNUAL AIR FAIR JUNE 27 * ANNUAL N. D. FLYING FARMERS AND RANCHERS _1 -- I' l'-! + , CONVENTION JUNE 24-25 , 4- J J ATTENTION , - Neighbor U 1- 1-,-1-4.ZYAEK-.W and Farmer: -*lb-/<Id'm)- - 3' Agriculture is here to stay However, the profits from agriculture are never assured until the crop Is harvested Now modern aviation has developed ap- pl ication methods for the positive con- trol of weeds and insects in a crpland _ and pasture with the use of a proven ester formulation of 2,4-D. Also great strides have been made todarws the use of airplanes in seeding acreages. The THOMPSON SPRAY CO, INC, invites your attention to Its complete aerial spray and seeding service with licensed pilots and qualified crop tech- niques to fulfill your demands May we invite you to attend one or more of these following meetings featuring aerial spraying, Agriculture's full color sound movies on spraying and how it can make a greater yield and profit for every farmer that wishes to avail his farm to this modern service. Cleans weeds out of small grains, corn, ffax, and --- Get the facts todoy on farm pastures PROVED-on more than 500, , DOD acres in 19471 Use no more than 1 gallon of oil per acre with only 2/4 to 2 pints of Weed-No-More! 1 NEW FREE BULLETINS - Before you buy any 2, 4-D TRADE MARK weed killer, get all the facts on Agricultural- Weed-No- More performance on farms like yours Ask for our new free bulletins.
    [Show full text]