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    Remember, We’re Better Together! 

    www.auaonline.com

     Aviation insurance with the EAA Vintage Program offers: 

    Lower premiums with payment options Additional coverages Flexibility on the use of your aircraft Experienced agentsOn-line quote request available AUA is licensed in all states

    The best is affordable. Give AUA a call – it’s FREE!

    Fly with the pros… fly with AUA Inc.

    800-727-3823

     AUA is Vintage Aircraft Association approved. To become a member of VAA call 800-843-3612.

    Ev has flown more than 100 types of airplanes and he has flownmore Ryan airplane types than any other living pilot.

    Dealing in any way with AUA is an old-time pleasure. Theyare, courteous, pleasant, thorough, personable, businesslike,competitive, and on top of that - they love old airplanes andtalk the language too. 

    — Ev Cassagneres 

    Ev CassagneresCheshire, Connecticut

    ■ Commercial Pilot 

    ■ Flying since 1945 

    ■ Ryan Aircraft Historian

    ■ Author

    a  n  s  A  U 

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      2  Straight & Level  Embracing change  by H.G. Frautschy

      3  News

    6 Making an Old Friend New Again  Envy of the airport—he flies an Aeronca  by Sparky Barnes Sargent

    14 Carburetors Are the Difference  by Steve Krog, CFI

    20 Light Plane Heritage  The Unique Longhead S-1

    by Bob Whittier

    26 The Vintage Mechanic  Engine cowls for drag reduction—Part I  by Robert G. Lock

    30 The Vintage Instructor  Flight reviews make them fun—Part II  by Steve Krog, CFI

     34 Mystery Plane  by H.G. Frautschy

     37  Classified Ads

    39 Making a Ramp Check a Short-Order Event  by Steven W. Oxman

    VINTAGE AIRPLANE 1

    A I R P L A N E A U G U S T

    C O N T E N T S

    S T A F FEAA Publisher Rod Hightower

    Director of EAA Publications Mary JonesExecutive Director/Editor H.G. FrautschyProduction/Special Project Kathleen Witman

    Photography Jim KoepnickCopy Editor Colleen WalshSenior Art Director Olivia P. Trabbold

    EAA Chairman of the Board Tom Poberezny

    Publication Advertising:Manager/Domestic, Sue Anderson

    Tel: 920-426-6127 Email: [email protected] Fax: 920-426-4828

    Senior Business Relations Mgr, Trevor Janz

    Tel: 920-426-6809 Email: [email protected] 

    Manager/European-Asian, Willi Tacke

    Phone: +49(0)1716980871 Email: [email protected]: +49(0)8841 / 496012

    Interim Coordinator/Classified, Alicia CanzianiTel: 920-426-6860 Email: [email protected] 

    C O V E R S

    Vol. 39, No. 8 2011

    FRONT COVER: The jaunty Aeronca Champ restored by Frank Jacobs cruises the skies of

    east-central Wisconsin. Since the beginning of the 1980s, the Champ and i ts sibling, the

    Chief, have been favorites of Aeronca restorers, thanks to their simple structure and fine fly-

    ing characteristics. Many Champs and Chiefs now qualify for operation by operators with sport

    pilot certificates. Read about Jacob’s Champ in Sparky Barnes Sargent’s story beginning on

    page 6. Photo by EAA Chief Photographer Jim Koepnick

    BACK COVER: “A Course In Aviation for Fifteen Cents a Month” the cover copy crowed

    about Model Airplane News , now the longest running model airplane magazine published

    under the same same name. Model Airplane News  ran this cover featuring the Nor thrup

    Alpha mailplane in January of 1933.

    14

    6

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    2  AUGUST 2011

    While President Geoff Ro-

    bison attends to some ur-

    gent family business, I’d

    like to take this oppor-

    tunity to thank each of you who at-

    tended EAA AirVenture 2011, and if

    you’re a VAA or EAA volunteer, you

    get a double “Thank you!” for your

    efforts. We really could not do it

    without you!Every year Theresa Books, VAA’s

    administrative assistant, and I en-

    joy the hectic month of July as our

    friends and fellow volunteers head to

    Oshkosh from all over North Amer-

    ica, and some even come to Oshkosh

    from overseas. It’s always good to see

    so many great folks, many of whom

    we get to see only once a year. Some

    are faces we’ve seen for more than 20

    years, and others are newer volun-

    teers. It’s a great mix of people whoall have enthusiasm for aviation as a

    common interest.

    So many of us in the EAA family

    have strong interests, and this wide

    world of aviation is part of what

    makes it so interesting. So many of

    our fellow VAA members have an

    equal interest in homebuilt airplanes,

    and quite a few have one or more

    of each in their hangars. Within the

    VAA family, we’ve got members who

    really like antiques best of all, andothers who really love their contem-

    porary or classic airplanes. Addressing

    the needs of each of these groups has

    been one of the most challenging as-

    pects for the offerings from the VAA.

    Each of them has particular needs,

    and at times it can be quite a juggling

    act to ensure we’re doing our best to

    meet members’ expectations with the

    resources at hand.

    Every day means change; some

    changes are for the better, some “just

    happen” without active work on our

    behalf. We have gone from fairly rudi-

    mentary cellphone communications

    to multi-media wireless communica-

    tions we can access nearly anywhere.

    The Internet as we know it was really

    just getting fired up, and since most

    of us were just getting started with

    using a 56k phone modem, it was a

    good thing that those early websiteswere pretty rudimentary!

    Now we have access to various fo-

    rums and websites that allow us to

    share information and enjoy the

    social aspects of being involved in

    aviation to whatever extent we de-sire. With all this change, it leads us

    to ask, on a regular basis, what it is

    our members desire from the VAA.

    Vintage Airplane magazine has long

    been your primary member benefit,

    along with an outstanding insuranceprogram administered by AUA Inc.

    We’ve had a website for more than

    a decade, and we have an active and

    growing component of EAA’s online

    community on www.Oshkosh365.org .

    But as we all know, change is inevi-

    table, and if we don’t actively man-

    age the change, some of it may not

    work out for the better. Oshkosh365.

    org will see some changes in the near

    future to enhance its usability, and

    we’re actively working on getting allof Vintage Airplane available in an on-line archive where members can read

    or download any issue.

    This fall, we’ve been planning on

    surveying the VAA membership on

    a variety of subjects related to their

    expectations and desires, and to

    help enhance the knowledge gained

    by that survey, I’ve got a few ques-

    tions for you, and I’m looking for-

    ward to hearing from as many of

    you as possible.

    If you could add one more thing to

    the member benefits you receive as a

    Vintage Aircraft Association member,

    what would it be? Why?

    Is there a current member bene-

    fit that you don’t feel is worth keep-

    ing? Why?

    Besides Vintage Airplane magazine,

    what other means of communica-

    tion would you like to see offered byVAA? What would you like to see in

    those communications? How-to vid-

    eos? Profiles of vintage aircraft restor-

    ers? Historical pieces of a particular

    aircraft or personality?

    If you’ve got an idea or comment

    about anything related to VAA and

    its activities, including the annual

    fly-in and convention, please feel free

    to send them as well. As EAA mem-

    bers, you have access to a wide vari-

    ety of member benefits, and while wedon’t want to duplicate their efforts,

    if you have a suggestion on how we

    can “fine-tune” an offering to make it

    fit better for your needs, please don’t

    hesitate to make a suggestion. Feel

    free to send us a response using what-

    ever method you prefer, either mail or

    e-mail. Our mailing address is:

    Vintage Aircraft Association

    PO Box 3086

    Oshkosh, WI 54903

    Or e-mail us at [email protected] .

    Once again (we can never say it

    enough!), “Thanks!” to each and ev-

    ery one of you who is a member of

    the VAA, and to each of you who en-

    hanced their membership experience

    by volunteering for the VAA. On be-

    half of Theresa Books and me, we’d

    just like to say that you folks are the

    best, and we enjoy helping you enjoy

    your love of vintage airplanes!

    H.G.

    H.G. FRAUTSCHY

    EXECUTIVE DIRECTOR, VAA

    STRAIGHT & LEVEL

    Embracing change

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    VAA NEWS

    VINTAGE AIRPLANE 3

    Marion Cole

    Longtime EAA and Vintage Air-

    craft Association members who

    recall one of the earliest pilots fly-

    ing a 450-hp Stearman in an air

    show act will be saddened to hear

    of the passing of Marion Franklin

    “Master” Cole, who lost a coura-

    geous battle with pancreatic can-cer on Friday, July 8, in Louisiana,

    at the age of 86. Marion, EAA

    Lifetime 48 and a founding (No.

    9) IAC member, was a part of the

    famous Cole Brothers Flying Cir-

    cus for 17 years, then flew the lead

    Pitts with Bob Heuer and Gene

    Soucy in the original Red Devils

    formation team. He is a past U.S.

    National Aerobatic Champion

    and competed as a member of the

    U.S. Aerobatic Team at Magde-

    burg, East Germany, in 1968. As

    an aerobatics instructor, Marion

    provided training for many of the

    great names in competitive and

    air show aerobatics.

    “Marion was a longtime sup-

    porter of EAA and one of the most

    outstanding aerobatic pilots I ever

    met,” said EAA Founder Paul Po-berezny. “Especially in the 450-hp

    Stearman—in my opinion, Mar-

    ion was top of the line in the pre-

    cision handling of that aircraft.

    He served as a role model for the

    entire aerobatic community, just a

    wonderful man.

    “Time flies too rapidly for us

    human beings.”

    Mar ion Co le was bo rn on

    December 9, 1924, in Toulan

    Township, Illinois. He became

    a “hangar brat” at an early age,

    cleaning airplanes and hangars—

    anything to earn a ride with a lo-

    cal pilot. He soloed at age 16 and

    never looked back.

    Marion joined the serv ice as

    soon as he was of age and be-

    came a flight instructor in the

    Navy. Following World War II,he flew with his brothers in the

    Cole Brothers Air Shows, then

    formed Marion Cole Air Shows,

    with which he performed until

    the early 1990s. Marion was alsoan aerobatic inst ructor, flight

    instructor, FAA examiner, a cor-

    porate pilot for 32 years, and

    a national and world aerobatic

    competitor. In all he logged more

    than 31,000 flight hours.

    Marion was a founding mem-

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    ber of the International Aerobatic

    Club, taught aerobatics at the ba-

    sic and advanced levels, and tu-

    tored many young aerobatic pilots

    for more than 50 years. He flew air

    shows throughout the continental

    United States from the late 1940s

    to the early 1990s. He retired from

    the air show circuit but continuedto council, tutor, and announce

    for young aerobatic hopefuls and

    attended several air shows, in-

    cluding AirVenture, each year.

    He is survived by his wife of 66

    years, Charlene; sons Bill and wife

    Norma, Larry and wife Terri, How-

    ard and wife Donna, Don and wife

    Sharilyn; grandsons Kevin and wife

    Tiffany, Aaron and wife Maegan,

    Ray, and Justin; and great-grand-

    children Kennedie and Collin.

    Enroll in an EAA Webinar! Jo in the thousands of people

    who have participated in free EAA

    webinars (web-based seminars).

    All you need is a computer and a

    broadband Internet connection to

    receive live streaming interactive

    multimedia programs at home.

    For instance, on August 10, 2011,

    maintenance expert and EAA Sport

     Aviati on columnist Mike BuschA&P/IA will offer his insight on

    owner-produced parts for cer-

    tificated aircraft, and even if you

    can’t be there to participate live,

    you can always watch the archived

    webinar. You can sign up for up-

    coming webinars at www.EAA.

    org/webinars (you’ll be redirected

    to a page on EAA’s Oshkosh365

    website), and you can also watch

    archived webinars starting from

    that website.

    4  AUGUST 2011

    Hall of Fame

     John Underwood

     Vintage Aircraft Association

    EAA will welcome and honor five new members to its Spor t

    Aviation Hall of Fame on October 29, 2011. All EAA members

    are invited to attend the induction ceremony and dinner that

    evening in the EAA AirVenture Museum. For tickets, please call800-236-1025.

    VAA’s 2011 inductee will be John Underwood of Glendale, Cali-

    fornia. Author of 10 aviation books and numerous ar ticles con-

    cerning aviation history, John has had a lifelong fascination with

    airplanes since his was a little boy of 7. Later, as an aviation tech-

    nical writer and illustrator, he earned a living in the industry, all the

    while amassing a vast collection of photographs and aeronautical

    materials. His work in the center of one of aviation’s most active

    locations, the Los Angeles basin, gave him access to a number of

    aviation luminaries, including Lockheed’s Kelly Johnson, test pilot

    Tony LeVier (with whom John was partners in a Monocoupe), airracing and test pilot Gordon Israel, Alden Brown (designer of the

    Brown racer), and even Douglas “Wrong Way” Corrigan.

    John’s dedication to “getting history right” often sees him lend-

    ing materials and photos to other authors so more people can be

    made aware of exactly what happened when.

    VAA is pleased to include him in its Hall of Fame, honoring his

    contributions to the modern-day efforts to keep the world of vin-

    tage aircraft alive and vibrant through his writings and research.

    Do come join us to honor him at the induction ceremony on Octo-

    ber 29, 2011.

    Bill Turner (left) presents the Cliff Henderson Award (c.1995) to

    John Underwood.

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    VINTAGE AIRPLANE 5

    To nominate someone is easy. It just takes a little time and a little reminiscing on your part.

    Mail nominating materials to: 

    Remember, your “contemporary” may be a candidate; nominate someone today!

    www.VintageAircraft.org 

     

     

       

     

    CALL FOR VINTAGE AIRCRAFT ASSOCIATION

    NominationsCall for VAA Hall of 

    Fame Nominations

    To the left is our informationfor nominations for VAA’s Hall

    of Fame, which is presented each

    year during a special dinner. This

    year’s dinner will be held Friday,

    October 28. We’ll have more on

    this year’s inductee, John Under-

    wood, in a subsequent issue of Vin-

    tage Airplane. If you are interested

    in purchasing tickets to attend the

    dinner to honor the inductees,

    contact EAA’s Matt Miller at 920-

    426-6886 or [email protected] .We would like to take this op-

    portunity to mention that if you

    have nominated someone for the

    VAA Hall of Fame, nominations

    for the honor are kept on file for

    three years, after which the nomi-

    nation must be resubmitted.

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    6  AUGUST 2011

    Making anOld Friend

    Envy of the airport—he flies an Aeronca

    BY SPARKY BARNES SARGENT

    JIM KOEPNICK

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    VINTAGE AIRPLANE 7

    Fr ank J acob and h i s

    Aeronca Champ have

    been buddies for a long

    time—and he just in-

    vested three and a halfyears restoring it to

    make sure they’ll continue their

    friendship for several more de-

    cades. Frank, a soft-spoken gentle-

    man with an amiable smile, flew

    his newly restored Champ from

    Lafayette, Louisiana, to Sun ’n

    Fun, International Fly-In & Expo

    at Lakeland, Florida, in the spring

    of 2010. His Champ and two oth-

    ers composed a friendly flight

    of three, and they enjoyed fineweather all the way to Lakeland.

    He knows N84856 from the in-

    side out, having owned it for 34

    years. “It has gone through a lot in

    its lifetime,” he says with a smile.

    “I found all the old records of

    what all the previous owners did

    to it when I got the file from the

    FAA in Oklahoma City.” Frank has

    also gone through quite a bit in his

    own lifetime, making aviation his

    profession in one way or another.“I flew various airlines that went

    bankrupt, went out of business,

    and all that sort of thing,” he ex-

    “The money isn’t really

    the reason for any of this.

    It’s fun!” —Frank Jacob

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    plains. “I did

    maintenance work for Ozark for

    a year in St. Louis and put in fouryears of maintenance work in the

    Air Force. I got my A&P at Spar-

    tan in Tulsa, and I was going to go

    through the flight engineer course,but the airl ine on the West Coast

    that Spartan had contracted to give

    us the flight training went out of

    business, so I got my multiengine

    instrument instead.”

    Frank first became enamored

    with Aeronca Champion airplanes

    in 1951. “That’s what I did my first

    flying in, and that’s what I soloed,”

    he recalls, with a twinkle in his eye,

    “and I like the airplane!”

    Champion History“So safe—so simple—now any-

    body can fly” boasted Aeronca’s ad-

    vertising of the era, along with the

    declaration that the Champ was

    “America’s No. 1 Low-Cost Plane,”

    and its pilot was the “envy of the

    airport.” The tandem AeroncaChampion trainer was designed

    by Raymond F. Hermes and man-

    ufactured by the Aeronca Aircraft

    Corporation in Middletown, Ohio.

    More than 8,000 were built, andjust like its predecessors all the way

    back through the 1930 Aeronca

    C-2, it incorporated aeronautical

    engineer Jean Roché’s unique trian-

    gular fuselage structure.

    In February 1946, as produc-t ion was about to begin, the

    Champ was advertised as “the easi-

    est plane you’ve ever flown…with

    far greater maneuverability and

    greatly broadened range of visibil-

    ity. …Just wait till you see Aeron-

    ca’s luxuriously finished interior…

    the extra room and comfort…the

    wide safety-swing door! Improved

    brake system and tie-down rings

    that are built in.”

    Features also included 300-degree visibility from the cockpit,a 38 mph landing speed, and stan-

    dard oleo landing gear. So it was

    easy for a pilot to let his gaze roam

    over a pastoral landscape and the

    open sky, thanks to the Champ’s

    low-profile nose, a one-piece Plexi-

    glas windshield, and rather large

    side and rear windows. And with

    its slow landing speed and shock-

    absorbing gear, the Champ could

    alight as softly as a flower petal

    floating to earth. With its 35-foot

    wingspan, and 21-foot 5- inch

    length, the Champ had excellent

    handling characteristics from

    taxi through landing. It offered

    a respectable performance

    among its contemporaries—

    its Continental A-65 pow-

    ered a top speed of 100 mphand a 90 mph cruise while

    sipping from a 13-gallon fuel

    tank for a range of 270 miles.

     N84856Unlike many Champs of the

    day that were used as trainers,

    N84856 went into service as an

    agricultural sprayer for Vanda-

    lia Flying Service Inc. in Van-

    dalia, Illinois. It installed an

    Aero Spray King Model A2 unitand converted the plane from

    a model 7AC to a 7BCM by re-

    moving the Continental A-65-8

    and wood propeller and install-

    ing a C-85-12F with a Hartz-

    ell ground-adjustable propeller.The Champ changed hands several

    times, and its Grade A cotton fab-

    ric was replaced in 1951. Five years

    later, while it was in Oklahoma, the

    Champ was converted back to a

    7AC model. By 1958, it needed newfabric again, and this time, its fuse-

    lage was covered in cotton, and the

    wings and tail were covered with

    Irish linen.

    N84856 continued flying from

    owner to owner through the years,

    experiencing a few mishaps (such

    as ground loops) along the way.

    Then in 1975, Frank Jacob became

    its new caretaker, and N84856 has

    remained in his capable hands

    ever since. An A&P and CFI, Frankexplains with a chuckle that he

    learned to fly “in west Texas where

    the wind blows pretty hard, and

    they say instead of a windsock,

    they use a logging chain. If the log-

    ging chain is standing straight out,

    then it gets to be fun.”

    He had a bit of work to do on

    the Champ when he first purchased

    it—but after all, the airplane only

    cost him only $3,000. “The gear

    had been wiped out from the fuse-

    8  AUGUST 2011

    d

    a

    i

    d

    Aan

    a

    m

    an

    in

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    lage one time, and the doorway was

    cut down to just a hole. I thought

    I was going to put the hinge pinsin place and put the door back on,

    but instead I wound up having to

    take fabric off around the bottom

    to weld a new door frame,” Frank

    recalls, then adds with a smile, “An

    FAA man came up behind me while

    I was welding on the airframe, and

    he thought he’d caught somebody!

    He said, ‘Let me see your A&P li-

    cense,’ and I pulled it ut to show

    him—then he just walked off.”

    Research and Resources

    By 2004, Frank decided, some-

    what apprehensively, to start restor-

    ing his aging friend. He had helped

    other folks with their projects, but

    he hadn’t tackled a full-blown res-

    toration. So the first year, he cau-

    tiously decided to fabricate a new

    cowling. With that accomplished,

    he says, “I kept doing a little more,

    a little more, and finally it was time

    to take the wings off—then I was

    committed! So I got serious about

    it and put in two and a half years

    of work.”

    Myriad questions sprang to

    Frank’s mind as he examined the

    condition of numerous airframe

    components and contemplated

    such things as par t s replace -

    ment, so he sought answers from

    technical, personal, and cyber re-

    sources. “A little bit of research

    can really do a whole lot for you,”

    he shares. “There’s a ton of infor-

    mation on the Internet from the

    various Aeronca flying clubs; Bill

    Pancake [well-known Aeronca

    VINTAGE AIRPLANE 9

    SPARKY BARNES SARGENT

    BRADY LANE

    Frank says his Champ is probably about 90 percent original.

    Frank Jacob

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    10  AUGUST 2011

    “guru”] is super friendly; and

     John Houser, who worked at the

    Aeronca factory, has the drawings

    for the wing spars and fuselage.

     [Editor’s Note: After decades of faith-

    ful service to Aeronca enthusiasts,

     John no longer prov ides th is he lp .

    See the note at the end of this article

    for information regarding sources of

    data for the Aeroncas.—HGF]  I used

    the Poly-Fiber fabric-covering pro-

    cess, and I dealt with Dondi and

     Jim Miller [of Ohio]. They were su-

    per helpful and mixed the original

    Champ colors for me.”

    Frank incorporated a few modi-

    fications to his Champ, by means

    of various STCs. Through his re-

    search, he discovered one from

    Cashmere Aviation Inc. (STC No.

    SA4760NM) that allowed him to

    use Marson Klik-Fast blind rivets to

    attach the wing fabric to the ribs,

    as opposed to using the original

    PK screws. Another handy one was

    from Rainbow Flying Service (STC

    No. SA00860SE), which allowed

    the installation of that company’s

    fuselage formers. Additionally,

    Frank also used two more STCs:

    one for the Champ’s fabric instal-

    lation (Poly-Fiber Aircraft Coatings’

    STC No. SA1008WE), and one sohe could burn autogas in the 65-

    hp Continental (STC No. SA732GL

    [airframe] and STC No. SE634GL

    [engine]).

    Snafus and ChallengesRemember tha t new cowl -

    ing that was the genesis of the

    Champ’s restoration? Well, as it

    turned out, Frank had to rework it

    just a bit. Explaining with a good-

    natured chuckle, he says, “I madethe new cowling first, and later

    on, I installed new rubber engine

    mounts, which lifted the engine

    up about an inch. Then the new

    cowling didn’t fit right! So I had to

    modify it, because the engine was

    in the proper position when I fin-

    ished the airplane.”

    One of the most challenging

    situations Frank encountered was

    installing the leading-edge metal

    around the wing ribs. “That wasbecause I had to get to the [pre-

    drilled] holes in the ribs from in-

    side the wing, in order to align

    them with the placement of holes

    on the leading edge, and that

    metal didn’t want to bend around

    the nose ribs. So I had to hold the

    metal down while reaching inside

    the wing with a pencil and making

    a little mark on the metal. Then I

    took the metal back off and drilled

    one hole. I did that for each hole,all the way across the wing lead-

    ing edge. That took a long time,”

    recounts Frank with a wry smile,

    “and that’s the thing—when I first

    took the airplane apart and looked

    at it, I thought, ‘Boy, this is going

    to take a whole year to do!’”

    Frank endured an odyssey of

    sorts when he ordered the Sitka

    spruce to make new wing spars. He

    says, “My first order was shipped

    in a cardboard box, and they

    The Champ at the beginning of the restoration.

    The refurbished fuselage, replete with stringers and formers.

       C   O   U   R   T   E   S   Y

       F   R   A   N   K

       J   A   C   O   B

       C   O   U   R   T   E   S   Y

       F   R   A   N   K

       J   A   C   O   B

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    VINTAGE AIRPLANE 11

    [the wood] rattled on the back of

    a truck until the cardboard was

    worn through, exposing the wood.

    I took the wood to a professional

    shop, and he ruined the wood,”

    Frank recalls, adding, “so then, I

    bought a second batch of wood

    from the same place, and it came

    and it was worn terribly, so I soldit back to the trucking company.

    Then I bought a third batch from

    a different source (Wicks Aircraft

    Supply), and they shipped it in a

    wood box. That spruce was so per-

    fect; it had exactly 90-degree grain

    instead of 45-degree, and the grain

    was perfectly straight for 16 feet—I

    didn’t think a tree could grow that

    straight! It was the most beautiful

    wood I’ve ever seen in my life, and

    we built the spars out of that.”When it came time to strip

    the airframe tubing down to bare

    metal, he tried using a heavy-

    duty commercial sandblaster at a

    boat yard, but its force was strong

    enough to pepper holes into one

    elevator, which necessitated weld-

    ing repair. Since the fuselage was

    in decent shape, Frank had it

    Sponge-Jet blasted (an environ-

    mentally friendly type of abra-

    sive blasting), and he sandblastedthe smaller parts in his hangar.

    He used two-part epoxy primer to

    protect and preserve the cleaned

    metal components.

    Finishing TouchesFrank wanted to make his Champ

    as original as he could, and overall,

    he thinks it’s “probably about 90

    percent original.” In summary, he

    used all new hardware and cables,

    some new ribs and drag wires fromWag-Aero, new aluminum leading

    edges, and new spars and stringers.

    He also installed new side windows

    and simply reused the windshield,

    since it was still in good shape. In-

    terestingly, the Champ’s original-

    style hubcaps came from the island

    of Guam; one of Frank’s friends

    found them on eBay.

    When he started on the inte-

    rior, he consulted Bill Pancake, who

    helped him identify the correct col-

    New and old ribs are mounted on the new spruce spars.

    The wings, ready for fabric.

    The fabric-covered fuselage and wings, coated with Poly-Brush.

       C   O   U   R   T   E   S   Y

       F   R   A   N   K

       J   A   C   O   B

       C   O   U   R   T   E   S   Y

       F   R   A   N   K

       J   A   C   O   B

       C   O   U   R   T   E   S   Y

       F   R   A   N   K

       J   A   C   O   B

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    12  AUGUST 2011

    ors. The brown paint was locally available, and the co-

    ordinating brown crackle coating on the instrument

    panel was available in a handy spray can from Ken-nedy Manufacturing Company (it makes tool boxes) in

    Van Wert, Ohio.

    Frank purchased the interior flocking kit from DonJer

    Products Corporation in Winnebago, Illinois. The kit, he

    says, consists of “one spray gun with glue and another

    spray gun with powder. You spray the glue on the sur-

    face; then you spray the powder and it sticks to it,” ex-

    plains Frank, adding, “Any excess falls off, and eventually

    it looks like suede. I had everything ready to spray, but I

    had the wrong fitting to plug the spray gun into the air

    hose. So I ran to town and went to all the places I could

    think of, but nobody had the right fitting. It was late inthe day, and I was discouraged, so I just brushed it on the

    cabin wall. So now, if you get the light just right, you can

    see little brush marks. Spraying is the way to go!”

    Engine and MagsBack when Frank started the Champ’s restoration,

    the A-65-8 engine was running so well that he merely

    took it off the airframe, pickled it somewhat and used

    dehydrator plugs, and hung it on the wall for three

    and a half years. At that time, it had a little more than

    1,000 hours since major and 200 since top overhaul.

    With the airframe completed, he reinstalled the engine

    Note the neat upholstery and “flocking” on the

    cabin wall.

       S   P   A   R   K   Y

       B   A   R   N   E   S

       S   A   R   G   E   N   T

       B   R   A   D   Y

       A   N   E

       P   H   O   T   O   S

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    and crossed his fingers. “It started

    after three flips of the prop,” he

    says happily, “and has been run-

    ning good ever since—I’ve flown it

    about 100 hours since June 2008.”

    He spruced up the engine com-partment by painting it and powder

    coated the black rocker box covers.

    Since the Continental has the old

    Bendix magnetos, he’s recently de-

    cided to buy a magneto with an im-

    pulse coupling, to facilitate hand

    propping the engine.

    Flying the ChampFrank describes flying N84856

    by saying, “Generally you want to

    lift off at 50 mph, climb at 60, andcruise at 80. As for landings, if you

    have a nice, calm day, it’s going to

    be all three-point landings, until

    you get used to the airplane,” he

    explains, emphasizing, “Basically

    you want to become part of the air-

    plane—you want to feel it. When

    most people land an airplane that

    has a nose wheel, as soon as they

    touch down they sort of relax and

    the airplane goes straight down the

    runway. But in this airplane, you

    ought to be relaxed until you touch

    down—and then you get serious

    and have to work at it to keep it

    straight. I like to wheel land in a

    strong crosswind, because you have

    a lot more control.”As a flight instructor, he feels that

    simply learning how to correctly taxi

    the tailwheel Champ is a good step

    in transitioning from a nosewheel

    airplane. “If you’re just starting out,

    mainly you want to get used to the heel

    brakes, which are unusual for most

    people. You turn the airplane with

    full rudder, and if that’s not enough,

    then add some brake and then some

    power—you’re just working every-

    thing when you’re taxiing. And youshould always be conscious of where

    the wind is when you’re taxiing, be-

    cause you’re flying it when you’re on

    the ground. You’ve got to feel the air-

    plane to see what it’s doing.”

    An Eye to the FutureFrank is affectionately attached

    to his Aeronca Champion—and

    with good reason; his own personal

    history is inextricably entwined

    with it. “My daughter, Cathy, first

    flew with me when she was 10 years

    old,” he reminisces, with a twinkle

    in his eyes, “and she used a cushion

    so she could reach the rudder ped-

    als. I never thought she would do

    much with flying…and today she’sflying internationally for Delta. My

    son, Don, soloed a few days after

    his 16th birthday but didn’t con-

    tinue with flying. But the kid across

    the street, every time I drive in the

    driveway, he wants to go flying! So

    you can never tell with kids.”

    Father and daughter still occa-

    sionally share the joy of flying to-

    gether in the faithful Champ, and

    Frank proclaims with a smile, “I

    plan to give it to her when I finishwith it. I hope to wear it out before

    then! I tell her I’ll restore it in an-

    other 40 years.”

    So it isn’t surprising that Frank

    won’t consider selling it. With a

    gentle laugh, he shares, “I have put

    $17,000 of parts in it, and all those

    hours that I can’t count. If some-

    body wants to buy it, I say, ‘No way,

    I don’t care how much!’ The money

    isn’t really the reason for any of

    this. It’s fun!”

    VINTAGE AIRPLANE 13

    JIM KOEPNICK

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    14  AUGUST 2011

    Ever wonder why your J-3 Cub,

    identical to your friend’s Cub in

    every way (i.e., engine, prop) just

    doesn’t perform like your friend’s

    Cub? You’ve checked everything,

    including compression, timing, and

    identical Stromberg carbs including

    the same type of fuel, but still your

    Cub is continually outperformed.

    The empty weight for both Cubs isnearly identical, and you and your

    friend are within five pounds of

    one another. Why does your Cub

    seem so sluggish on takeoff, but the

    other Cub just leaps into the air?

    This issue has puzzled Cub own-

    ers for decades, but finally there ap-

    pears to be a cause and solution on

    the horizon. It’s the carburetor!

    I recently had an opportunity to

    sit down with Robert Kachergius,

    Uni-Tech Air Management Systems

    Inc. Bob has an engineering as well

    as aviation maintenance back-

    ground including an A&P and IA,

    and for the past number of years he

    has specialized in the rebuilding of

    Stromberg carburetors.

    For years if not decades most

    aviation mechanics have been frus-

    trated by the Stromberg carbs. If you

    get a good carb, they run beauti-fully. But they often cause mechan-

    ics much frustration and gray hair.

    Consequently, many Strombergs

    have been removed and replaced

    with a Marvel carb. Now, thanks to

    Bob’s research, the cause and solu-

    tion have been found.

    Bob was asked to take a look at

    a Stromberg carb that had been in-

    stalled on a Continental A-65 en-

    gine. The owner stated the engine

    started easily and idled smoothly,

    but when full power was applied,

    the engine just was turning up. The

    normal things had been checked

    but made no difference.

    The carb was carefully disassem-

    bled and all parts checked for wear

    and correct assembly. Everything

    seemed to be in order. The float

    drop was then measured. It should

    measure 0.048 inch in all Strom-bergs. However, this float was only

    dropping about 0.032 to 0.033

    inch and didn’t meet that specifi-

    cation, causing the engine to run

    lean on partial power. Upon closer

    examination it was determined the

    float was coming in contact with

    the main metering jet, restricting

    float drop. In normal operation,

    the float will rest on a castin-posi-

    tion 45-degree bevel at the bottom

    of the float bowl, thus clearing and

    Carburetors

    BY STEVE KROG

    To highlight the special attention that must be paid to even the simplest of mechanical

    items like the reliable Stromberg carburetor, the photos are of the work per formed by BobKachergius of Uni-Tech.

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    VINTAGE AIRPLANE 15

    not hitting the edge of the main

    metering jet. Operating under

    these circumstances the float was

    restricting fuel flow, so the engine

    was only producing about 60 per-

    cent to 65 percent power due to

    restricted fuel flow.

    Bob had a number of the Strom-berg carbs on hand and pulled sev-

    eral of them apart to check float

    travel and drop as well as clearance

    near the main metering jet. Bob fur-

    ther disassembled each of the carbs

    to carefully measure the position,

    angle, and height of the main meter-

    ing jet. Nearly half of the carbs had

    restricted float travel due to contact

    with the main metering jet. It be-

    came quite apparent that a number

    of these carbs had been incorrectly

    Above and below: The three-legged fuel level measuring tool must be used in conjunction with the

    proper amount of fuel feed pressure, or “head,” so the needle and seat will be set properly. Before the

    carb is reassembled, the parting surfaces of the carb are carefully checked for flatness using a granitesurface block.

    For more explanation on the reason for the fuel level sitting at an angle in the float bowl, see

    the photo on page 18.

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    16  AUGUST 2011

    machined during manufacture

    when the main metering jet open-

    ing was drilled into the bottom of

    the carb fuel bowl. There appeared

    to be a large machining variation.

    With that finding it bec ame

    clear as to why one Stromberg

    carb performs as expected, while

    the identical carb runs and per-forms poorly causing the me-

    chanic and owner fits.

    If you’re experiencing lethargic

    performance from your Stromberg-

    equipped airplane, don’t go tearing

    Fuel Drip—WhoGets the Blame?

    By Bob Kachergius

    As we all know, a lot of Strom-

    berg NA-S3 carburetors truly do

    drip when the plane is sitting

    there, not running. It appears that

    the poor little Stromberg is always

    blamed as the culprit in this situa-

    tion. That’s not always the case.

    There are two other factors that

    contribute to the fuel drip, but most

    of the time they are overlooked.

    It could be that the primer or fuel

    selector valve is leaking, causing

    the problem. Two tests can quickly

    and easily solve the puzzle:

    First: Disconnect the small primer

    line from the fitting on the fuel in-

    take spider. Make sure the primer

    is seated in its “park” position on

    the instrument panel and not par-

    tially out. If the primer line continues

    to drip, the primer assembly needs

    service or replacement.

    Second: With the fuel selector

    valve turned to the off position, dis-

    connect the fuel line at the carbure-

    tor. If the fuel line drips, the culprit

    here is a leaky fuel shut-off valve.

    Repair or replace it.

    So, in the end, the poor little

    Stromberg that “drips” may not al-

    ways be the cause of the problem.

    Any time you experience a fuel drip,

    do these two tests. They are fast

    and simple to perform. The tests

    should always be part of a 100-

    hour or annual inspection.

    Completely overhauled and ready for installation after Uni-Tech’s Bob

    Kachergius has given it a thorough going-over. As is typical for most instal-

    lations of the Stromberg with the back-suction mixture control installed, the

    control lever for the mixing disks is either safety wired in the closed posi-

    tion, or, as in this carb, had it removed and replaced with a simple cover

    plate. The yel low dot indicates the carburetor has had its fl oat chamber

    vent hole repositioned per a Stromberg service bulletin.

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    into your Stromberg carb just yet.

    There is a simple check that you can

    do. Remove and inspect the spark

    plugs. If the probe ends are a nice

    even chocolate brown, your carb is

    probably performing as was intended.

    However, if your plug ceramic insula-

    tors are white to light gray in color,

    you are running a lean mixture thatis probably caused by this float/fuel-

    flow restriction. In this case you may

    want to have your carb thoroughly

    inspected and corrected.

    Bob has developed a “fix” for

    those carbs experiencing float

    travel restrictions. He has devel-

    oped machining so that the main

    metering jet orifice can be counter-

    bored slightly, thus allowing full

    float drop and proper fuel flow.

    When done properly and legally,

    VINTAGE AIRPLANE 17

    Stromberg NA-S3 Carburetor—Helpful Hints

    By Bob Kachergius

    They say in life there are two ways to get a job done—doing it the

    easy way or the hard way.

    When removing and then re-installing a Stromberg carburetor on a

    small Continental engine, because of the lack of room, it becomes an

    act of frustration in trying to get the castellated nuts and cotter pins

    started on the intake spider studs. Doing this while the intake spider is

    mounted to the engine becomes, at best, very time-consuming. That’s

    the hard way.

    Try this instead:

    Remove the intake spider from the engine (two AN6 nuts and wash-

    ers, four rubber intake tubes and clamps, one primer line connection)

    and then easily re-install the carburetor to the intake spider while it’s

    on the workbench; it’s fast and simple. This is the easy way.

    You will find, in most cases, that the rubber intake tube sleeves are

    pretty old, dry, and cracked and in need of replacement anyway.

    Stromberg Carb Information Chart

    CARB MODEL ENGINE MFR ENGINE MFR ENGINE MODEL HORSEPOWER FUEL FEEDSETTING NUMBER

    NA-S3A1 series carburetors with mixture controlA18033B CONT 3628 A-65 65 GRAVITY

      A-75 75 GRAVITY

      A-80 80 GRAVITY

    A30177 CONT 4631 A-75 (Stinson) 75 GRAVITY  50” HEAD380162 CONT 40059 C-75 75 GRAVITY380167 CONT 40590 C-85 85 GRAVITY

    380171 CONT 36019 C-75 75 PRESSURE

    380172 CONT 40636 C-85 85 PRESSURE

    380174 CONT 24716 C-75-12 75 GRAVITY

    380231-3 CONT ------ C-9012F 90 GRAVITY

    380231 CONT ------ C-90 90 PRESSURE

    391090 CONT ------ C-90 90 GRAVITY

    391156 CONT ------ C-90 90 GRAVITY

    391229-1-2 CONT ------ C-90-14F 90 GRAVITY

    391257 CONT 531157 C-90-14F 90 GRAVITY

    391716-1 CONT ------ A-50 50 PRESSURE  “ “ “ A-65 65 3 PSI /

      “ “ “ A-75 75 .048” FLOAT

      “ “ “ A-80 80 DROP

    392458 CONT 4805 A-80 80 GRAVITY

    NA-SO3A1 (rarely seen )380168 CONT 50335 A-100 100 GRAVITY

    380175 CONT 36020 A-100 100 PRESSURE

    NA-S3B (no mixture control)380155 CONT 35885 A-50 50 GRAVITY

      “ “ “ A-65 65 “

    380205 CONT 36109 A-65 65 PRESSURE

      “ “ “ A-75 75 “380206 CONT 36109 A-65-8 65 PRESSURE

    This chart details the proper engine/application with the model number stamped on the carb body.

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    18  AUGUST 2011

    the float restriction is no longer a

    problem and the carb can be re-

    turned to service.

    Bob also does several other things

    to a Stromberg to get it to run prop-

    erly. He finds that in all the carbshe gets in for overhaul, almost ev-

    ery one has the old neoprene needle

    and seat. These needles were the sec-

    ond generation from Stromberg and

    were designed to eliminate the fuel

    drip common to Strombergs. These

    needles came out in 1943 after the

    war, and some can approach 60-plus

    years in age. They get very brittle

    and will crumble when squeezed

    with a long nose pliers. It is also

    common knowledge that when us-

    ing auto fuel containing ethanol,

    many of these needles can swell up

    and cause real fuel flow problems.

    There were three other manufactur-

    ers of the neoprene needles along

    with Stromberg, and it is impossibleto differentiate as to who made the

    needle. The three clone needles were

    made of an inferior-grade neoprene

    and did swell up. The OEM Strom-

    berg needle did not. Thus, at over-

    haul, Bob will use the latest stainless

    steel or Delrin needle and seat, elim-

    inating the neoprene headache.

    Another interesting find is that

    when dismantling the carbs for

    overhaul, Bob finds that whoever

    worked on the carb in the past had

    grossly overtorqued the six 1/4-

    20 fillistered head screws holding

    the upper casting half to the lower

    one. The normal torque specified

    in the Stromberg overhaul is only

    35-45 inch-pounds. This puts ex-cessive stress on the casting and

    warps them, causing possible vac-

    uum and fuel leaks. Bob has to

    custom lap each casting parting

    surface on a granite lapping plate

    to get perfectly flat mating surfaces,

    guaranteeing a positive seal. This

    procedure is done on every carb he

    overhauls.

    Another situation exists contrib-

    uting to fuel drip. The Stromberg

    was originally designed for the Er-

    The steel needle and its corresponding sharp-edged

    brass seat.

    An original and aftermarket set of neoprene-tipped

    needles, illustrating the brittleness that occurs as the

    needles age.

    The Delrin needle used in many Stromberg carbs

    seems to offer the best of both worlds.

    Here is a 12-degree wedge plate Bob uses to show how

    the fuel level sits in a taildragger after the float level was

    set to 13/32 inches wet in the bench. It shows how the

    fuel sits at an angle in the bowl, and, even when the

    float level is proper at 13/32 inches level, the rear of the

    main gasket can get “wet” and seep a little fuel at the

    casting parting line, causing a blue stain. This is why Bob

    always turns the fuel selector off after every shutdown.

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    coupes, which sat on tricycle gear and level to the

    ground. Now, install the Stromberg on a taildragger,

    and it no longer sits level, causing fuel to drip out

    of the carb float bowl vent opening. This vent port

    is located in the lower casting about 1/4 inch be-low the parting surface. Stromberg came out with a

    service bulletin to effect a fix. This involves sealing

    the lower casting port opening and relocating the

    port to the upper casting half, approximately 1/4

    inch above the parting surface. This raises the float

    bowl vent 1/2 inch higher than original and elimi-

    nated float bowl drip. Bob makes this modification

    on every carb he overhauls. The easy way to see if

    this mod was done to your carb is to look and see

    if there is a 1-inch-diameter yellow dot painted on

    the face of the float bowl as recommended by the

    Stromberg service bulletin. If this mod isn’t done,your carb will drip. Bob has found that on almost

    every carb that comes in for overhaul, none have

    this modification installed.

    Another situation occurs when someone in the

    field attempts to set the float level of 13/32 inch

    (all Stromberg carbs) below the lower casting part-

    ing surface and doesn’t dry mechanically. This is

    impossible to do accurately. The float level has to

    be set “wet” with fuel fed to the float bowl with the

    recommended gravity flow pressure head. This has to

    be done on a flow fixture device to be accurate. Fuel

    float level is done by randomly stacking variable-thickness special gaskets under the brass needle seat

    to attain the proper level.

    The Stromberg carburetor is an excellent unit and

    will perform flawlessly if inspected, overhauled, and

    maintained properly. Bob’s diligence in really figur-

    ing out the manufacturing variances in the original

    parts is to be commended. His company, Uni-Tech

    Air Management Systems, located at 13221 Wind-

    ward Trail in Orland Park, Illinois, specializes in

    overhauling only  the Stromberg carburetor. Bob can

    be reached at 708-267-7111 to answer any questions

    you may have on your Stromberg.VINTAGE AIRPLANE 19

    THE “STROMBERG SPECIALIST”

    R.E. “Bob” Kachergius A&P/IA

    UNI-TECH AIR MANAGEMENT SYSTEMS, INC.

    Call: 708-267-7111 Mail: 13221 WINDWARD TRAIL 

    ORLAND PARK, IL. 60462 E-Mail: [email protected] 

     Does your Stromberg NA-S3 carburetor Drip - Leak - Perform poorly ? ? ?

    Have it Overhauled & Restored to “Grand Cham-

     pion” standards and quality by us…

    WE: Dismantle & Inspect –

    Clean & Glass Bead Blast –Aluma-Etch & Alodine –

    Custom Lap mating

    surfaces – Re-

    assemble using all

    new AN hardware,

    gaskets, Stainlesssteel or Delrin needle

    & seat – proper metering

     jets & venturis… Float level

    is set “wet” to 13/32” – Stromberg service letter

     procedure installed to raise float bowl vent position

    eliminating fuel drip – prepare a log book entry

    sheet… 

     All for $850.00+ $25.00 freight & handling

    Before re-assembling the Stromberg carb, the cast-

    ings are carefully inspected and finished, with the

    mating surfaces trued up on a granite surface plate.

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    20  AUGUST 2011

      Light Plane Heritage

    published in EAA Experimenter October 1991

    Editor’s Note: The Light Plane Heritage series in EAA’s Experimenter  magazine often touched on aircraft and concepts

    related to vintage aircraft and their history. Since many of our members have not had the opportunity to read this se-

    ries, we plan on publishing those LPH articles that would be of interest to VAA members. Enjoy!—HGF

    THE UNIQUE LONGHEAD S-1BY BOB WHITTIEREAA 1235

    In the autumn of 1918 the feel-

    ing became widespread that the

    long and bloody conflict we called

    World War I was at last moving to-

    ward its end. This prompted lively

    discussions to take place in a mod-

    est aircraft manufacturing shop lo-

    cated in the California seaside town

    of Santa Barbara.“What are we going to do after

    the war?” was the gist of the talk

    that went on between the brothers

    Allan and Malcolm Loughead and

    their associates John Northrop and

    Anthony Stadlman. They finally

    agreed that they should turn their

    quite impressive mechanical and

    engineering talents to developing a

    small sportplane that would appeal

    to the thousands of men who had

    learned to fly during the war.

    Before getting into the story of

    the Loughead S-1 (for Sportplane

    No. 1), let’s say something about

    the two Lougheads. The name, bythe way, was and is pronounced

    “Lockheed.” They came from a fam-

    ily of Scottish origin and were born

    in the late 1880s. They had an older

    half-brother, Victor, from their fa-

    ther’s previous marriage. He had

    formal training in engineering and

    as early as 1909 was writing books

    on aviation and aircraft design.

    The two younger Lougheads be-

    came expert automobile mechan-

    ics during the first decade of the

    20th century. Then living in San

    Francisco, the three spent much

    time discussing aviation. This led

    Allan in 1910 to move to Chicago,which at that time was a beehive

    of aeronautical activity. There he

    became a good aircraft mechanic

    and taught himself to fly by acci-

    dent. That is to say, an airplane he

    was taxi testing picked up enough

    speed to become airborne, oblig-

    The young lady gives an idea of the

    Loughead S-1’s dimensions as it sits on

    display in front of the San Francisco CityHall in 1920.

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    VINTAGE AIRPLANE 21

    ing him to “fly” it as best he could

    in an erratically circular path so as

    to return to the field from which

    he had departed. Since the landing

    injured neither the plane nor him-

    self, that made him into a pilot by

    the standards of that time.

    Early in 1912, Allan returned

    to San Francisco and persuadedbrother Malcolm to join him in

    building an airplane. Malcolm

    had remained in Cal i fornia ,

    where he worked as an accom-

    plished auto mechanic and de-

    veloped what became the widely

    used Lockheed hydraulic brakes

    for cars. Between 1912 and 1916

    the two divided their time among

    assorted aviation projects and

    prospecting for gold. In 1916 they

    relocated to Santa Barbara, wherethey set up a modest aeronautical

    shop in a garage.

    Here they built a small number

    of flying boats. The aforementioned

     John Northrop and Tony Stadlman

    had also been active in the heady

    early days of aviation and during

    the war joined the Loughead shop

    to help build a small number of na-

    val flying boats. Between them the

    four possessed very considerable

    practical and engineering knowl-edge. As mentioned previously,

    they began to brainstorm their

    ideas for a postwar civil airplane.

    Now, in the year 1918 nobody

    foresaw clearly the enormous impact

    that thousands of war-surplus mili-

    tary planes would have on the post-

    war civil aviation scene. Not realizing

    that the aircraft manufacturing in-

    dustry would be severely depressed

    for several years by this vast supply of

    cheap surplus airplanes and engines,the quartet enthusiastically drew up

    a list of desirable characteristics for

    their new plane.

    Of course, there were often

    strong differences of opinion while

    all this talk was going on, but in the

    end they agreed on what it should

    be like. It would be a single-seater,

    partly so that a small and therefore

    economical engine could fly it satis-

    factorily, but in retrospect probably

    also because they felt that the typi-

    cal returning military pilot would

    be one who was accustomed to fly-

    ing a fast and nimble single-seater

    or at least being in total command

    of a two-seater.

    Airplane fuselages of that time were

    tediously put together from wooden

    longerons and cross-members

    held together with a great many

    intricate metal fittings, braced

    against bending and twisting with

    many crisscrossing steel cablesand trued up by expertly adjust-

    ing a multitude of turnbuckles.

    All of this was much too labor-

    intensive for a plane meant to be

    sold to civilians at the lowest fea-

    sible price. For this reason they

    developed a more suitable form

    of construction, which will be de-

    scribed shortly.

    They also decided that their

    plane should perform well enough

    to have a reasonable chance of sat-isfying pilots accustomed to flying

    lively military planes, within the

    limitations set by an economical

    selling price. Yet at the same time,

    because real airports with good

    runway and hangar facilities were

    at that time still very few in num-

    ber and far apart, they agreed that

    their plane would have to be able

    to take off from and land on what-

    ever modest-sized clearing owners

    might be able to find.

    Because the g lues and var -

    nishes available in those long-ago

    days were rather lacking in water-

    resistance, the new plane would

    have to be designed so that its wing

    folded for towing behind a car to a

    garage or barn for storage.

    While some European war-

    planes such as the German Fokkers

    had fuselages put together com-

    paratively quickly by welding steel

    tubing of suitable length and di-ameters, the technique of building

    this way was not very well under-

    stood in the United States. Also,

    expert oxyacetylene welders were

    scarce in California.

    Much thought and experimen-

    tation went into the method set-

    tled upon for building the fuselage.

    They knew of other airplanes that

    had wooden fuselages of the mono-

    coque-type construction. That

    word is of French origin and is pro-nounced monoKOK. It means es-

    sentially “a stiffened sheet of metal,

    veneer, plastic, etc. to bear loads.”

    Various other fuselages of this

    type had been built using tech-

    niques familiar to builders of light-

    weight boats. Typically strips of

    veneer would be laid onto a suit-

    able building form made of bulk-

    heads and stringers. One of the

    problems was to end up with an

    acceptable smooth, sound, and

    Obviously the result of a lot of pattern work and concrete mixing, the fuse-

    lage molds for the S-1 were solid and durable. While books on the Lockheeds

    claim birch plywood was used for lamination, material visible to the right looks

    more like some kind of veneer.

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    22  AUGUST 2011

    strong laminate using whatever a

    builder chose in the way of tacks,

    staples, and glues. Sometimes lam-

    inations sprung apart before the

    glue set adequately.

    They were not, by the way, the

    only ones looking for an alterna-tive to the wood-and-wire type

    of construction. While they were

    building their S-1 in early 1919,

    the Curtiss company on Long Is-

    land in far-away New York built

    a number of Curtiss Oriole three-

    seater biplanes that had fuselages

    made with Curtiss’ version of the

    laminating process. The fuselage of

    an Oriole can be seen and studied

    today at the Glenn H. Curtiss Mu-

    seum at Hammondsport in centralNew York.

    The Lougheads came up with

    the idea of using large concrete

    molds in which to laminate right

    and left shells from which to as-

    semble a complete fuselage. While

    very heavy, concrete was inexpen-

    sive and admirably rigid. The glue

    most generally used for aircraft

    construction in those days was

    of the casein type, made of dehy-

    drated milk curds ground into a

    powder and then mixed with wa-

    ter for use. Commercial glues of

    this kind usually had additives in

    them to impart desirable charac-

    teristics. While water-resistant for

    periods of time reckoned in terms

    of a few days immersion, it wasnot truly waterproof.

    Information in available litera-

    ture is vague and confusing, but

    it appears the Loughead team

    gradually devised a method of

    preparing materials and position-

    ing them in the concrete molds.

    Three layers of very thin spruce

    plywood were laid up, and one

    old book claims that layers of thin

    cloth were spread between them

    to serve as binding membranes.When the laminating materi-

    als were in position in the mold,

    a rubber bag was laid in place and

    the mold capped with a bolted-

    on cover. Air pressure then forced

    the rubber against what would be

    the inner surface of the finished

    molding. This applied necessary

    pressure to assure proper bond-

    ing of the glue, absence of voids,

    and a smooth outer surface. When

    the glue had cured, right- and left-

    hand moldings were joined to-

    gether with longitudinal bonding

    strips to form a light, strong fu-

    selage. The finished laminate was

    1/8 inch thick.

    The structure and shape of the

    tail surfaces were made to fit onthe torpedo-like tail end of the fu-

    selage. This characteristic look ap-

    peared some years later on the

    Lockheed Vega, Sirius, Orion, and

    Altair designs.

    The Santa Barbara experiment-

    ers originally intended to use an

    English Green engine on their new

    design, but had to give up this idea

    when the manufacturer went out

    of business. So expert mechanic

    Stadlman designed a two-cylinder,horizontally opposed engine that

    he and Allan built in their shop.

    At that time designers and found-

    ries were much more familiar with

    the technique of casting deep,

    closely spaced air-cooling fins. So

    this new engine was water-cooled.

    A radiator of crescent shape was

    made to fit neatly under the fu-

    selage below the firewall. The en-

    gine developed 25 hp.

    To get acceptable takeoff and

    This view of the S-1 in flight suggests that the German Albatros of World War I could have been the inspiration for its

    overall shape.

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    VINTAGE AIRPLANE 23

    climb performance from this en-

    gine, the plane’s wings were given

    the ample span of 28 feet for the

    upper one and 24 feet for the lower

    one. While at first sight appearingto be a biplane, the S-1 was actu-

    ally a sesquiplane. “Sesqui-” means

    “one-and-a-half,” and so this now

    seldom-encountered aviation term

    refers to a two-winged aircraft in

    which the area of one wing (in this

    case the lower) is one-half or less of

    the other.

    The top wing was of conven-

    tional two-spar, fabric-covered

    wooden construction and had no

    ailerons to simplify manufactur-ing of the ribs. The wingtips were

    of very pleasing and efficient semi-

    elliptical shape. Lower wings were

    of single-spar construction. V-

    shaped interplane struts connected

    the two spars of the upper wing

    panels to the single spars of the

    lower ones. This layout originated

    in the famous French World War I

    Nieuport fighters as a result of de-

    signer Edouard Nieuport’s strong

    feeling that the number of wing

    A Hint From Boat BuildersMonocoque construction has been little used in homebuilt aircraft or re-

    storers, but offers possibilities for experimenters having a working knowl-

    edge of stress analysis and weight control. For example, using certain

    modern techniques, a fuselage could be made without the need for an

    expensive mold, and the method could be adapted to such things as tail

    booms, seaplane floats, and flying boat hulls.

    Epoxy resins that develop full strength without the need for great clamping

    pressure are now available. They are used in a method of amateur and cus-

    tom boatbuilding called cold molding, from the fact that these resins cure atroom temperatures. A study of this boat-building technique could be produc-

    tive. But a word of caution—poorly chosen lamination schedules can result

    in unacceptably heavy or costly aircraft components.

    In copies of WoodenBoat  magazine, you’ll find advertisements of epoxy

    suppliers such as Chem Tech and Gougeon Brothers and get prices for their

    how-to literature and trial samples. WoodenBoat  has a catalog that among

    other things lists books on lightweight wooden boat construction. Their ad-

    dress is Box 78, Brooklin, ME 04616. Write to Forest Products Laboratory,

    One Gifford Pinchota Drive, Madison, WI 53705 and request copies of “List

    of Publications on Veneer and Plywood” and “Glass and Glue Products – List

    of Publications.”

    Veneer used for cold-molded boat hulls is about one-eighth inch in thick-ness and produces laminates too thick and heavy for aircraft. Being an ex-

    pensive manufactured product, there’s a question if it’s economical to buy

    thin plywood and slice it into strips for lamination work. When homemade ve-

    neer is produced by running planks through a table saw, much of the raw ma-

    terial one has purchased is turned into wor thless sawdust. Veneer is made

    by special machines in which very large blades slice wood from logs without

    producing sawdust.

    Builders of fiberglass boats use a wide variety of special foam plastic and

    balsa wood core materials that add thickness and rigidity to laminates. A

    successful epoxy-based monocoque aircraft structure would be the result of

    careful study of the many special materials and techniques available today.

    The S-1’s wing assembly was really

    unique. Lower wings pivoted to act

    as ailerons, and tipped on edge to

    clear the fuselage when the wings

    were folded for towing and storage.

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    24  AUGUST 2011

    struts and brace wires should be

    kept to a minimum for the sake of

    minimizing wind-resistance while

    retaining the strength and rigiditycreated by trussing biplane wings

    together with a system of struts and

    crisscrossed wires. The Germans

    imitated this approach in their Al-

    batros fighters, and we can see a re-

    semblance to the Albatros’ lines in

    those of the Loughead S-1.

    The S-1’s lower wings also had

    no ailerons. Because each had but a

    single spar, it was feasible to make

    fittings that attached them to the

    fuselage in such a way as to al-

    low these wings to pivot about the

    spanwise centerlines of their spars.

    The control system was designed to

    make the lower wings move exactlyas do conventional ailerons. In ef-

    fect, the smallish lower wings were

    the plane’s ailerons.

    The control system incorporated

    another feature. By pulling a lever

    just after touching down on a land-

    ing, the pilot could cause the lower

    wings to rotate 90 degrees, with

    leading edges poi nting straight

    down and trailing edges straight

    up. This presented the lower wings’

    full surface broadside to the air and

    provided dramatic braking effect.

    The cleverness of the wing struc-

    ture’s overall design is further il-

    lustrated by the fact that wing rootfittings also allowed right- and left-

    hand assemblies to be folded back-

    ward (on the ground, of course!) to

    make the ship narrow enough to

    be towed tail-first behind a car over

    the road from landing field to stor-

    age building.

    Extensive test flying was carried

    out during 1919, and the plane at-

    tracted much favorable attention

    when exhibited and demonstrated

    at the 1920 San Francisco Aeronau-

    Two workmen easily hold the partly completed fuselage of the S-1. In the original 8-by-10-inch photo, strips of veneer

    of verifying widths could clearly be seen running in a straight fore and aft direction.

    It’s a widely acknowledged truth that each new airplane design is based at

    least in part on lessons learned from previous aircraft. In 1927 the Lock-

    heeds (having changed the spelling of their family name) based the fuselage

    of their Vega on the construction method used for the 1919 Loughead S-1,

    combined with Anthony Fokker’s method of making wooden cantilever wings.

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    VINTAGE AIRPLANE 25

    tical Exposition. Empty weight was

    only 375 pounds, all the more im-

    pressive when we remember that it

    was fitted with a water-cooled en-

    gine with its radiator and coolant

    weights. Weight fully loaded was

    an equally impressive 600 pounds.

    Top speed was 70 mph; landing

    speed a very useful 25 mph. Rate ofclimb was 700 fpm, which is very

    good for the power available.

    This interesting plane was a tech-

    nical and operational success, but

    a commercial disappointment. Af-

    ter investing $29,000 in healthy

    1919 dollars in its development,

    the Lougheads were very disap-

    pointed when not a single order

    came in. They went out of busi-

    ness in 1921, engaged in a variety

    of other enterprises, and becausepeople persistently mispronounced

    their name in such ways as “Log-

    head,” changed the spelling to the

    phonetic Lockheed. Theirs was but

    one of the many firms that suf-

    fered from the flood of cheap, war-

    surplus airplanes.

    As the 1920s wore on, new and

    vastly improved aircraft engines ap-

    peared on the scene. Notable was

    the very reliable Wright Whirl-

    wind nine-cylinder radial engineof 200 to 220 hp, which powered

    the planes of Adm. Byrd, Charles A.

    Lindbergh, Clarence Chamberlin,

    and others. Designers began to re-

    alize that the drag of biplane wings

    handicapped these better engines

    and turned to monoplanes. Most

    monoplanes of the late 1920s were

    strut-braced.

    Despite their setback, the Lock-

    heeds maintained their interest in

    aviation and in 1927 came up withsomething really good. By combin-

    ing Anthony Fokker’s method of

    building low-drag cantilever wings

    of wood with their method of mak-

    ing the S-1’s fuselage, they came up

    with the very sleek and fast Lock-

    heed Vega. In the hands of intrepid

    pilots like the Wilkins-Eielson

    team, Wiley Post, and Amelia Ear-

    hart, it made many daring and dif-

    ficult flights.

    Developed from the high-wing

    Vega, the low-wing Sirius led tothe retractable-gear Orion and Al-

    tair low-wings that introduced

    high speed and reliability to airline

    scheduling. Lessons learned while

    building stressed-skin Lockheeds of

    wood taught lessons to designers

    like John Northrop that stood them

    in good stead when in the early

    1930s they began to design all-

    aluminum aircraft of monocoque

    fuselage and cantilever wing design.

    So despite its lack of commercial

    success, the innovative LougheadS-1 contributed greatly to aeronau-

    tical progress. It even passes along

    two important lessons to those

    who are working with amateur-

    built aircraft today. One is that

    there is always more than one way

    to do something, and the other is

    that when well-informed experi-

    menters start brainstorming, no

    one can predict to what surpris-

    ing developments their efforts will

    eventually lead!

    This set of general-arrangement drawings, done by Patricia and Monty Groves,

    originally accompanied an article by them concerning the history of the S-1,

    and the building of a scale R/C model. It appeared in the October 1972 issue

    of American Aircraft Modeler .

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    26  AUGUST 2011

    One of the first designs, whichproved successful in dealing

    with the problem of engine drag,

    was the Townend ring cowl. De-

    signed by British engineer B.

    Melvill Jones, this cowling was

    intended to reduce cooling drag

    but did little for improved cool-

    ing, thus it was strictly for in-

    creased airspeed.

    I l l u s t r a t i o n 1 s h o w s t h e

    Townend ring cowl (also called a

    speed ring), when installed prop-erly, reduced drag by as much

    as 11 percent. However, the

    Townend ring impeded visibil-

    ity while taxiing on the ground.

    Engineers and researchers be-

    gan to explore improved designs

    that would address the issues of

    drag and visibility. In 1928, Fred

    Weick (pronounced Wyck), an

    engineer from the National Advi-

    sory Committee for Aeronautics,

    led the development of what wasto become known as the NACA

    low-drag engine cowling. Weick

    had access to the NACA Propeller

    Research Wind Tunnel at Lang-

    ley, Virginia. Weick and his team

    won the 1929 Collier Trophy,

    the first of five Collier awards

    for NACA. One of the four Col-

    lier trophies received by NASA’s

    Langley Research Center, Hamp-

    ton, Virginia, was in 1929 for the

    development of the cowling for

    radial air-cooled engines. By theend of September 1928, tests of

    Cowling No. 10 in the Propeller

    Research Wind Tunnel, shown

    here, demonstrated a dramatic re-

    duction in drag.

    Illustration 1

    Weick (Illustration 2) authored

    a number of technical papers for

    NACA regarding his research on

    engine cowlings, both full-pres-

    sure cowlings and speed r ings.

    Weick was also interested in de-signing a safe aircraft, one that

    would not stall or spin. His de-

    sign was wind tunnel tested in

    the Langley facility, and a full-

    size aircraft was constructed and

    flown as a proof-of-concept ve-

    hicle, but it never went into pro-

    duction. Weick and his staff made

    numerous wind tunnel tests of

    various configurations and instal-

    lations of engine cowlings. All

    showed a tendency to reduce par-

    asite drag by smoothing out theairflow around cylinder heads,

    but there was a penalty in engine

    operating temperature. As the

    team continued the experiments,

    it became apparent that some-

    thing other than the cowling

    was needed. Intercylinder baffles

    directed the air more efficiently

    around cyl inder barre l s and

    heads for better cooling. For the

    speed ring or Townend cowl, it

    was the angle to which the cowl-ing mounted to the engine cylin-

    ders. The following charts show

    Weick’s experiments on cowling

    configuration. Weick was head of

    the Propeller Research Wind Tun-

    nel section from 1925-1929.

    Illustration 2

    BY ROBERT G. LOCK

    Engine cowls for drag reductionPart I

    THE VintageMechanic

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    28  AUGUST 2011

    Illustration 3 depicts experiments with a wide

    and narrow speed ring configuration shown with

    mounting locations forward and aft on the cylin-

    der heads. The location of the speed ring would

    give varying drag decreases and would also affect

    engine cooling. Early experiments were carried out

    using a Wright J-5 radial engine, but were expanded

    to other radial engines of the time. Oscar W. Schey

    and Ernest J ohnson authored NAC A Technical

    Notes No. 334, and Melvin Gough authored No.

    335 dated February 1930.

    Illustration 3

    Illustration 4 shows NACA Technical Note No.

    355 authored by Melvin N. Gough and detailing

    the tilting of a speed ring +6 to -20 degrees to the

    longitudinal axis of the aircraft. These experiments

    were carried out on Curtiss SF7C-1 aircraft.

    Illustration 4

    Illustration 5 shows a photograph of experimen-

    tal military aircraft used for flight testing and vali-

    dating the NACA speed ring engine cowlings. Not

    only was drag measured but also engine cooling.

    Early cowling experiments tended to reduce drag

    but increase the engine-operating temperature, es-

    pecially the oil temperature.

    The full-pressure NACA cowl installed on a Cur-

    tiss AT-5 aircraft, ready for another test flight in the

    early 1930s, is shown in Illustration 5. The develop-

    ment of this speed ring was a major breakthroughfor all World War II aircraft.

    Illustration 5

    On a test flight, the NACA speed cowl or Townend

    cowl can readily be seen in these NASA photo-

    graphs. The aircraft is a Curtiss P-3 Hawk with a

    Townend ring cowl.

    Early cowling

    experiments tended to

    reduce drag

    but increase the

    engine-operating

    temperature, especially

    the oil temperature.

    NASA

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    Illustration 6

    Curtiss P-3 Hawk with Townend

    ring cowling.

    Illustration 7

    Curtiss P-3 Hawk with NACA

    cowling.

    Engine cowlings became a method

    to increase performance of an air-

    craft, both in speed and range. This

    invention was to have a profound

    effect on future aircraft.

    VINTAGE AIRPLANE 29

    As the team

    continued the

    experiments, it

    became

    apparent that

    something

    other thanthe cowling

    was needed.

    L a n g l ey may have been the

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    1903: Samuel Pierpont Langley’s “Aerodrome”attempts to take off from a floating platform.

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    What Our Members

    Are RestoringAre you nearing

    completion of arestoration? Or isit done and you’rebusy f l y ing andshowing it off? Ifso, we’d l ike tohea r f r om you .Send us a 4-by-6-inch print from a

    commercial source(no home printers,please—those prints just don’t scan well) or a 4-by-6-inch, 300-dpi digital photo. A JPG from your 2.5-megapixel (or higher) digitalcamera is fine. You can burn photos to a CD, or if you’re on ahigh-speed Internet connection, you can e-mail them along witha text-only or Word document describing your airplane. (If youre-mail program asks if you’d like to make the photos smaller, sayno.) For more tips on creating photos we can publish, visit VAA’swebsite at www.vintageaircraft.org . Check the News page for ahyperlink to Want To Send Us A Photograph?

    For more information, you can also e-mail us at [email protected]  or call us

    at 920-426-4825.

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    30  AUGUST 2011

    In the last issue of Vintage Airplane magazine I offered

    a brief overview of “Rock,” a local general-aviation,

    pleasure-flying pilot in need of a flight review. Much

    of the article was told in a “tongue in cheek” manner,

    but it was more real than fiction. This article will dealwith a flight review and some of the considerations I

    like to use when conducting a review.

    The requirements of a flight

    review consist of one hour

    (minimum) of flight training

    and one hour (minimum) of

    ground training. It should

    include:

    • A review of the current

    general operating and flight

    rules of Part 91, and

    • A review of those maneuversand procedures that, at the

    discretion of the person giving

    the review, are necessary for the

    pilot to demonstrate the safe

    exercise of the privileges of the

    pilot certificate.

    There Is No “Pass or Fail”

    The flight review should

    not be viewed as a necessary

    evil. Rather, approach it as a

    means of making you a better,safer pilot. If should be fun

    and, yes, even challenging,

    depending upon how much

    flying you do annually. It is not  a pass-or-fail test!

    This is what I like to do when I conduct a flight

    review.

    Review the aircraft paperwork. This gives me an

    opportunity to ensure the airplane is legal to fly and

    point out discrepancies, if found. Does the airplane

    have a current weight and balance sheet? If so, is it kept

    in the airplane as it should be? Or is it with the logbooks

    and other paperwork? If it is not in the airplane with

    the airworthiness certificate and registration, I’ll make

    several copies of the sheet for the individual, making

    sure one is installed in the plane and the other copies

    kept safely with the logbooks. This exercise helps pilots

    make or keep their airplane legal should they everexperience a ramp check.

    If the airworthiness certificate is tattered and torn?

    I’ll usually make several copies

    of it and suggest that the extra

    copies be safely kept with the

    logbooks. If the airworthiness

    certificate is lost someday, or if

    it blows out of the airplane (I’ve

    had this happen), it’s quite easy

    to get a replacement from the

    local flight standards district

    office if you can produce a copyof the old certificate.

    N o w t h a t t h e F A A h a s

    converted to the new registration

    system, I find it a good idea to

    look at the registration and

    remind the pilot of when he

    or she can expect to receive a

    new registration notice from

    the FAA. (You would be amazed

    at how many individuals

    are confused by this new

    registration system.)I ’ l l n e x t r e v i e w t h e

    individual’s logbook, discussing

    the type of flying as well as how

    much flying the pilot has done in the past two years.

    Is it local flying never beyond 50 miles from home?

    Or is it one or two cross-country flights annually? This

    information will help me decide what to cover when it

    comes time to fly.

    I then like to discuss the new style of NOAA sectional

    charts, pointing out various changes that have been

    made both in color usage as well as chart symbols.

    If you haven’t recently looked at one, you will be

    BY Steve Krog, CFI

    THE VintageInstructor

    Flight reviews make  them funPart II

    Most pilots with

    whom I’ve worked

    with on a flight

    review will be

    quite candid and

    want to talk

    about things in

    which they may

    feel weak.

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