Taylorcraft 20 Ranchwagon / Zephyr 400

The Taylorcraft 20 Ranch Wagon, later dubbed the Zephyr 400, covered with Fiberglas that was intended to be the best seller. The use of Fiberglas shells over the steel fuselage was considered a technological breakthrough, and Taylorcraft dubbed it “The bulletproof vest with wings.” In all, there was nearly 40 Model 20s made.

Each one was made on demand, and therefore, each was slightly different. Some of those differences would appear around the windows or doors or other nonstructural areas, former Taylorcraft engineer Jack Gilberti said. A fourth door was optional with the 15A and 20.

The model 20 was based on the 15A, but was different in three ways: It had a 225-horsepower Continental O-470 engine and the maximum gross weight jumped from 2,200 pounds to 2,750 pounds. It also had Fiberglas wing skins, gas tanks, and seats, and was among the first airplanes ever to make such extensive use of Fiberglas.

They needed something to stimulate sales, Gilberti said, and thought up the Fiberglas idea. He said it was the first use of Fiberglas covering on an aircraft. The company sought help from a man across town who made Fiberglas boats. Workers took the bare steel-tube frame, wrapped it with chicken wire, and slathered it with plaster of paris to make a mold for the Fiberglas. The aircraft was then touted in Taylorcraft ads in 1956 as the “new Fiberglas Taylorcraft, the most advanced design for safer flying.” During demonstrations journalists were invited to hit the airplane with a hammer to demonstrate the aircraft’s toughness, and it was no lie. Photos of two Model 20s that crashed in wooded areas show the fuselage intact; the passengers were unharmed. “It was a tank,” Gilberti said.

The model 20 repowered Ag Topper built at Collinsville around 1951 were specialised versions of the model 15 as crop sprayers. TC 3A3 was issued on 12 May 1955 for 208hp Continental O-470-A and 225hp O-470-J engines.

Taylorcraft 20 Topper

Gallery

20 Topper
TC 3A3
Engine: Continental O-470-J, 225hp
Wingspan: 34’8″
Length: 24’4″
Max speed: 115 mph
Cruise speed: 110 mph
Stall: 46 mph
Range: 325 mi
Ceiling: 15,000′

20 Topper
TC 3A3
Engine: Continental O-470-A 208hp
Wingspan: 34’8″
Length: 24’4″

Zephyr 400
c.1990
Engine: Continental O-470J, 225hp
Wingspan: 34’8″
Length: 24’4″
Max speed: 160 mph
Cruise speed: 150 mph
Stall: 60 mph
Range: 675
Seats: 4
Price: approx $70,000

Taylorcraft 15 Tourist / Foursome / 16

Taylorcraft 15A

In the late 1940s and the early 1950s the people at Taylorcraft wanted to better cash in on the coming boom in general aviation. The boom never happened, but its promise generated a Taylorcraft big enough for the whole family.

The idea of a four-place aircraft began in 1945 as the war ended. A prototype was built at that time, but it never got out of the development stage. According to the book, The Taylorcraft Story by Chet Peek, the prototype began as a tube-and-fabric aircraft at the Taylorcraft plant in Alliance, Ohio, and was dubbed the Tourist. development stopped with the bankruptcy of the company.

Taylorcraft 15 prototype NX36320

When the Taylorcraft company was bought by Ben Mauro and moved to Conway, Pennsylvania, the model went with him but wasn’t developed further until 1949. Prototype NX36320] had a 125hp Franklin and the Model 15A, which retained the Tourist moniker, was intended to have a 125-horsepower Franklin engine. First flying on 1 December 1944, concerns that Franklin might go out of business caused a switch to 145-horsepower Continental C-145 engine.

The 15A features three large doors – a fourth was optional – slotted wing tips to improve aileron effectiveness at slow airspeeds, and the same door handles used for Nash automobiles.

It has a wing with wooden spars and stamped-aluminum ribs. C.G. Taylor, the founder and former owner, was working with Mauro as a vice president when he was asked to take weight out of the airplane; he took 150 pounds out but he never touched the wings. For stress testing during the wing’s design, it was hung from the roof of the factory and loaded with increasing weight over the course of an afternoon. Mauro got bored waiting for it to break and went back to his office. Finally the workers heard a crack and thought the wing had failed, but it hadn’t: The roof beam of the factory had cracked from the weight of the still-intact and heavily loaded wing.

Preflight includes draining two tank sumps and the gascolator. The tanks are covered by fabric. Features include side window panels that slide up and down and an overhead trim control. The preflight also includes the gas caps. Because they use forward-facing vent tubes, care must be taken not to install them backward, which can result in siphoning out gas in flight.

The interior is tight enough that you must fly with someone you like, but it is not uncomfortable. Steel tubes of the airframe limit foot space. Original avionics included Narco tube radios (an outside vent channeled air to cool the tubes).

Takeoff requires a 10-degree flap setting using a mechanical lever on the floor. (Takeoff with two people aboard took less than the advertised 500 feet). True airspeed measured at typical cruise power setting of 2,350 rpm was 85 knots (98 mph. Stalls with power on dropped the right wing.

Production began in 1947 at Conway, and later (c.1950) Collinsville. ATC 3A3 was first issued on April 3, 1951 for the 15-A with Franklin 6A4-150-B31 or 145hp Continental C-145-2 engines. Selling for $4,500 a total of 31 were built.

The original four-place 1953 demonstrator Taylorcraft 15A, N6653N, first went to a flight school in Texas where it was used for rides. Then it went to Alaska where in the 1950s and 1960s a church flew supplies to remote settlements until a shortage of parts led to dereliction. The aircraft sat in the weeds at Fairbanks International Airport in the 1970s until it left Alaska on a truck with the promise of restoration in Florida.

The restoration never happened, but two pilots in Alliance stepped in, restored it, then sold it to finance their North American T-6 restoration. Roe bought it in 1992 for $24,000 and brought it to Culpeper, Virginia. By 2010 it was owned by Robert Peterson of Mahaffey, Pennsylvania. It features a Lear Omnimatic navigation radio developed by Bill Lear, father of the Learjet.

Roe said. “I can use short fields – it probably made a heck of a bush plane in Alaska. If only it were a little faster.” He flight-plans for 105 mph and burns 8.5 gallons per hour; usable fuel totals 40 gallons. Roe uses 80 mph in the pattern, 70 on final, 60 over the numbers, and finds that touchdown occurs at 45 to 50 mph. The only modification he made was to add Fiberglas wing tips.

The Taylorcraft 16 of 1946 was an all-metal model 15 of which only one was built.

Taylorcraft 15-A Foursome
Engine: Franklin 6A4-150-B31, 150hp
Wingspan: 36’3″
Length: 24’0″
Useful load: 925 lb
Max speed: 125 mph
Cruise speed: 112 mph
Stall: 38 mph
Range: 450 mi
Seats: 4
TC 3A3 / ATC 775

Taylorcraft 15-A Tourist
Engine: Continental C-145-2, 145hp
Wingspan: 36’3″
Length: 24’0″
Seats: 4
TC 3A3 / ATC 775

Taylorcraft 500

The 1959 Model 500 that was tested briefly before being canceled.

Mike Rodina of Hampshire, Illinois, has the only Taylorcraft 500 on the registry. Basically a Model 20, it had a fifth seat mounted at an angle in the cargo compartment. The rear seats tilted forward to allow access, but after brief experimentation the idea was dropped. The 500 was also to have a nosewheel and disk brakes. It got the brakes, but the nosewheel modification was never attempted.

Taylorcraft Aviation Corporation / Taylorcraft / Taylor Brothers Aircraft Corp

Taylor Aircraft Company
Taylorcraft Aviation Company
Taylor-Young Airplane Company
Taylorcraft Aviation Corporation

C. Gilbert Taylor and his brother had first established the Taylor Brothers Aviation Corporation- slogan; “Buy Your Airplane Taylor Made” – in Rochester, New York, in 1926 to market the Taylor Chummy lightplane, a two-seat high-winged monoplane, priced at $4,000.

The Chummy failed to sell, and after Gordon died flying another Taylor design in 1928, Clarence moved to Bradford, Pennsylvania, where the townsfolk had offered him a new factory at the local airfield plus $50,000 to invest in the company. One of the investors was William Thomas Piper, who had made his money from oil wells.

More concerned about solvency than perpetuating his name, he re-organized the assets into the Taylor Aircraft Com¬pany, giving C. Gilbert Taylor half inter¬est in the new enterprise as an induce¬ment to stay on board. Piper handled the finances as the firm’s secretary and trea¬surer, while Taylor served as president and chief engineer.

After continuing with the Chummy for a time, Taylor abandoned the design and began work on a new inexpensive aircraft to compete with the heavier craft common at the time. A battle between engineer and businessman caused a rift between the two. Piper took advantage of Taylor’s absence during an illness, and instructed Taylor’s junior engineer Walter Jamouneau to modify the Cub, in Models E-2 and F-2, to be more attractive and marketable. Taylor returned from his illness and left the company in 1936; and Walter Jamouneau took over as chief engineer.

A disastrous factory fire brought production of the Cub J-2 to a halt. When the company ran into financial difficulties, manufacturing and marketing rights for the Taylor Cub, which had first flown in September 1930, were acquired by W. T. Piper in 1935 for $761, who in 1937, formed Piper Aircraft Corporation to continue production of this aircraft. It was placed back in production as the Piper J-3 Cub.

Taylor vowed to build a personal aircraft superior to the Cub. Taylor formed his own company in 1935 as Taylor Aircraft Company at Alliance, Ohio, renamed Taylor-Young Airplane Company, then Taylorcraft Aviation Corporation in 1940. In 1936 Taylor rented facilities at Pittsburgh-Butler Airport and first manufactured the “Taylorcraft” plane. Main pre-war lightplanes were Models B, C and D, of which C and D formed basis for formation of Taylorcraft Aeroplanes (England) Ltd. Taylor gave his airplane a closed cabin with doors and a control wheel instead of a stick. The fat, side by side T Craft was faster than a tandem Cub. It set speed, distance and altitude records for light airplanes. No Taylorcraft has a number below 25. They figured nobody would want an airplane from a company that had built only three or four.

During WWII, light aircraft were used for training, liaison, and observation purposes. Taylorcraft’s DCO-65 model was called the L-2 by the United States Army Air Forces and served alongside the military version of the Piper Cub in WW2. Built over 1,900 similar L-2 Grasshoppers for USAAF, TG-6 training gliders based on L-2, and components for Consolidated PBY, Curtiss C-46 and Douglas A-26.

In November 1938 the company established its Taylorcraft Aeroplanes (England) Ltd as its British subsidiary, based in Thurmaston, Leicestershire, England. British production was mainly of the Plus C and Plus D models, and in 1939 the Royal Air Force impressed 24 of the 32 aircraft for evaluation as observation and artillery spotter aircraft. The evaluation confirmed the soundness of the concept, and a derivative of the Plus D was ordered into production as the Auster Mk 1. This entered service in August 1942. The military chose the name “Auster”, which translates as a warm or gentle breeze, possibly from the south. Thus Taylorcraft Plus D built for the army became Auster Mk 1. After the war, Auster Aircraft Ltd was formed and commenced a series of variations on the basic theme until 1960 when it was absorbed into Beagle Aircraft Ltd.

Taylorcraft Aeroplanes Ltd developed the Taylorcraft Model ‘D’ and the Auster Mk. I through Mk. V, which became the backbone aircraft of the British AOP (Air Observation Post) and the three Canadian AOP squadrons, No. 664 Squadron RCAF, No. 665 Squadron RCAF, and No. 666 Squadron RCAF.

Built some 2,800 Model B-12Bs in 1945-1946, but in the fall of 1946 production was halted following a fire in the Taylorcraft factory at Alliance, Ohio and the company went into bankruptcy. Re-formed in 1947 as Taylorcraft Inc, producing models BC-12D, Ace, Traveler, Topper, Ranch, Wagon, Tourist, Sportsman and Special de Luxe.

In 1949 C.G. Taylor bought the assets from the former company, and started a new company Taylorcraft, Inc. at Conway, Pennsylvania. The company restarted production of the BC-12D Traveller and the BC-12-85D Sportsman. The company produced few aircraft and the type certificates were sold to Univair and production was halted.

The factory moved to Pittsburgh in 1954 but then ceased manufacture four years later. It was re-formed again in April 1968 as Taylorcraft Aviation Corporation, and from 1973 resumed production of an updated two-seat Sportsman 100.

In 1971 the Taylorcraft Aviation Corporation, owned by Charles Feris put the Model 19 back into production as the F-19 Sportsman and added the F-21 model. Feris died in 1976 and the production continued at a low rate until 1985. Charles Ruckle bought the company in 1985 and he moved the operation to Lock Haven, Pennsylvania, where the company produced 16 aircraft before it went bankrupt in 1986 and the company was offered for sale.

Company ceased trading 1986, and in 1989 was purchased by West Virginia based Aircraft Acquisition Corporation, developed a series of two/three-seat lightplanes under the F22 designation. From 1992 operated independently of AAC and took name of Taylorcraft Aircraft. The assets were sold to key investor East Kent Capitol.

1990: Taylorcraft Aircraft corporation, PO Drawer 3350, Morgantown, WV 26505, USA.

John Polychron, former CEO of Del Monte Foods purchased Taylorcraft and operated it for approximately one year until he sold it to Philadelphia Attorney Phillip O’Rielly. O’Rielly never reopened and the company became deeply in debt resulting in a Sheriff’s sale in 1996.

Taylorcraft was saved from extinction by Lee Booth, a former Marine and an engineer from Seaford Delaware. Booth renamed the Company Booth-Taylorcraft Aerospace, Inc. Booth-Taylorcraft Aerospace paid all creditors in full and relocated the entire company in 88 53 ft long truck trailers to Greensboro, North Carolina.

Booth, as Chairman and President, directed the Corporation through an extensive recertification of all type certificates, engineering, FAA audits up to the Aircraft Certification Office level, production procedures, complete re-tooling and certification of tooling and work processes. Booth enlisted the assistance of Darrell C. Romick, former Chief Engineer of Taylorcraft Airplane Company and of BF Goodrich. Romick was a close associate of Wernher von Braun and worked for Goodyear Aircraft in the 1950s.

Booth-Taylorcraft Aerospace, Inc became a contractor to numerous governments for military aircraft, weapons systems and firearms. Booth was the first Taylorcraft owner in the company’s history to keep the company debt free the entire time he operated it. In March 2000, Booth formed a strategic partnership by selling half of the Civil Aircraft Division to Harvey Patrick of Pats, Inc. Booth retained all military items, UAVs, several type certificates, designs and patents. The Small Aircraft Division was moved to Georgetown, Delaware at the Sussex County Airport. Booth and Patrick then formed Taylorcraft 2000, LLC and served as Co-chairmen. Booth eventually sold his half to Harvey Patrick and Taylorcraft 2000, LLC was owned by the Harvey and Vera Patrick Foundation. In 2003 The Harvey and Vera Patrick Foundation sold the company to Harry Ingram, with 100% financing.

Harry Ingram, moved the plant to La Grange, Texas in 2003 and on April 25, 2005 it was announced that the factory was moving again to Brownsville, Texas and outsourcing the labour.

On February 21, 2008 the company was repossessed by its former owner, Taylorcraft 2000 LLC. The previous owners had taken orders for new struts for existing aircraft to alleviate a repetitive inspection Airworthiness Directive and was delivering struts to customers. The design’s type certificates, drawings, jigs, templates and parts were put up for sale.

Taylor Imp

The Mini-IMP is a “second generation” version of the original, 2+2 place, Taylor IMP (an acronym for Independently Made Plane) homebuilt aircraft. This original version proved to be too complicated and too costly to build for the “average” homebuilder.

Design work began in 1973 for all-metal construction with a two-blade controllable-pitch prop aft of the negative-dihedral V-tail.

Engine: Limbach, later 200hp Franklin 4R pusher
Wingspan: 29’0″
Length: 22’0″
Useful load: 450 lb
Max speed: 150 mph
Stall: 50 ph
Seats: 4

Taylor Micro-Imp

In 1978, with the success of the Mini-IMP program, Molt Taylor and his friend, Jerry Holcomb began construction of the prototype Micro-IMP aircraft. It was intended as an alternative to the then-new “Quickie” aircraft, a Burt Rutan design, which was being offered by Quickie Aircraft Company of Mojave, CA. Like the Quickie, the Micro-IMP was intended to be a very light-weight, low-power and low cost sport plane. Molt and Jerry chose to use a new building material that they had developed for the primary structure, a special resin-impregnated, fiberglass-reinforced paper that they called TPG (Taylor-Paper-Glass).

The Micro-IMP was basically a smaller, lighter version of the Mini-IMP and embodied most of the Mini-IMP features and design ideas. It featured a fully retractable tri-cycle landing gear, full span, reflexing flaperons, a NASA GA-PC(1) airfoil, a unique two-position propeller and a fully trimmable inverted “V” tail.

Molt had intended to have Wicks Aircraft Company, a leading supplier of materials for experimental aircraft builders, provide complete kits for the Micro-IMP, with all the parts pre-printed on the TPG paper stock, so that the builder would only have to cut out the pieces and laminate them with the cloth. The kit would have included all instrumentation and materials to build the airplane. The engine which powered the prototype was a 25-hp Revmaster converted 620cc Citroen 2CV automobile engine which has been produce in the millions in Europe. The engine, which was intended to put out about 32-38 h.p. simply couldn’t be persuaded to put out more than about 16-18 h.p. and thus the prototype was severely underpowered. A planned 800 cc version of the engine never got produced.

The Citroen 2CV engine has been extensively modified to provide an excellent, low cost, durable, aircraft power plant and includes such features as solid state magneto, anti-reversion exhaust manifolding, injection carburetor, electric starting with alternator, etc.

The Micro-IMP was finished in 1981 and was last flown at a demonstration during Oshkosh 1982. At that time, the airframe was hung up in the rafters at Molt’s shop awaiting inspiration, time and money to install another, more powerful engine.

Due to other events, notably the Bullet 2100 project and Molt’s declining health, the Micro-IMP was not developed further. Jerry Holcomb went on however to develop, build and fly a refinement of the Micro-IMP design which he named the “Perigee”. Information packages were sold but plans and kits never materialized.

Prior to Molt’s death, the “hulk” of the Micro-IMP was sold to a teenager in the local area and its whereabouts at this time is unknown.

Designed in 1975, first built in 1976.

The limited tooling for the Micro-IMP and the production rights to the design were in the possession of the Mini-IMP Aircraft Company. A large collection of Molt’s original drawings and shop sketches for the Micro IMP have been found. These drawings along with a large number of B/W photographs were being made available on a compact disk. While there are no plans at this time for Mini-IMP Aircraft Co. to develop the design, they were interested in a joint venture with interested individuals or companies to further refine and market this aircraft.

Engine: 620cc Citroen 2CV, 25 hp
Gross Wt. 700 lb
Empty Wt. 360 lb
Fuel capaci¬ty 7 USG
Wingspan 27’
Length 15’
Max speed: 120 mph
Cruise 110 mph
Stall 45 mph
Climb rate 500 fpm
Takeoff run 800 ft
Range 500 miles
Undercarriage: retractable

Taylor Coot

Coot A

Molt Taylor developed his Coot Amphibian from a World War II Marine assault glider design that featured the unique low “Float-wing” common to both Coot A and Coot B models. The former features a fiberglass hull, the latter a twin-boom tail. Both prototypes have been flying for a number of years. The Coot Floatwing design eliminates the need for tip floats for lateral stability, provides a “deck” to step on for hand-cranking the propeller, protects the engine and propeller from spray, and provides ground-cushion effect for shorter takeoffs. Taylor considers the optimum engine to be the Franklin 180-hp Sport Six, which permits a smooth-water takeoff at 1950 pounds gross in six to eight seconds from a standing start though power can be supplied by any engine from 150 to 220 hp with a controllable propeller. A deep-V hull design permits rougher water operations than possible with twin-float designs, and a low thrust-line offers optimum elevator response for faster water liftoff. The Coot is a comfortable two-place ship with side-by-side seating and dual controls. The folding wings make road towing and home storage possible. With all his aircraft designs Molt Taylor emphasizes that performance and specification figures are greatly dependent on such variables as engine size, fuel capacity, etc.

Taylor Coot Article

The first Coot-A flew in 1969. Two prototypes were built, Coot A with a single tail, and Coot B with twin tail booms. Sooper-Coot Model A was a series version of the former.

Sooper-Coot A N1070

The Sooper-Coot-A two place amphibian price in 1982 was $12,000 (Excludes engine and instruments). Units delivered to June 1982: 100.

Coot A

Over 400 reportedly were being constructed by home-builders by 1977 with various 100-180hp engines.

Coot
1969
Engine: Franklin 335, 180hp
Wingspan: 36’0″
Length: 20’0″
Useful load: 850 lb
Max speed: 140 mph
Cruise speed: 130 mph
Stall: 56 mph
Seats: 2

Coot A
Engine: Franklin, 180 hp
HP range: 100-225
Construction: wood/fiberglass
Wingspan 36’-37’
Wing area: 180 sq.ft
Weight empty: 1450 lbs
Gross: 1950 lbs
Baggage 100 lb
Fuel capacity 24-50 USG
Height: 7 ft
Length: 22 ft
Seats: 2
Landing gear: retractable nose wheel
Speed max: 140 mph
Cruise 100-130 mph
Climb rate: 600-1250 fpm
Stall 45-50 mph
Takeoff run (land) 200-600 ft
Takeoff time (water) 10-12 seconds
Service ceiling: 15,000 ft
Range: 500 sm
Designed: 1967
First built: 1968

Coot A
Empty weight: 700 kg
Wing span: 11 m
Wing area: 14 sq.m
Fuel capacity: 151 lt
Engine: Lycoming/Continental
MAUW: 1043 kg
Seats: 2
Max speed: 190 kph
Cruise speed: 177 kph
Minimum speed: 97 kph
Climb rate: 5 m/s
Fuel consumption: 23 lt/hr
Plan price (1998): $205

Sooper-Coot-A
Gross weight: 1,950 lb
Empty weight: 1,250 lbs
Useful load: 700 lbs
Seats: 2

Taylor Aerocar

Extensive development was undertaken to enhance flight and road performance. Accumulated road travel on six Aerocars exceeded 200,000 miles (321,865 km) and more than 5,000 flying hours.

One prototype was built in 1949 (N31214/N4994P), sold to B F Goodrich Co c.1952 for $10,000. In 1956 production under 4A16 totalled 5 (N100D/103D), plus 1 unlicensed for testing. Certification was in 1956.

With business recessions in the 50’s and 60’s, a war priorities in Korea and Vietnam, the Aerocar was never put into large scale production.

The most famous was NC102D, serial number 4, sold to actor/pilot Bob Cummings who used it on his long running TV show, as well as for everyday transportation. That machine was specially fitted and certified with a 135hp O-290 Lycoming. The other Aerocars were powered with 143hp versions of the O-320.

The Aerocar II Aeroplane aka 1-A of 1964 was a four seat non-roadable tri-gear version of the original Aerocar using many of its components and with a fiberglass cab. Power was a135hp Lycoming O-290-D2 pusher. The project was considered by Ford Motor Co but never pursued. The Model II first flew in August 1953.

Taylor Aerocar II

The Aerocar (TC 4A16) was developed through three models, and the two place Aerocar III, aka 1-C, first flew in 1968. A small, streamlined red car about the size of a Honda Civic, with a pair of bucket seats, deep pile carpet and a woodrim steering wheel. It has a 143 hp Lycoming engine with a fluid drive system for its retractable road wheels and dry fluid drive for the Hartzell ground-adjustable pusher propeller mounted behind the aircraft’s distinctive Y shaped tail unit. In the air it would cruise at 217 kph (135 mph), at 97 kph (60 mph) on the road, and go 24 km (15 miles) for every 4.55 litres of fuel burned, flying or driving. The car is 11 feet long and five feet wide. The wings and tail fold to only eight feet wide for highway travel. When it turns into an Aerocar, the plane is 23 feet long. Possibly was the one advertised as Sky Car in a non-flying version.

The most famous was NC102D, serial number 4, that was sold to actor/pilot BobCummings who used it on his long running TV show, as well as for everyday transportation. That machine was specially fitted and certified with an O-360 Lycoming. The other Aerocars were powered with versions of the O-320.

With business recessions in the 50’s and 60’s, a war priotites in Korea and Vietnam, the Aerocar was never put into large scale production.

Extensive development was undertaken to enhance flight and road performance. Accumulated road travel on six Aerocars exceeded 200,000 miles (321,865 km) and more than 5,000 flying hours.

The Aerocar was developed through three models, and the Aerocar III first flew in 1968. A small, streamlined red car about the size of a Honda Civic, with a pair of bucket seats, deep pile carpet and a woodrim steering wheel. It has a 143 hp Lycoming engine with a fluid drive system for its retractable road wheels and dry fluid drive for the Hartzell ground-adjustable pusher propeller mounted behind the aircraft’s distinctive Y shaped tail unit. In the air it would cruise at 217 kph (135 mph), at 97 kph (60 mph) on the road, and go 24 km (15 miles) for every 4.55 litres of fuel burned, flying or driving. The car is 11 feet long and five feet wide. The wings and tail fold to only eight feet wide for highway travel. When it turns into an Aerocar, the plane is 23 feet long.

Model III

The Model II Aerocar was a pure aeroplane (non-roadable) that used the Aerocar I wings, tailcone and tail plus some fuselage parts. It has a tricycle gear instead of the Aerocar I’s 4-wheel landing gear. Molt sold this maching to Ed Sweeney (who also owned Bob Cummings machine).

The Aerocar III was an updated version of the Aerocar I with a more modern shape for the car body that incorporated an improved fiberglass body and retractable wheels. The machine is displayed at the Museum of Flight in Seattle.

Aerocar III

Aerocar I serial number 2, registered N103D was owned by Gary Norton.

Molt Taylor donated the prototype of his flying automobile, the Aerocar, to the EAA Aviation Foundationn. A complete restoration was commenced at Hales Corner. This halted during the move to Oshkosh. The Buehler Foundation then provided a grant to provide the financial resources and the skilled manpower to complete the restoration. Molt Taylor was providing photographs, documentation, and his knowledge to assist.

Ford Motor Company wanted to build Aerocars, but the Federal Aviation Administration said no way did they want the sky full of flying automobiles. They were going to build 25,000 of them the first year and with their dealer organization they figured they could sell them. It never happened.

Gallery

Aerocar I
Engine Lycoming O-290, 135-hp / Lycoming O-320, 143 hp
Wing span: 34’0″
Length: 21’6″
Gross wt. 2,050 lb
Empty wt. 1,400 lb
Fuel capacity 24 USG
Top speed 112 mph
Cruise 100 mph
Stall: 50 mph
Range 300 miles
Ceiling 12,000 ft
Initial climb rate 500 fpm
Takeoff run 655 ft
Landing roll 300 ft
Seats 2

Aerocar II / 1-A
Engine: 135hp Lycoming O-290-D2
Wingspan: 34’0″
Wing area: 168 sq.ft
Length: 22’9″
Height: 7 ft 2 in
Empty weight: 1408 lb
Loaded weight: 1950 lb
Useful load: 900 lb
Max speed: 112 mph
Cruise speed: 100 mph
Stall: 50 mph
Range: 300 mi
Ceiling: 13,000′
ROC: 500 fpm
Price: $9,995
Seats: 4

Aerocar III / 1-C
Engine: Lycoming O 320 AlA 4 cylinder, 143 hp (auto 40 hp)
Length: 21 ft 6 in
Wingspan: 36 ft
Useful load: 720 lb
Max speed (air) 137 mph, (road) 67 mph
Cruise spped: 120 mph
Stall: 50 mph
Ceiling: 12,000 ft
Range: 500 miles
Seats 2