TEAM 1030R Max 103UL

1030R Max 103UL

The 1030R Max 103UL featured an open cockpit with swing over canopy.

JDT 1030F MAX 103
Engine: Hirth F-33
Flight controls: 3-Axis
Wingspan: 25′ 0″
Wing area: 112.5 sq. ft.
Wings: Removable
Length: 16′ 0″
Empty weight: 250 lbs.
Gross weight: 500 lbs.
Design load factors: +4.4 -1.8
Top speed: 63+ mph
Cruise speed: 55 mph
Stall speed: 26 mph
Climb rate: 650 fpm
Vne: 90 mph
Take-off roll: 150 ft.
Landing roll: 180 ft

1030R Max 103UL
Engine: Rotax 277, 28 hp
Fuel cap: 5 USG
Weight empty: 250 lbs
Gross: 500 lbs
Height: 5 ft
Length: 15.5 ft
Wing span: 25 ft
Wing area: 113 sq.ft
Speed max: 62 mph
Cruise: 55 mph
Range: 120 sm
Stall: 26 mph
ROC: 650 fpm
Take-off dist: 150 ft
Landing dist: 180 ft
Service ceiling: 10,000 ft
Seats: 1
Cockpit width: 22 in
Landing gear: tail wheel
LSA: yes

TEAM Inc / ISON Aircraft

Tennessee Engineering and Manufacturing

1995-8: 10790 Ivy Bluff Rd. K, Bradyville, TN 37026, USA.

Markets plans and/or kits to build a range of aircraft, including Air-Bike single-seat and open-frame microlight, Hi-MAX single-seat cabin monoplane, and miniMAX single-seat mid-wing monoplane.

ISON Aircraft (formerly TEAM Aircraft) won prestigious awards at Oshkosh and Sun ‘n Fun, and Wayne Ison and were EAA Ultralight Hall of Fame Inductees.

Production of the TEAM Inc Mini-MAX and Hi-MAX lines has moved to the JDT facility at the Nappanee, Indiana Airport (Hangar M). Who do not own the rights to any other Ison designs.

Taylorcraft F-22

Taylorcraft F22 N191TC

The design has its origins in the Taylorcraft Model B of the early 1940s, which was developed into the F-19 that was built until 1980. A higher-powered version, the F-21 two-seat sporting trainer, was designed with aluminium ‘T’-beam wing spars and a new fuel system. This in turn has given way to the F-22, in which the most noticeable change is the introduction of a nosewheel and flaps.

Other innovations on the F-22 include wider doors with hinged windows for better ventilation, easier access to seats, and quick-removal rear seats for cargo flights.

The 1990 F22 was a revival of original Taylorcraft BC-12D design, this time with flaps, options of IFR, tri-gear or conventional gear. When powered by a 180hp Lycoming engine it sold for $42,975.

The 1992 F22A Nose Wheel Taylorcraft aircraft were built by Taylorcraft in the old Piper Plant in P.A. USA.

Taylorcraft F22A Tracker
F-22A Tracker N87HJ sn/2214 Courtesy Paul Harrington – Harrington Aviation

This 1992 Taylorcraft F-22A has flaps, strobe lights, nav lights, dual landing lights, heated pitot tube, new sealed wing struts, disc brakes, full sky light, stall warning system and much more.

About 6 of the nosewheel F-22A were built as late as 1992. These models were about the last 6 or so to come out of the Taylorcraft factory, when it ended production.

Engine: Lycoming O-235-L-2C, 118hp
Wingspan: 36’0″
Length: 21’2″
Useful load: 650 lb
Max speed: 125 mph
Cruise speed: 120 mph
Stall: 49 mph
Range: 724 mi
Ceiling: 18,000′
Seats: 2

Taylorcraft F22A Tracker
Engine: Lycoming O-235, 118 HP
Wingspan: 36’0″
Length: 21’2″
Empty Weight: 1090 lbs
Max Weight 1750 lbs
Useful Load: 660 lbs
Max Fuel: 42 USGal
Service Ceiling: 18000 ft
Cruise Speed(75%BHP): 96 kts
Range (75% BHP): 501 nm
T/O Roll: 500 ft
T/O over 50 ft: 792 ft
Seat Capacity: 2

Taylorcraft Ranger / STOL 180 / Sports Special

Ranger 180GT

US aircraft manufacturer Taylorcraft was marketing a Taylorcraft STOL 180 in 1990 as well as a Ranger and 118hp model. Features of the new 180 range include a three-¬bladed fully reversable Sensenich propeller as well as a Sports Special an aerobatic variant intended as a candidate for the USAF Air Training Command’s aerobatic screening aircraft for potential fighter pilot candidates. The Sports Special is reportedly capable of 155 mpb in level flight and a 2300 fpm capability.

A three seat 180 hp Lycoming powered aircraft. The 180GT is billed as a STOL performer with an initial climb rate of over 1600 fpm.

STOL 180

180GT
Engine: Lycoming, 180 hp
Seats: 3
ROC: 1600fpm

118hp
Engine: 118 hp

Sports Special

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 Bullet

The 1982 Taylor Bullet was a two-seat counterpart of Micro-IMP. With retractable undercarriage, power was a 2100cc Revmaster pusher. He used the best features of his earlier designs, including the GA(PC)-1 airfoil with full length flaperons and optimal adaptations of TPG. With significant assistance from Jerry Holcomb, Molt wound up with a contoured fiberglass shell that gave no impediments to the smooth passage of air over it. The wings had a high angle of attack, allowing it to get in and out of small airstrips. Molt kept the nose low (tail high) for maximal forward visibility during low-speed take-offs and landings. This allowed him to mount the propeller on the tail and give clean airflow over the fuselage and wings. Its reverse pitch capability shortened the ground run after landing. By sweeping the wings forward and placing the Revmaster engine at the front of the plane, Molt assured that variations in pilot/passenger weight would not disturb the Bullet’s center of gravity.

As with most prototypes, there were some annoying glitches, such as difficulties with the long Flexidyne coupling between the engine in front and the propeller at the tail, and some trouble retracting the main gear, which were left extended during the 50 hours of flight-testing. Eventually the owner, Jim Berry, donated his Bullet to the Oregon Air Museum in Eugene, where it remains on display.

Engine: Revmaster 2100cc, 70 hp
Wingspan: 31’0″
Length: 18’9″
Useful load: 550 lb
Max speed: 150 mph
Stall: 50 mph
Range: 500 mi
Seats: 2

Taylor Mini-Imp

During the energy crisis of the mid 1970’s Moulton B. (Molt) Taylor decided to turn to a small, easy-to-build, light plane which focused on maximum cruise speed and efficiency. The result is the Taylor Mini-IMP.

Taylor Mini-Imp Article

The Mini-Imp is a two-seat version of the single-seat Imp designed in 1975. It features an unusual configuration with a pusher prop aft of an inverted V-type tail assembly and cantilevered high wing that folds back for towing and storage. The wing is the latest NASA design with spoiler and flaps. The retractable gear is the tricycle spring-legged type. A controllable propeller is available. Power is provided by any engine from 60 to 115 hp with the 60-hp Franklin, 60-hp Limbach VW, 70-hp Turbo Revmaster VW, 100-hp Continental or 115-hp Avco Lycoming modification being the most common. The aluminum and fiberglass Mini-Imp requires a minimum of tools to construct, and all hard-to-build parts are available. It offers unequalled safe flyability and stability, positive spiral stability, limited acrobatic capability (stressed to 9 Gs), and good fuel economy (3 1/2 gph).

The O-200 powered price in 1982: $10,000 (Includes complete kit). All metal construction. Year. Units delivered to June 1982: 50.

The Model “C” version of the Mini-IMP is the long nose version which was developed after the prototype was flown with the Limbach converted VW engine. The Model “C” is powered with the Continental O-200 engine (100 HP at sea level at full throttle). The Model “C” also incorporates a larger baggage compartment and the nose is lengthened 12 inches so that the pilot sits one foot further forward of the main bulkhead. This lengthening of the nose required the installation of an additional vertical fin on tip of the tail boom giving the “long nose” Mini-IMP an inverted “Y” tail configuration. This addition was used instead of lengthening the tail boom to accommodate the longer nose length of the design rather than lengthen the shaft and to accommodate the further aft placement of the propeller (with its weight effect on the CG).

The O-200 powered Mini-IMP requires the use of a different propeller and due to the increased weight of the engine a heavier landing gear is used. The drawings indicate several other areas of change for the Model “C” needed to accommodate the higher power and resulting performance increases. These include heavier side frame members and a different nosewheel installation. When ordering “kits” be sure to advise of your preference in this regard. The same set of drawings is used to cover either version of the Mini-IMP (the long nose or the short nose).
It is practical to use the long nose version with the big baggage compartment if the builder intends to use the turbocharged Revmaster engine and controllable propeller. However, if the normally aspirated Revmaster engine and a fixed pitch propeller (or other such VW conversion) is to be used, the short nose configuration should be used.

A prototype of the Model “C” has been flown extensively and its improved performance with the higher power is evident. Flight tests of the O-200 powered Mini-IMP “C” have shown a cruise speed of approximately 175 MPH at 4000 foot altitude at 75% rated power. Climb speeds of better than 1500 FPM are initially available at full throttle. These performances are obtained at approximately 1000 pounds gross weight. Exact performance to be obtained with any engine combination is of course dependent on the power level the builder wants to pull from his engine/propeller installation. The O-200 Model “C” requires approximately the same takeoff and landing run as the VW versions, with exact performance dependent on temperature, altitude, and gross weight.

Following Taylor’s death, the plans and licensing for the Mini-IMP have been marketed by the Mini-IMP Aircraft Company of Weatherford, Texas. The Mini-IMP Aircraft Company was formed to provide builder support and to further promote the design.

Gallery

Engine: Continental O-200, 100 hp
Hp range: 8-125
Speed max: 200 mph
Cruise: 170 mph
Range: 500 sm
Stall: 45 mph
ROC: 1500 fpm
Take-off dist: 600 ft
Landing dist: 600 ft
Service ceiling: 20,000 ft
Fuel cap: 13 USG
Weight empty: 700 lb
Gross: 1000 lb
Height: 4 ft
Length: 16 ft
Wing span: 27 ft
Seats: 1
Cockpit with: 26 in
Landing gear: retractable nose wheel

Engine: 60-hp
Gross Wt. 800 lbs
Empty Wt. 500 lbs
Fuel capacity 12+ USG
Wingspan 25’
Length 16’
Cruise 150+ mph
Stall 48 mph
Climb rate 1200 fpm
Takeoff run 800 ft
Range 500 sm

Taylor, Molt

Born in 1912 in Portland, Oregon, Moulton B. (Molt) Taylor developed the Aerocar, the flying automobile that is easily converted back to a car with trailerable wing and tail components. Taylor started out in 1948 with $50,000 capital put up by businessmen in his home town of Longview, Washington. But his innovative ideas have found their way into many other unusual aircraft including the US Navy XLRQ-1 Amphibious Assault Glider, the Coot Amphibious aircraft, the IMP (also known as the Ascent 1 Tribute) and the Mini-IMP and Micro-IMP.

He wrote regularly for Sport Aviation, and other aviation magazines on everything from engine selection to static testing of aircraft parts.

1961: Aerocar International, Longview.
c.1970: Aerocar Inc.
Moulton B “Molt” Taylor, Chehalis and Longview WA. USA
1980: MB. (Molt) Taylor, P.O. Box 1171, Longview, WA 98632, USA.
Mini-IMP Aircraft Co, Saginaw TX. USA
2001: Aerocar International.

Molt was officially inducted into the EAA Hall of Fame by Paul Poberezny on November 10th, 1995. Only 6 days later, on November 16th, he left this world and us behind.

Aerocar International is a new firm formed by Roy Hyde (Hyde Investment Co) of Ft Worth TX with Molt Taylor as vice president-engineering and Herman Zimmer, vice president-marketing. Taylor, who first flew his Aerocar in 1950 and has logged more than 1,000 flight hours and 100,000 road miles on the vehicle, was a naval aviator and project engineer at the Naval Aircraft Factory where he was in charge of pilotless aircraft and missile development prior to setting up Aerocar Inc in Longview.

Taylor Aero Industries Bird

Taylor Bird N303TB

Circa 1980 Clarence Gilbert Taylor and son Bruce built the two place, mid wing ‘Bird’, registered N303TB, with a 75hp Subaru pusher (converted auto engine). Single tail boom with T-tail.

An update of the original Bird that appeared at Oshkosh in 1976.

Engine: 75hp Subaru
Wingspan: 26’0″
Length: 18’0″
Useful load: 600 lb
Max speed: 115 ph
Cruise speed: 105 mph
Stall speed: 45 mph
Range: 420 mi
Seats: 2