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.
Taylor E-2 Prototype NC10547 with C G Taylor and company pilot Bud Havens
Taylor first built a glider that looked like a small Breezy and the E 2 Cub evolved from towing that glider behind a car up and down the Bradford runway.
Designed by C. Gilbert Taylor in 1930 and produced as the Taylor E 2 Cub in 1931, much of the inspiration and many of the design goals for the airplane came from W.T. Piper, Sr. Taylor selected the U.S.A. 35B airfoil for the Cub. This airfoil had a reputation for providing favorable flying qualities at low speeds; all subsequent Cubs. The E 2 was open air except for a windshield and had squared off wingtips and tail surfaces. The tandem cockpit of the E 2 was without side windows, but a young man named Waiter Jamouneau, subsequently chief engineer and now a vice president at Piper, designed optional sliding side windows and a door arrangement that remain features of the Super Cub.
Reliable lightplane engines were virtually nonexistent when the E 2 was designed. For the first E 2, Taylor found a two cylinder engine of 20 horsepower. It was known as the Brownbach Tiger Kitten, and the name reportedly inspired the E 2 to be called the Cub. The plane handled fine on its first flight (in September 1930) but on 20 hp didn’t get too high five feet, actually The new Taylor E-2, now known as the “Cub,” was meant to be an affordable aircraft that would encourage interest in aviation and was awarded its type certificate on July 11, 1931 and licensed by the U.S. Department of Commerce for manufacture.
Twenty-two Taylor E-2 Cubs were sold during 1931, retailing for $1,325; by 1935, sales had increased to more than 200 E-2 Cubs.
A 45 hp, nine-cylinder French Salmson AD-9 was tried: its performance was spectacular, but it was too expensive.
Continental provided the solution with the A 40, a “40 hp” flat four that actually produced 37 hp. The E 2 was certified with this engine on June 15, 1932 and was put on the market for $1,325, or $1,495 with optional 40hp Aeromarine AR-3 engine, or $895 less motor.
Taylor E-2 NC14346 with AR-3 engine
Unfortunately, the early Continentals were giving trouble, for the engine company was using the Cubs as test beds. One of Piper’s five children, Tony, said that he rarely got more than 20 miles per forced landing. Sales to people who wanted to fly longer between stops were, naturally, a little sluggish. There was a frustrating period before Continental improved the A 40 during which Taylor actually started designing his own engine.
Continental added dual ignition and cured the annoyances of blowing head gaskets and breaking crankshafts.
Taylor E-2 NC15370 with A-40 engine
The Prototype (s/n 11) was powered by a 20 hp Brownbach Tiger Kitten and was first flown on September 12, 1930. The E2 barely managed to leave the ground with the tiger kitten, however the engine left a legacy in that it prompted one of C.G. Taylor’s colleagues to remark that since the engine was called the Tiger Kitten the E2 should be called the cub. The engine was deemed too weak and a 40 hp French Salmson was tried and deemed too expensive. Ultimately the decision was made to try a brand new and untried 40 hp engine from continental. That engine was an air cooled flat four cylinder designated the A-40. An uncertified A-40 was fitted to s/n 12 which was completed on April 9, 1931. The engine had a number of teething problems and Taylor has been quoted as saying that in the first 30 days of flying with the A-40 the E2 had to make 26 forced landings. It was also discovered that the crankshaft’s tended to break at around 100 hours.
Continental eventually worked the bugs out and the A-40 received its certification on May 15, 1931 which cleared the way for the E2 aircraft certification on June 15, 1931. The E2 was originaly certified under group 2, no 2-358 which covered the first 14 aircraft. The remaining aircraft were certified under ATC A455 which was issued on November 7, 1931 (covering s/n 26 and up.) The aircraft originaly sold for $1325 and no options were offered. The fuel tank was moved from the wing as shown on s/n 12 to the fuselage where it was located between the panel and the firewall starting with s/n 13. A fully enclosed cockpit was introduced on February 9, 1932 and became standard starting with s/n 35 and up.
Sales reflected the improvements, and 351 E 2s were produced between 1931 and 1936.
E-2
In the midst of the depression Continental announced that they were getting out of the aircraft engine business (a decision they later changed.) As a result the Aeromarine AR3-40 (40 hp) was installed starting with s/n 75 (3 Jan 34). This new configuration was designated the F2 cub. The Aeromarine was not satisfactory and several further engines were tried (models G2 with a Taylor designed T-40 and the H2 with a 35 hp Szekely SR-3-35.) Eventually Continental updated to the A-40-3 and this engine was used for s/n 178 and up.
The company was always sensitive to customer desires, and in 1936, Taylor introduced a refined Cub in order to incorporate design improvements as well as suggestions from the field. A young man named Walter Jamouneau was given the job of improving the E 2 resulting in the Piper J 2. In 1937 a fire destroyed the plant, prompting the company to relocate to a defunct textile mill in a town called Lock Haven. In November of 1937, the relocated company changed its name and became the Piper Aircraft Corporation.
The 1934 Taylor F-2 Cub (ATC 525) featured and open-sided cabin with optional side panels. Selling for $1,470, about 30 were built.
The 1934 Taylor G-2 Cub was an F-2 with a 40hp Taylor T-50 experimental motor. Only the one was coverted, N14756, which was rebuilt as an H-2 Cub in 1935.
The 1935 Taylor H-2 Cub (ATC 572) featured an open-sided cabin with optional side panels. Selling for $1,425, at least four were built.
Production Summary
Year
Model
Quantity
S/N Range
Note
1931
E-2 Prototype
1
11
1931
E-2
21
12 to 32
1932
E-2
22
33 to 54
*
1933
E-2
18
55 to 72
1934
E-2
1
73
1934
F-2 Prototype
1
74
1934
E-2 & F-2
64
75 to 139
*
1934
H-2 Prototype
1
140
1934
E-2
8
141 to 148
1935
G-2
0
149
*
1935
E-2 & H-2
206
150 to 358
*
1936
E-2
5
359 to 380
*
Total Production: 348
22 Aircraft in the batches marked * were not delivered. They were either not built or they were completed as later models and assigned new serial numbers.
Taylor E 2 Cub Engine: Continental A 40, 36 hp Length: 23 ft 3 in / 6.78 m Wingspan: 35 ft 3 in / 10.74 m Chord: 5 ft 3 in Airfoil: USA 35B Wing Area: 183 sq.ft Empty Weight: 532 lb Gross Weight: 925 lb Useful Load: 393 lb Gross Weight (ATC 455): 970 lb Emp Weight (ATC 455): 556 lb Useful Load (ATC 455): 414 lb Fuel Qty: 9 gal (54 lb) Oil: 1 gal (7 lb) Fuel Consumption: 2.8 gph Max speed: 74 kts / 137 km/h / 80 mph Cruise speed: 68 mph Stall: 28 mph Best Climb: 450 fpm Ceiling: 12,000 ft Take off (ground run): 120 ft Landing (ground roll): 95 ft Range: 173 nm / 320 km Crew: 2 Original Sales Price: $1325 Datum: Rear of Wing LE (aft positive) CG Limits: +16 to +20.5 in Incidence at Root: 2.5 deg Incidence at Tip: 0 deg Diehedral at Front Spar: 3/4 deg Diehedral at Rear Spar: 1 deg Horiz Stab Area: 24.2 sq.ft Aileron Area: 9.77 sq.ft Rudder Area: 7 sq.ft Fin Area: 3 sq.ft
The birth of Taylorcraft came in early 1936 when city fathers offered C G Taylor the old Hess-Argo factory rent-free in order to encourage new industry. William C Young entered the picture as a partner in April 1937, and city support was dramatically demonstrated in late 1937 in the sale to townspeople of more than 35,000 shares of company stock for needed capital.
The Taylorcraft A represents the first model series of the line, and it is powered by the 40-horsepower Continental A40-4 engine, one of the first to use opposed cylinders. The engine came out in the early 1930s and was used on the Taylor Cub that later became the Piper Cub. The huge tachometer, oil temperature gauge, and oil pressure gauge were bought by Taylorcraft from the same supplier that sold the units to the Dodge car company, and relabeled. (They were used in the early Luscombes, too.) As the model numbers increased, so did the number of doors: one with the A, two with the B, and three with the 15A and 20.
The prototype, NX16393 c/n 25, was built by Taylor Aviation Co under (2-529) and subsequent planes by Taylor-Young Airplane Co under (ATC 643). Selling in 1936 for $1,495 and $1,595 in 1938. With company reorganization in 1938 it gained a “craft” and the Taylor-Young A became known and advertised as Taylorcraft A.
Taylorcraft production includes 100 prewar Model As, 1800 military L-2s, more than 2800 post-war BC-12Ds, and more than 120 F-19 Sportsmans.
A total of 606 were built. Prototype NX16393, NC15757-15763, NC15776, NC18301-18347, NC18349-18373, NC19000-19099, NC19600-19699, NC19800-19818, NC19821-19895.
The Taylor Brothers Company had produced two two-place, side by side, high wing monoplanes called the Chummy. Designed by C G Taylor it was a fabric covered high wing airplane with a price tag of $3,985 during the Depression. The planes were first known only as Chummy or Arrowing Chummy; numeric designations came in 1930.
First flown in December 1927 piloted by Gordon Taylor. The two built were NX4203 and N4901 c/ns 3 and 4, powered by 90hp Anzani and 125hp Siemens-Halske SH-12 engines.
Wingspan: 34’0″ Length: 22’0″ Max speed: 110 mph Cruise speed: 100 mph Stall: 38 mph Range: 500 mi
Two Special four place monoplane were ordered in 1928 by a Mr Wuriman and a Mr Bishops. Powered by 180hp Hisso, only one was finished, and that eventually sold to a George Kallfelz registered N7698.
The 1958 Taylor Aero Plane was a four-place version of the Aero-Car built strictly as an airplane by eliminating the “car” components. It was built by Aerocar of Longview, Washington. The engine was behind the cabin and the wings fold for storage.
Engine: Lycoming, 143 hp Span: 34 ft Weight: 1,150 Ib
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