Taylor Cub
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The Taylor Cub was originally designed by C. Gilbert Taylor as a small, light and simple utility aircraft, evolved from the Taylor Chummy. It is the forefather of the popular Piper J-3 Cub, and total production of the Cub series was 23,512 aircraft.[1]
Key Information
Design and development
[edit]In 1930 with C. G. Taylor as Chief Engineer, the Taylor Aircraft Company embarked on the production of a two-seat tandem low-powered aircraft, designated the Taylor Cub. The Cub featured a design with wings mounted high on the fuselage, an open cockpit, fabric-covered tubular steel fuselage and wooden wings which used the USA-35B airfoil.[citation needed] It was originally powered by a 20 horsepower (15 kilowatts) Brownback "Tiger Kitten" engine. Since the young offspring of the tiger is called a cub, Taylor's accountant, Gilbert Hadrel, was inspired to name the little airplane "The Cub".[2]
The "Tiger Kitten" engine roared but was not strong enough to power the Cub. On September 12, 1930, a test flight of the Taylor Cub ended abruptly when the aircraft ran out of runway; the underpowered engine was unable to lift the monoplane higher than five feet (1.5 meters) above the ground. In October, a Salmson AD-9 radial engine produced in France was fitted to the Cub giving good performance, but it was expensive to maintain.[citation needed]
Finally in February 1931, Taylor introduced an improved Cub airframe, powered by the newly developed Continental Motors 37 horsepower (27.6 kilowatt) A-40 engine. The new Taylor E-2 Cub was awarded Category 2 or "Memo" certificate 2-358 on June 15, 1931, and licensed by the U.S. Department of Commerce for manufacture (it was later awarded full Approved Type Certificate A-455 on November 7). Twenty-two E-2 Cubs were sold during 1931, retailing for $1,325; by 1935, cost had increased to $1475 and by the end of production in February 1936, 353 Cubs had been built at Emery Airport, Bradford, Pennsylvania.[citation needed]
Variants
[edit]
- Taylor E-2
- Prototype first flown in September 1930 with a 20 hp (15 kW) Brownbach Tiger Kitten engine, engine changed to a 40 hp (30 kW) Salmson D-9 radial in October 1930. although the D-9 had enough power for the E-2 it was expensive and was built to metric sizes which would have caused maintenance problems.
- Taylor E-2 Cub
- Production variant of the E-2 with the Continental A-40-2 or in later production the improved A-40-3 engine, produced from 1931 to 1936.
- Taylor F-2
- Persistent troubles with the early A-40 engines on the E-2 led to a search for other suitable powerplants. First choice was the Aeromarine AR-3-40, a three-cylinder air-cooled radial engine which produced 40 horsepower at 2050 RPM. The Aeromarine-powered Cub was designated the F-2.[citation needed] One float-equipped aircraft was designated F-2S.
- Approved Type Certificate A-525 was awarded on February 16, 1934, and the F-2 had an initial price of $1495. Approximately 33 were made.[citation needed]
- Taylor G-2
- In another search for a replacement for the A-40, Taylor went to the extreme of designing and building his own 35-40 horsepower engine. This was fitted to serial number 149, registration X14756. The Taylor-powered Cub was designated the G-2.[citation needed]
- No information was published about the one-off engine, and no details are known today. With a new engine, this aircraft would become the Taylor H-2.[citation needed]

- Taylor H-2
- The G-2 Cub was re-engined with a 35 horsepower Szekely SR-3-35 (pronounced Say-Kai), another three-cylinder air-cooled radial engine which produced 35 hp at 1750 RPM. The Szekely-powered Cub was designated the H-2.[citation needed]
- Approved Type Certificate A-572 was awarded on May 28, 1935. Three F-2's were converted to H-2 standard (construction numbers 40, 66 and 74), as was a single J-2 (c/n 792).[3][4]
- In 1937, Beverly Dodge and a passenger set the women's altitude record (16,800 feet) in a Szekely powered Taylor H-2.[citation needed]
- Taylor J-2
- The Taylor J-2 was the final iteration of the Cub series under the Taylor name, before the company renamed itself to Piper Aircraft in November 1937, production had moved from Bradford to Lock Haven, Pennsylvania earlier in 1937 following the destruction of the Bradford factory by fire.[citation needed]
- Taylorcraft A
- When C. G. Taylor broke with Taylor Aircraft and founded the new company Taylor-Young, its first aircraft, originally known as the Taylor-Young Model A, was little more than a refined Cub with side-by-side seating. Taylor-Young soon changed its name to Taylorcraft and the Model A became the Taylorcraft A, first in the Taylorcraft series.[citation needed]
Operators
[edit]Surviving aircraft
[edit]Canada
[edit]- 289 – E-2 on static display at the Canada Aviation and Space Museum in Ottawa, Ontario.[5][6]
United States
[edit]- 32 – E-2 airworthy at the Western Antique Aeroplane & Automobile Museum in Hood River, Oregon.[7][8]
- 33 – E-2 on display at the Shannon Air Museum in Fredericksburg, Virginia.[9]
- 36 – E-2 airworthy at the Western North Carolina Air Museum in Hendersonville, North Carolina.[10][11]
- 54 – E-2 airworthy at the Golden Age Air Museum in Bethel, Pennsylvania.[12][13]
- 83 – E-2 airworthy at the Old Rhinebeck Aerodrome in Red Hook, New York.[14][15]
- 283 – E-2 airworthy at the Kelch Aviation Museum in Brodhead, Wisconsin.[16][17]
Specifications (Taylor E-2 Cub)
[edit]
Data from [1]
General characteristics
- Crew: one
- Capacity: one passenger
- Length: 22 ft 6 in (6.86 m)
- Wingspan: 35 ft 2 in (10.72 m)
- Height: 6 ft 6 in (1.98 m)
- Wing area: 184 sq ft (17.1 m2)
- Empty weight: 510 lb (231 kg)
- Max takeoff weight: 970 lb (440 kg)
- Powerplant: 1 × Continental A40-2 4-cylinder air-cooled horizontally-opposed piston engine, 35 hp (26 kW)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 80 mph (130 km/h, 70 kn)
- Cruise speed: 70 mph (110 km/h, 61 kn)
- Range: 225 mi (362 km, 196 nmi)
- Service ceiling: 12,000 ft (3,700 m)
- Rate of climb: 400 ft/min (2.0 m/s)
- Wing loading: 6 lb/sq ft (29 kg/m2)
- Power/mass: 0.04 hp/lb (0.066 kW/kg)
See also
[edit]Related development
Aircraft of comparable role, configuration, and era
References
[edit]- Notes
- ^ a b King, H.F. (1969). Milestones of the Air (McGraw-Hill ed.). New York: Jane's All the World's Aircraft Publishing Company. p. 72.
- ^ Francis, Devon (1973). Mr. Piper and His Cubs. Ames, Iowa: Iowa State University Press. pp. 23–24. ISBN 0-8138-1250-X.
- ^ Bowers, Peter M. (1993). Piper Cubs (1st ed.). TAB Books. p. 13. ISBN 0-8306-2170-9.
- ^ Peperell, Roger W.; Smith, Colin M. (1987). Piper Aircraft and their forerunners. Air-Britain (Historians) Limited. p. 21. ISBN 0-85130-149-5.
- ^ "Taylor E-2 Cub". Canada Aviation and Space Museum. Retrieved May 28, 2024.
- ^ "Airframe Dossier - Taylorcraft E-2 Cub, c/n 0289, c/r C-GCGE". Aerial Visuals. Retrieved May 28, 2024.
- ^ "Taylor E-2 Cub". Western Antique Aeroplane & Automobile Museum. Retrieved May 28, 2024.
- ^ "FAA Registry [N12627]". Federal Aviation Administration. U.S. Department of Transportation. Retrieved May 28, 2024.
- ^ "FAA Registry [N12628]". Federal Aviation Administration. U.S. Department of Transportation. Retrieved May 28, 2024.
- ^ Lilley, Joseph W. "1932 E-2 Taylor 'The Cub'". Western North Carolina Air Museum. Retrieved May 28, 2024.
- ^ "FAA Registry [N12664]". Federal Aviation Administration. U.S. Department of Transportation. Retrieved May 28, 2024.
- ^ "1932 Taylor E-2 Cub". Golden Age Air Museum. Retrieved May 28, 2024.
- ^ "FAA Registry [N13146]". Federal Aviation Administration. U.S. Department of Transportation. Retrieved May 28, 2024.
- ^ "Taylor E-2 Cub". Old Rhinebeck Aerodrome. Retrieved May 28, 2024.
- ^ "FAA Registry [N951V]". Federal Aviation Administration. U.S. Department of Transportation. Retrieved May 28, 2024.
- ^ "1930 Taylor E-2 "Cub #1"". Kelch Aviation Museum. Retrieved May 28, 2024.
- ^ "FAA Registry [N10547]". Federal Aviation Administration. U.S. Department of Transportation. Retrieved May 28, 2024.
- Sources
- Bowers, Peter M. (1993). Piper Cubs. McGraw Hill. ISBN 0-8306-2170-9.
- "The Piper Cub" by Roger Guillemette, US Centennial of Flight Commission, retrieved December 6, 2005
- "Szekely SR-3 L" Old Rhinebeck Aerodrome, retrieved December 6, 2005
External links
[edit]- Old Rhinebeck Aerodrome's Taylor E-2 Cub page
- Taylor E-2 Cub - Holcomb's Aerodrome
- Taylor Cub - A version of the original E-2 Cub manufactured by the Taylorcraft Company
- ATC 455, the FAA type certificate data sheet for the Taylor E-2.
Taylor Cub
View on GrokipediaHistory
Origins and development
Clarence Gilbert Taylor, born on September 25, 1898, in Rochester, New York, was a self-taught aeronautical engineer who developed a passion for aviation early in life.[5][6] As a teenager during World War I, he designed and constructed his first monoplane in the attic of his family home, assembling components separately due to space constraints, though it never flew successfully.[7] Following the war, Taylor pursued various aviation-related projects, including work as a mechanic and further experimentation with aircraft designs, honing his skills without formal training.[8] In September 1927, Taylor co-founded the Taylor Brothers Aircraft Manufacturing Company in Rochester, New York, with his brother Gordon S. Taylor, initially to produce affordable small aircraft for the burgeoning private flying market.[9] The brothers' first product was the 1928 Taylor Chummy (also known as the A-2 or D-2), a two-seat, high-wing monoplane powered by a 90 hp Anzani radial engine, intended for utility and training but priced too high at around $4,000 for widespread adoption during economic uncertainty.[10] In 1930, facing limited success and seeking better opportunities, the company relocated to Bradford, Pennsylvania, where Taylor began work on a more economical successor.[11] The Taylor Cub emerged as a direct evolution from the Chummy, redesigned as a smaller, simpler, and cheaper single-engine parasol monoplane aimed at personal ownership by amateur pilots.[12] The prototype, designated E-2, featured tandem seating, fabric-covered construction, and an emphasis on ease of handling to appeal to novice flyers. Its first flight occurred on September 12, 1930, powered by an underpowered 20 hp Brownbach Tiger Kitten Moth engine, which proved inadequate and was soon replaced by a 40 hp Salmson radial for better performance.[13] The aircraft received an initial "memo" type certificate (No. 2-358) from the U.S. Department of Commerce on June 15, 1931, followed by full Approved Type Certificate A-455 on November 7, 1931.[2] Taylor's design goals for the Cub centered on affordability and accessibility amid the Great Depression, pricing the E-2 at $1,325 to serve as a light utility aircraft for private pilots seeking an easy-to-fly option for recreation and basic transport.[14] This focus on simplicity and low cost marked a pivotal shift toward democratizing aviation for everyday users.Production and transition to Piper
In 1931, following the bankruptcy of Taylor Brothers Aircraft Manufacturing Company, a group of Bradford, Pennsylvania, businessmen, including oil executive William T. Piper, acquired the assets and reorganized the firm as the Taylor Aircraft Company, establishing a factory in Bradford to resume operations.[10] The company focused on producing the newly certified E-2 Cub, a more affordable successor to the higher-priced Chummy, amid the economic constraints of the Great Depression, which had severely limited sales of luxury-oriented aircraft like the Chummy and contributed to widespread industry slumps. Between 1931 and February 1936, Taylor Aircraft built approximately 353 E-2 Cubs, with initial sales of 22 units in 1931 at a price of $1,325, with sales increasing significantly by 1935 when the cost had increased to $1,475 due to engine upgrades and inflation.[2][10] The Cub's design as a cost-reduced alternative helped sustain production during the Depression, but financial pressures persisted until Piper, who had been an early investor since the late 1920s, increased his stake in 1935 to become the majority owner and effective controller of the company, with C. Gilbert Taylor remaining as nominal president.[15][8] In 1936, production shifted to the improved J-2 Cub variant, achieving over 1,200 units by mid-1937, while early recognition came from feats like the 1937 women's altitude record of 16,800 feet set by Beverly Dodge and a passenger in a Szekely-powered Taylor H-2.[10][16] Tensions arose from design disagreements and Taylor's prolonged illness in 1935, culminating in his departure in December 1935 after ongoing disputes with Piper; Taylor subsequently founded the Taylorcraft Aircraft Corporation in Alliance, Ohio.[17][8] A factory fire in Bradford that March 1937 accelerated the transition, prompting relocation to Lock Haven, Pennsylvania, and the official renaming to Piper Aircraft Corporation in November 1937.[18] Under Piper, Cub production continued seamlessly with the J-2, evolving into the J-3 model in 1938 featuring an enclosed cowl and a 40-horsepower Continental A-40 engine for improved performance and manufacturability.[19] The entire Cub series, encompassing Taylor- and Piper-built aircraft, ultimately exceeded 23,000 units, establishing it as a cornerstone of affordable general aviation.[10]Design
Airframe and construction
The Taylor Cub features a high-wing parasol monoplane configuration with two open cockpits arranged in tandem, positioning the pilot forward and the passenger aft for optimal visibility and control. It employs fixed tailwheel landing gear, consisting of rubber shock cords for absorption on rough surfaces, enhancing its suitability for operations from unprepared grass fields or short runways. The open cockpits provide unobstructed forward and peripheral views, a deliberate design choice to aid in low-altitude flying and instruction.[2][14] The airframe measures 22 ft 3 in (6.78 m) in length, with a wingspan of 35 ft 3 in (10.74 m), a height of 6 ft 6 in (1.98 m), and a wing area of 184 sq ft (17.1 m²). The fuselage is constructed from welded tubular steel tubing, covered in doped fabric for a lightweight yet durable structure that resists corrosion and simplifies maintenance. The wings are wooden, built with spruce spars and aluminum-alloy ribs, also fabric-covered, and utilize the USA-35B airfoil to promote gentle stall characteristics and efficient low-speed handling. Strut-braced with V-struts and internal wire bracing, the wings contribute to the aircraft's overall aerodynamic simplicity and structural integrity.[2][3][14] Emphasizing affordability and ease of assembly, the Taylor Cub's construction was intended for production in small shops or by individual builders, leveraging readily available materials and straightforward techniques like welding and doping. The empty weight is approximately 525 lb (238 kg), underscoring its lightweight design that facilitates short takeoffs and landings while maintaining stability. This approach to airframe design prioritized ruggedness for recreational and training use without complex manufacturing processes.[3][20][14]Powerplant and performance
The initial prototype of the Taylor Cub, first flown on September 12, 1930, was powered by a 20 hp (15 kW) Brownbach Tiger Kitten two-stroke engine, which proved severely underpowered and was promptly replaced after the aircraft nosed over during testing.[13] The production E-2 model featured a 37 hp (28 kW) Continental A-40-2 four-cylinder inline, air-cooled, direct-drive engine.[11][13] This powerplant provided reliable operation for the lightweight airframe, enabling the Cub's reputation as an accessible trainer. Performance characteristics of the E-2 included a maximum speed of 80 mph (129 km/h), a cruise speed of 68 mph (109 km/h), and a stall speed of 28 mph (45 km/h), with a range of 205 mi (330 km).[10] Fuel capacity consisted of 9 US gal (34 L) stored in wing tanks.[14] The aircraft utilized a fixed-pitch wooden propeller of 6 ft 6 in (1.98 m) diameter to optimize low-speed efficiency.[2] The Cub's handling was notably stable and forgiving, with reluctance to stall and excellent low-speed manners that suited novice pilots; it achieved a short takeoff run of approximately 150 ft (46 m), aided briefly by the airframe's wire bracing for enhanced slow-flight stability.[13][4][21]Variants
E-2 Cub
The E-2 Cub served as the primary production variant of the Taylor Cub series, representing the baseline model manufactured from 1931 to 1936 and equipped with a 37 horsepower Continental A-40 four-cylinder engine.[10] This configuration evolved from an earlier prototype tested in 1930, establishing the foundational design for subsequent light aircraft.[22] The aircraft featured a simple, high-wing parasol design with a fabric-covered tubular steel fuselage and wooden wings, optimized for affordability and ease of maintenance during the economic challenges of the Great Depression.[2] Approved Type Certificate (ATC) No. 455 was issued by the U.S. Department of Commerce on November 7, 1931, certifying the E-2 for production with a useful load of 400 pounds.[10] As the most numerous variant, the E-2 accounted for the majority of the 353 total Taylor Cubs built, all in a standard two-seat tandem open-cockpit arrangement suitable for pilot training and recreational flying.[20] Its construction emphasized lightweight components, including initial Grade A cotton fabric covering applied directly over the airframe without the structural reinforcements—such as additional bracing wires or metal fittings—added in later Piper iterations.[2] The E-2's cockpit included basic instrumentation limited to an airspeed indicator, altimeter, and tachometer, reflecting its role as an entry-level trainer without advanced avionics. Priced at $1,325 upon its 1931 introduction, the aircraft targeted private owners and flight schools seeking a reliable, low-cost option amid widespread economic hardship, with sales reaching 22 units in the first year alone.[2] By 1935, production had ramped up to over 200 units annually, underscoring its appeal in the burgeoning general aviation market.[2]Other variants
The F-2 variant, produced in 1934, substituted the standard inline engine with a 40 hp Aeromarine AR-3-40 three-cylinder radial for improved cooling in hot climates, receiving Approved Type Certificate #525 on February 16, 1934; approximately 33 examples were built.[10] The G-2 employed custom Taylor-designed engines in limited numbers as an experimental effort to enhance reliability, with only a single proof-of-principle prototype completed.[10][23] The H-2 variant utilized a 35 hp Szekely SR-3-35 three-cylinder radial engine and was awarded Approved Type Certificate #572 on May 28, 1935, though fewer than 10 were produced owing to persistent engine reliability problems.[10] As Taylor's final variant, the J-2 was manufactured from 1935 to 1936 with an upgraded 40 hp Continental A-40-4 inline-four engine, a widened fuselage for better cabin space, and an enlarged rudder for improved stability; limited numbers were constructed under Taylor, facilitating the design's transition to Piper Aircraft production, where over 1,200 additional units were built.[10][24] Overall, the E-2 remained the primary production model, while these other variants were produced in small numbers collectively under Taylor.[10]Operational history
Civilian use
The Taylor E-2 Cub emerged as an affordable personal aircraft and primary trainer, appealing to individual owners and small flight schools across the United States in the 1930s. Its simple design and forgiving handling characteristics made it ideal for novice pilots learning to fly, fostering the expansion of recreational and instructional aviation during the economic constraints of the Great Depression.[1] With production spanning from 1930 to 1936, approximately 350 units were built, the majority sold to civilians for private use and club operations, significantly contributing to the popularization of light aircraft ownership at a time when aviation was becoming accessible to the broader public.[3] The E-2 Cub participated in notable civilian achievements, including air races and tours that highlighted its reliability in competitive sport aviation.[22] After Taylor Aircraft's transition to Piper in 1936, the Cub's legacy persisted in civilian hands through evolved models like the J-2 and J-3, but the original E-2 remained prized by early private aviators for its unpretentious role in general aviation. Its open cockpit and 37-horsepower engine, while enhancing simplicity and low-speed stability, restricted operations in adverse weather and limited cruising speeds to around 70 mph.[19][4]Military operators
The Taylor Cub experienced limited military adoption, reflecting its primary design as a civilian trainer and utility aircraft. No additional military operators or exports have been documented for the E-2 Cub, resulting in no confirmed units entering service worldwide. This modest uptake stemmed from the Cub's emphasis on simplicity and affordability for non-military applications, rather than the durability required for broader tactical employment.Preservation
Surviving aircraft in Canada
The Canada Aviation and Space Museum in Ottawa houses a preserved Taylor E-2 Cub, registered as C-GCGE, which was built in August 1935 by Taylor Aircraft Company.[3] This aircraft, acquired by the museum in June 1985, underwent restoration in 1975 by Garth Elliot, including replacement wings after a fire, and is now displayed in static condition in the Reserve Hangar, highlighting its role as a precursor to the Piper J-3 Cub and early Canadian imports of light aircraft in the 1930s.[3] It represents the initial cross-border interest in Taylor's designs, with only three E-2 Cubs imported to Canada before World War II.[3] At the Reynolds-Alberta Museum in Wetaskiwin, Alberta, a 1936 Taylor J-2 Cub variant, registered CF-BEE with serial number 1064, is preserved as part of the aviation collection.[25] This static display exemplifies the improved J-2 model, which featured refinements over the E-2 and influenced subsequent Piper production, underscoring the design's enduring appeal in Canadian aviation history.[25] One airworthy example survives in private hands north of Guelph Airpark, Ontario: a 1935 Taylor E-2 Cub registered CF-ANT, restored in the 1990s by the Tiger Boys group after damage in 1940.[26] As the first Taylor Cub to fly in Canada, it demonstrates the feasibility of maintaining these early aircraft in flying condition and their ongoing significance in recreational and historical flying.[26] No additional airworthy Taylor Cubs are confirmed in Canada, with preservation efforts centered on static museum exhibits from 1930s-era imports.[3]Surviving aircraft in the United States
Several Taylor E-2 Cubs survive in the United States, primarily preserved in museums and a few maintained in airworthy condition by private owners, reflecting the aircraft's historical significance as an early light trainer from the Taylor Aircraft Company in Bradford, Pennsylvania.[27] One notable example is the 1932 E-2 Cub (serial number 54) at the Golden Age Air Museum in Bethel, Pennsylvania, which was acquired in 1991 after 50 years in storage and restored to original condition over three years, remaining airworthy and highlighting the Bradford production heritage.[27] This aircraft, powered by a 37-horsepower Continental A-40 engine, exemplifies the type's role in early flight training and is one of the oldest surviving E-2s.[27] At the Kelch Aviation Museum in Brodhead, Wisconsin, a replica of the 1930 E-2 "Cub #1" prototype is on static display, rebuilt by museum founder Al Kelch with assistance from designer C.G. Taylor to match the original factory test flight appearance, including a French AD-9 Salmson 40-horsepower radial engine and a map case from the actual prototype.[1] This exhibit represents the first production example of the parasol monoplane design that influenced later Cubs.[1] The Western North Carolina Air Museum in Hendersonville, North Carolina, houses a 1932 E-2 Cub equipped with a 37-horsepower Continental A-40-2 engine, restored and maintained in flyable condition as part of its collection of operational vintage aircraft.[2] Similarly, the Western Antique Aeroplane & Automobile Museum in Hood River, Oregon, displays a 1931 E-2 Cub, the seventh production airframe, restored between 2007 and 2008 with its first post-restoration flight on May 15, 2008, underscoring ongoing efforts to keep these early models aloft.[20] The Old Rhinebeck Aerodrome in Red Hook, New York, operates an airworthy 1934 E-2 Cub (serial number 83, registration NC951V), restored and flown by private owner Ken Cassens as part of the aerodrome's collection.[4][28] A 1935 E-2 Cub (registration NC15045) is preserved on static display at the Gig Harbor Vintage Aero Museum in Gig Harbor, Washington.[29][30] In September 2025, a 1932 E-2 Cub at the Shannon Air Museum in Fredericksburg, Virginia—the oldest remaining flying example—returned to flight after a restoration spanning over 40 years.[31] A 1932 E-2 Cub (construction number 33, registration NC12628), originally from York County, Pennsylvania, and owned by G.G. Naugle, was restored prior to 2016 and exhibited at the Virginia Aviation Museum in Richmond, Virginia, where it represented local aviation history from promotional flights in the 1930s; following the museum's closure in 2016, as of 2025 its location remains part of unresolved relocation efforts for the collection.[32] An estimated 5 to 10 Taylor E-2 Cubs survive in the United States, mostly early E-2 variants, with additional airworthy examples in private hands concentrated in Pennsylvania and the Midwest, such as NC951V (serial 83) actively flown by a private owner.[33] Preservation initiatives, including involvement from the Experimental Aircraft Association (EAA) through events like AirVenture showcases of Continental A-40-powered aircraft, and support from the Piper Aviation Museum in Lock Haven, Pennsylvania, aid in maintaining these rarities despite challenges like parts scarcity for vintage components such as engines and fabric coverings.[34][35][36]Specifications
General characteristics (Taylor E-2 Cub)
The Taylor E-2 Cub features the following general characteristics:| Characteristic | Specification |
|---|---|
| Crew | 1 pilot [http://www.westernnorthcarolinaairmuseum.com/1932-e-2-taylor-cub.html] |
| Capacity | 1 passenger [http://www.westernnorthcarolinaairmuseum.com/1932-e-2-taylor-cub.html] |
| Length | 22 ft 3 in (6.78 m) [https://ingenium.ca/aviation/en/collection-highlight/taylor-e-2-cub/] |
| Wingspan | 35 ft 3 in (10.74 m) [https://ingenium.ca/aviation/en/collection-highlight/taylor-e-2-cub/] |
| Height | 6 ft 6 in (1.98 m) [https://ingenium.ca/aviation/en/collection-highlight/taylor-e-2-cub/] |
| Wing area | 184 sq ft (17.1 m²) [http://www.westernnorthcarolinaairmuseum.com/1932-e-2-taylor-cub.html] |
| Empty weight | 525 lb (238 kg) [https://ingenium.ca/aviation/en/collection-highlight/taylor-e-2-cub/] [https://www.waaamuseum.org/collections/airplanes/178-Taylor-E-2-Cub] |
| Gross weight | 925 lb (419 kg) [https://ingenium.ca/aviation/en/collection-highlight/taylor-e-2-cub/] [https://www.waaamuseum.org/collections/airplanes/178-Taylor-E-2-Cub] |
| Fuel capacity | 12 US gal (45 L) [] |
| Powerplant | 1 × Continental A-40-2 4-cylinder inline, 37 hp (28 kW) [http://www.westernnorthcarolinaairmuseum.com/1932-e-2-taylor-cub.html] [https://ingenium.ca/aviation/en/collection-highlight/taylor-e-2-cub/] |
| Propeller | 2-bladed fixed-pitch wooden [] |
Performance (Taylor E-2 Cub)
The Taylor E-2 Cub delivered reliable performance suited to training and recreational flying, characterized by modest speeds, good short-field capabilities, and sufficient endurance for local operations. Powered by a single Continental A-40-2 inline-four engine rated at 35–37 hp (26–28 kW), the aircraft emphasized simplicity and low operating costs over high performance.[20] Its flight envelope included a maximum speed of 80 mph (129 km/h, 70 kn) at sea level and a cruise speed of 65 mph (105 km/h, 57 kn), enabling efficient travel at economic power settings.[22][20] The stall speed was 30 mph (48 km/h, 26 kn), contributing to forgiving handling during low-speed maneuvers.[14] Endurance was supported by a range of 225 mi (362 km, 196 nmi), while climb and altitude performance allowed access to typical training altitudes, with a service ceiling of 12,000 ft (3,700 m) and a rate of climb of 450 ft/min (2.3 m/s).[22] Short-field operations were a strength.[37]| Performance Metric | Value |
|---|---|
| Maximum speed | 80 mph (129 km/h, 70 kn) at sea level |
| Cruise speed | 65 mph (105 km/h, 57 kn) |
| Stall speed | 30 mph (48 km/h, 26 kn) |
| Range | 225 mi (362 km, 196 nmi) |
| Service ceiling | 12,000 ft (3,700 m) |
| Rate of climb | 450 ft/min (2.3 m/s) |
