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

Taylor Tater Bug

In 1963 Merton Taylor built a single place low-wing cabin monoplane Tater Bug registered N1052Z. Using an NACA 4309 – NACA 4309 wing, the first flight was in Febuaray 1963.

Engine: Continental C-85-12, 85hp
Wing span: 18’0″
Length: 17’5″
Useful load: 330 lb
Max speed: 170 mph
Cruise speed: 150 mph
Stall: 80 mph
Range: 550 mi
Seats: 1

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

Taylor JT-2 Titch

The Taylor JT.2 Titch was designed in 1964 to meet Rollason’s Midget Racer competition, placed second overall. A prototype built by John Taylor was first flown at Rochford on 22 January 1967 with a Continental C85-12F engine. It crashed in May 1987, killing Taylor. The plans then being sold by his widow.

Titch G-BCSY at Sywell 1975

The Taylor Titch has a reputation as a pleasant-to-fly aerobatic plane. Its stall occurs at a very high angle of attack and is straightforward, with no wing drop and a height loss of only 50 feet. This single-place monoplane features all-wood wings with plywood and fabric covering. Its fuselage is also an all-wood structure that includes double-curvature plywood covering and aluminum cockpit side panels. When the low-powered Taylor Monoplane became known in the United States, requests were made for permission to fit larger engines than the design permitted. This led to the introduction of the Titch. The Titch is stressed for any engine from 40 to 90 hp, the only provision being a reposition of the engine bulkhead for engines of 65 hp or more. This allows for the use of VW, Lycoming or Continental powerplants.

Engine: Continental, 85 hp
HP range: 60-100
Speed max: 200 mph
Cruise: 160 mph
Range: 380 sm
Stall: 48 mph
ROC: 1600 fpm
Take-off dist: 350 ft
Landing dist: 900 ft
Service ceiling: 18,000 ft
Fuel cap: 10 USG
Weight empty: 500 lbs
Gross: 760 lbs
Height: 4.8 ft
Length: 16.7 ft
Wing span: 18.9 ft
Wing area: 68 sq.ft
Seats: 1
Landing gear: tail wheel

Engine: VW 2100
Cruise: 115 mph
ROC: 800 fpm
Range: 250 sm
Span: 18 ft 9 in
Length: 16 ft 1.5 in
Empty wt: 455 lbs
Max wt: 710 lbs

Taylor JT-1 Monoplane

Designed by John Taylor, the Monoplane is a single seat, cantilever, low wing. acrobatic aircraft built with the object of producing an airframe for not more than £100 Sterling. The wing is a constant chord structure with an RAF 48 aerofoil section, and consists of a centre section and outer panels. Each panel has two spruce and plywood spars, wooden ribs and a plywood covered leading edge D nose, the remainder of the wing being fabric covered. Split trailing edge flaps are fitted. The fuselage is a conventional wooden structure hav¬ing spruce longerons and frames and plywood covering. The wing centre section is built integral with the fuselage. The fin and tailplane are plywood covered wooden structures, while the rudder and elevators are fabric covered wooden structures. The main undercarriage consists of cantilever legs fitted with coil springs for shock absorption. The wheels have Avro Anson tailwheel tyres. A leaf spring tail skid with a steerable skid pad is fitted. A 6 Imp. gallon fuel tank is installed behind the firewall. The prototype flew with a 37 h.p. JAP engine, but converted Volkswagen engines are also suitable. Since the first prototype flew in June 1960, no modifications of any kind have been incorporated.

Variation: Ladd Taylor Chihuahua

Gallery

Engine: VW 1500cc
HP range: 40-60
Speed max: 115 mph
Cruise: 100 mph
Range: 290 sm
Stall: 35 mph
ROC: 950 fpm
Take-off dist: 350 ft
Landing dist: 750 ft
Service ceiling: 13,500 ft
Fuel cap: 7.5 USG
Weight empty: 430 lbs
Gross: 660 lbs
Height: 4.1 ft
Length: 15 ft
Wing span: 21 ft
Wing area: 76 sq.ft
Seats: 1
Landing gear: tail wheel

Engine: VW 1600cc
Cruise: 90 mph
Climb: 500 fpm
Range: 250 sm

Engine: JAP, 38 hp
Wing span: 21 ft 0 in (6.4m)
Wing Area: 72 sq. ft
Length: 15 ft 0 in (4.57 m)
Height: 4 ft 10 in (1.47 m)
Empty Weight: 400 lb
Max TO wt: 610 lb (276 kg)
Wing Loading: 8.5 lb/sq.ft
Max level speed: 105 mph (169 kph)
Cruise Speed: 92 mph
Stall Speed: 34 mph
Climb: 650 fpm
Range: 230 miles

Taylor Experimental

A two-seat cabin monoplane of all-metal construction with a high lattice girder with diagonal surface bracing.

Built at Hamsey Green, UK, by designer R.Taylor in 1936. Only one was built of three planned. The designer died in the crash of the prototype in 7 January 1937 on its first flight.

c/n TE.2 G-AEPX prototype built with Cirrus Minor I engine.
c/n TE.3 G-AEPY single seat, not built
c/n TE.4 G-AEPZ two-seater, not built
c/n G-AERA not built