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The Heath Parasol is an American single or two seat,[1] open-cockpit, parasol winged, homebuilt monoplane.

Heath Parasol
Parasol, photographed in 1935.[Notes 1]
Role	Home-built aircraft Type of aircraft
National origin	United States
Manufacturer	Heath
Designer	Edward Bayard Heath
First flight	1926
Introduction	Parasol (1926); 1927 (Super Parasol); 1930 (V Parasol; 1931 (LN Parasol)
Primary user	Recreational flyers

Design and development

In 1926, Edward Bayard Heath, a successful American air racer and the owner of an aircraft parts supply business, built the first example of the Heath Parasol, a small, single seat parasol winged airplane using surplus wings from a Thomas-Morse S-4, a World War One fighter trainer, mounted above a steel-tube structure fuselage and powered by a Henderson four-cylinder motorcycle engine.[1] This was the prototype for a series of single and two-seat recreational craft that utilized the Clark Y airfoil. In 1929 Modern Mechanix magazine published the plans in a series[2]^{[failed verification]} and the plans were reprinted in their "1930 Flying & Gliding Manual," which in turn has been reprinted periodically by the EAA (Experimental Aircraft Association).[1]

Although Heath died in 1931 his Parasol designs remained extremely popular, being economical to build and operate as well as easy to fly. Subsequently, the Heath Company of St. Joseph / Benton Harbor Michigan sold nearly 1,000 kits on an installment basis.[3] Fewer than 50 aircraft were factory built, but several hundred were completed and flown by homebuilders during the Great Depression. Heath is remembered today for having helped pioneer the homebuilt aircraft industry and for having introduced the kit concept of packaging the materials needed to build an aircraft.

When it ceased producing aircraft kits to concentrate on electronics (Heathkit), the Heath Company sold the ATC (CAA Aircraft Type Certificate) for the LNA-40 (ATC-487) [4] to the EAA who continued to sell original plans to potential homebuilders.[1]

Except for the prototype, the wings consist of two solid spruce spars, built up wooden ribs, compression struts, and internal drag and anti-drag bracing. The Parasol's empennage is built of wood, and externally braced. Depending on the model, the fuselage was built of wood, bolted steel tube, or welded steel tube.[3] Wing, empennage, and fuselage are fabric covered. Two five gallon fuel tanks are typically installed at the root end of each wing, the fuel being gravity fed, sometimes to a small collector tank behind the firewall. The only tools necessary to assemble one of the Parasol kits were a pair of small pliers, screwdriver, hacksaw (with plenty of blades), hammer, small hand drill, chisel, center punch, file and drill.^{[citation needed]}

A variety of powerplants could be fitted, including the factory-supplied converted Henderson Motorcycle engine (viz. 25 hp (19 kW) Heath-Henderson B-4). Post-war, the VW boxer engine was used as well.[1]

Production of an early version was undertaken as early as 1931, in Australia, by the Adcock-Heath Company.

Variants

Home building encourages local variations that blur type definitions for non-certificated versions.

Prototype

Used the 24 ft 0 in (7.32 m), wing from a Thomas-Morse S-4C "Tommy."

CA-1 Parasol

Wingspan of 24 ft 0 in (7.32 m), with square tips. Parallel wing struts. First built 1928. Not Certificated (nor required to be). One seat. 260 pound empty weight. Heath B-4 engine, 27 hp at 2800 rpm.[1][5]

CA-1A Super Parasol

Wingspan of 25 ft 0 in (7.62 m), with rounded tips. Parallel wing struts. First built 1929. Not Certificated (nor required to be). One seat. 260 pound empty weight. Heath B-4 engine, 27 hp at 2800 rpm.[1][6]

V-Parasol

Span 25 ft 0 in (7.62 m), various more powerful engines and V-form wing struts.[7]

LNB-4 Parasol

Wing span increased to 31 ft 5 in (9.58 m). N-form struts. One or two seat. 450 pound empty weight. Heath B-4 engine, 25 hp at 2800 rpm. Certificated (CAA, ATC-456)[4] June 3, 1932.

LNA-40 Parasol

Wingspan of 31 ft 5 in (9.58 m), V-form struts. One or two seats. 465 pound empty weight. Door moved to opposite side of fuselage to accommodate hand-propping the clockwise turning 37 hp (28 kW) (at 2550 rpm) Continental A40 powerplant. First built 1932. CAA type certificated (ATC-457) June 3, 1932.[4][1][8]

Survivors

• There is a LNB-4 Parasol on display at the New England Air Museum, Bradley International Airport, Windsor Locks, CT.[9]
• The Museum of Flight, Seattle, WA, owns a Parasol. It is currently at their Restoration Center in Everett, WA.[10]

Specifications (Super Parasol)

Data from Aviation[11]

General characteristics

• Crew: 1
• Length: 17 ft 0 in (5.18 m)
• Wingspan: 25 ft 0 in (7.62 m)
• Height: 4 ft 6 in (1.37 m)
• Wing area: 110 sq ft (10 m²)
• Empty weight: 280 lb (127 kg)
• Gross weight: 580 lb (263 kg)
• Fuel capacity: 9 US gal (7.5 imp gal; 34 L)
• Powerplant: 1 × Heath , 27 hp (20 kW)

Performance

• Maximum speed: 70 mph (110 km/h, 61 kn)
• Cruise speed: 65 mph (105 km/h, 56 kn)
• Stall speed: 32 mph (51 km/h, 28 kn)
• Range: 270 mi (430 km, 230 nmi)
• Service ceiling: 12,500 ft (3,800 m)
• Rate of climb: 500 ft/min (2.5 m/s)

See also

• Heathkit descendant company, maker of electronic kits

Aircraft of comparable role, configuration, and era

• Dormoy Bathtub
• Aerotique Parasol
• Fisher FP-505 Skeeter
• Loehle Sport Parasol
• Pietenpol Air Camper
• Pop's Props Cloudster
• Pop's Props Zing
• Powell P-70 Acey Deucy
• RagWing RW5 Heath Replica

Notes

References

• Berkeley, John (April 2021). "Parasol's Progress". Aeroplane. Vol. 49, no. 4. pp. 90–96. ISSN 0143-7240.

Further reading

• Sport Flying Quarterly, Vol.9 No.7, 1975, pp 54–63.

External links

• LNB-4 at EAA
• The Heath Story
• LNA-40 at Mid-America Air Museum
• V Parasol
• Museum of Flight, Everett WA
• "1932 Ad for Heath home built aircraft" Popular Mechanics, August 1932
• Reprint of Peter M. Bower's January 1982 AOPA Pilot article.
• Photo and caption.

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