Van Pomer 1910 Biplane

In 1910 John Van Pomer built a single-seat copy of Curtiss A, one of the undocumented first attempts by early home-builders. Based on the then-popular Wright design, power was a 35hp Kemp engine.

A colleague, who as a teenager helped with the construction, said that he once had ridden on the wing in one of its short flights, which were always downhill and never involved turns.

The aircraft was located in a barn and recently restored to display condition at Empire State Aerospace Museum, Schenectady County airport NY.

Vance V-S-1 Baby Lark

The 1929 Vance V-S-1 Baby Lark was a single place, open cockpit biplane powered by a 27hp Kemp-Henderson. All-wood with fabric-covered wings, it was priced at $935, oe $1,180 with a 40hp Szekely engine.

Advertisements appear for a home-builders’ Vance project as either biplane or monoplane, with a complete kit offered for $180 less motor and dope, which is most likely a version of this model. It is unknown is if any were ever built and flown, but ads like these, catering to the flying craze of the late 1920s, were common in periodicals.

Engine: 27hp Kemp-Henderson
Wingspan: (upper) 20’0″ (lower) 21’10”
Length: 14’6″
Useful load: 250 lb
Max speed: 85 mph
Cruise speed: 70 mph
Stall: 24 mph
Range: 350 mi
Seats: 1

Vance M-1 Golden Arrow / V-1 Golden Arrow

One M-1 Golden Arrow was built in 1929, priced at $895. It was a single place, open cockpit, low wing monoplane of wooden construction with fabric-covered wings.

The V-1 Golden Arrow of 1929 was a single place, open cockpit, biplane, priced at $895. All-wood with fabric-covered wings, those built include N365H c/n 5.

M-1 Golden Arrow
Engine: 27hp Kemp-Henderson
Wingspan: 24’6″
Length: 15’9″
Useful load: 225 lb
Max speed: 80 mph
Cruise speed: 70 mph
Stall: 28 mph
Range: 250 mi
Seats: 1

V-1 Golden Arrow
Engine: 27hp Kemp-Henderson
Wingspan: 20’6″
Length: 14’6″
Seats: 1

Van Berkel 1919 seaplane

The 1919 Van Berkel seaplane is a twin-float seaplane, shown at the E.L.T.A. exhibition without engine, but intended for a Mercedes. The fuselage is built up of a light framework covered with three-ply wood. The ply-wood covering of the rear portion of the fuselage is continued outwards over the tail plane, which latter is built integral with the body. The fuselage is very deep at the rear, where it performs the function of a fin, no other vertical fin being fitted. The tail plane is at the top of the fuselage and the rudder has its balanced portion projecting below the stern.

The two floats, which are single step, are flat-bottomed as regards their front portion, but to the rear of the step the bottom gradually changes from flat to Vee bottom, finally corning to a point at the heel of the float. The construction is very similar to that of the fuselage, brass screws and nails being used throughout. The floats are fitted with water-tight bulkheads, detachable inspection doors being provided in the deck for examining the interior.

The wing bracing is only one pair of struts on each side. The upper plane is of slightly greater span than the bottom, and the inter-plane struts slope outwards. The lift and landing loads are taken by tubes sloping from the floats outward to the lower surface of the bottom plane at the points where occur the inter-plane struts. A speed of 155 km. per hour is estimated.