San Jose CA.
USA
Built the Parso Solo Sport in 1933.
San Jose CA.
USA
Built the Parso Solo Sport in 1933.

Major August von Parseval’s Aeroboat of 1909 – “Das Aeroplan”, was taken to Plau, in Mecklenburg, where it was to be tested along the shore of the lake in 1910.
The first test of August von Parseval’s seaplane was on April 6, 1910 with pilot Oberingenieur Blochmann, but the plane would not leave the water. On April 14 the machine capsized in a storm and sank. The pilot was saved and the machine salvaged and modified. The biggest changes were straight wings (original wing tips were in V-shape), extra water planes and a triangular fuselage, instead of rectangular. Since the machine couldn’t start from water a Wright-like construction was built, with a trolley on rails. On October 7, 1910 a successful first attempt was made with the starting device. The machine flew at 3 meters for a length of 100-800 meters. A second flight on October 15, 1910 was very successful as the machine flew 3-4 kilometers. The landing on the water was not smooth, so Blochmann was lightly injured. Parseval realized that the machine could never start from the water and ended development.
The machine has a span of 14 metres, while it is 7 metres long and is fitted with a motor of 114-h.p.

Engine: VW 2100cc, 80 hp
HP range: 80-150
Height: 5.42 ft
Length: 15.25 ft
Wing span: 23 ft
Wing area: 74 sq.ft
Weight empty: 625 lbs
Gross: 1200 lbs
Fuel cap: 25 USG
Speed max: 200 mph
Cruise: 160 mph
Range: 1000 sm
Stall: 55 mph
ROC: 1200 fpm
Service ceiling: 20,000 ft
Seats: 2
Landing gear: nose wheel
1995: 1125 S.W. 49th Terr., Plantation, FL 33317, USA.
Offered the Parrish Dart aircraft
A two-seat training monoplane.
Brasil
The works at Rio de Janeiro’s military air base built Waco biplanes for Brazilian Air Force mail services in late 1930s, plus Muniz two-seat training monoplane.

1929
Parasol
Engine: 1 x 226hp Armstrong Siddeley Lynx IV
Max take-off weight: 1302 kg / 2870 lb
Empty weight: 1008 kg / 2222 lb
Wingspan: 12.80 m / 42 ft 0 in
Length: 9.24 m / 30 ft 4 in
Height: 2.89 m / 10 ft 6 in
Wing area: 27.31 sq.m / 293.96 sq ft
Max. speed: 177 km/h / 110 mph
Ceiling: 8900 m / 29200 ft
Crew: 2

1927

Imp
Engine: 1 x 80hp Armstrong-Siddeley Genet II
Max take-off weight: 599 kg / 1321 lb
Empty weight: 386 kg / 851 lb
Wingspan: 7.77 m / 26 ft 6 in
Length: 6.45 m / 21 ft 2 in
Height: 2.33 m / 8 ft 8 in
Wing area: 16.35 sq.m / 175.99 sq ft
Max. speed: 164 km/h / 102 mph
Cruise speed: 128 km/h / 80 mph
Crew: 2

A submarine based sea surveillance aircraft, United Kingdom, 1926
Engine: Armstrong Siddeley Moongoose III C, 148 hp
Length: 22.507 ft / 6.86 m
Wingspan: 28.412 ft / 8.66 m
Wing area: 174.377 sq.ft. / 16.2 sq.m
Max take off weight: 1949.2 lb / 884.0 kg
Weight empty: 1314.2 lb / 596.0 kg
Max. speed: 98 kt / 182 km/h
Wing loading: 11.28 lb/sq.ft / 55.0 kg/sq.m
Range: 216 nm / 400 km
Endurance: 2 h
Crew: 2


1923
Possum
Engine: 1 x 450hp Napier Lion
Max take-off weight: 2858 kg / 6301 lb
Wingspan: 14.02 m / 46 ft 0 in
Length: 11.89 m / 39 ft 0 in
Height: 4.20 m / 14 ft 9 in
Wing area: 72.20 sq.m / 777.15 sq ft
Max. speed: 170 km/h / 106 mph
Cruise speed: 142 km/h / 88 mph
Armament: 2 x 7.7mm
Crew: 3