Smith DSA-1 Miniplane / Sky Classic Aircraft Miniplane

The primary appeal of the Smith Miniplane is its small-size construction simplicity and open-cockpit. The fuselage framework is a conventional truss structure of welded steel tubing, faired to shape with wood stringers. As on most similar designs, the vertical stabilizer is welded up as part of the rear fuselage structure. The wings are made from spruce spars and ribs. Several engines can provide the power, the Continental from 65 to 85 hp or the Lycoming from 100 to 125 hp.

Smith DSA-1 Miniplane Article

The 1956 DSA-1 Miniplane model designation was for “Damn Small Aeroplane”. The prototype first flew on 29 October 1956.

Smith Miniplane N90P

There have been hundreds of the original Smith Miniplane Biplanes built and flying today. In 1996 plans cost US$140.

Sky Classic Aircraft introduced the 2000 version of the Smith Miniplane Biplane. Many of the parts and pieces on the aircraft were simplified to make it easier to build.

Changes include:
1) New wing fittings to simplify building.
2) Stretched the length of the fuselage by 5 inches to accommodate a larger person.
3) Stretched the width of the fuselage by 2 inches to accommodate a larger person.
4) Added a trim tab to the elevator.
5) Reshaped the rudder assembly to look more racy.
6) Added struts to the horizontal stabilizer to stop any cracking like the Pitts did.
7) Changed the wing foil to a NASA 23013. Good for aerobatics yet very stable with less drag.
8) Changed the wing angles of attack to fix an old problem on the old aircraft.
9) Reduced the rudder control speed to make it just a little easier to fly.
10) Aircraft plans on computer CAD so that they are easy to read.
11) Adding springs to the original type landing gear.

Gallery

Engine: 65- 85-hp Continental, 100-125-hp Lycoming.
Gross Wt: 1000 lb
Empty Wt: 616 lb.
Fuel capacity: 17 USG
Wingspan: 17’.
Length: 15’3”
Wing area: 100 sq.ft.
Top speed: 130 mph
Cruise: 122 mph.
Stall: 56 mph
Climb rate: 1600 fpm.
Ceil¬ing: 13,000 ft
Takeoff run: 450 ft
Landing roll: 500 ft
Range: 275 sm
Seats: 1

Sky Classic Aircraft Smith Miniplane 2000
Engine: Lycoming O-235, 100 hp
HP range: 90-120
Length: 15.5 ft
Wing span: 17 ft
Wing area: 100 sq.ft
Empty weight: 650 lb
Gross weight: 1000 lb
Fuel capacity: 15 USG
Cruise: 125 mph
Stall: 60 mph
Range: 90 sm
Rate of climb: 1000 fpm
Takeoff dist: 400 ft
Landing dist: 400 ft
Seats: 1
Cockpit width: 23 in
Landing gear: tailwheel

Sky Classic Aircraft Smith Sport Miniplane
Engine: Continental O-200, 100 hp
HP range: 90-120
Height: 5.5 ft
Length: 15.5 ft
Wing span: 100 ft
Wing area: 100 sq.ft
Empty weight: 650 lb
Gross weight: 1000 lb
Fuel capacity: 17 USG
Top speed: 135 mph
Cruise: 125 mph
Takeoff dist: 400 ft
Landing dist: 400 ft
Seats: 1
Landing gear: tailwheel

Smidley 1910 monoplane

Smidley began construction of his monoplane in 1909. It was described in the August 1909 NY Times as having large wings on either side of the central rectangular box. A smaller plane was above and in front, and a fixed semicircular plane was at the tail. Control was a semicircular device at the front with the halves of the semicircle moving together as elevator or separately. It was mounted on four small wheels that ran on rails. This was the 223 pound bamboo version with 18 hp engine. At some point the machine was changed to larger wheels for take-off from the ground and probably rebuilt in other ways. Smidley is credited with three aircraft and a completely rebuilt version of his first machine was reported to be ready for testing in a March 1910 Aeronautics. There is a small picture in November 1910 Aeronautics that shows a machine with the larger wheels, powered by an 18 hp 2-cylinder Stevens Duryea air-cooled engine, and the structure doesn’t look like bamboo. These machines were not powered by an electric motor, but a machine identified as Smidley’s third machine was displayed at a Harrisburg auto show in early 1910, where an electric motor was used to run the propeller in the exhibition. The picture is either the second version incomplete or the third, with the Duryea.

Engine: Duryea auto
Wingspan: 32’0″
Seats: 1

SMAN Petrel

A side by side two seat amphibious pusher biplane. A full detachable canopy that can be converted into an open cockpit with its own separate windshield.

The wings, boom and tail section detach for reduced storage and easy transportation.

Production of the Petrel was taken over by SMAN, who returned it to the market circa 1998.

Engine Rotax 618
Propeller Airplast 166DAS6275/3
Undercarriage retractable

Engine: Rotax 912, 80 hp
Wing span: 8.50 m
Wing area: 17 sq.m
MAUW: 450 kg
Fuel capacity: 53 lt
Max speed: 150 kph
Cruise speed: 130 kph
Minimum speed: 65 kph
Climb rate: 3.5 m/s
Seats: 2
Fuel consumption: 13 lt/hr
Price (1998): 245 000 F
Kit price (1998): 121 000 F sm