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

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

Slip Stream International Genesis / Innovation Engineering Genesis

Originally designed by Chuck Hamilton and prototyped in 1992, the Genesis is a two-place, roomy, side-by-side aircraft for a 2009. Available with a choice of dual yoke controls or center stick, and equipped with the standard Rotax 582, in solo configuration take-off roll is 100 feet, with a 250 foot landing roll and a climb rate of 1,000 fpm. The Genesis base 2009 Price also included dual 10-gallon wing tanks to provide for four hours endurance.

The series were originally produced by Innovation Engineering of Davenport, Iowa and then by SlipStream International of Wautoma, Wisconsin.

Innovation Engineering Genesis

The XL version has extended wings. The kit price in 1997 was US$12,900, including engine.

Optional are “Shark Series” amphibious floats. Computer designed to reduce drag and to provide for rapid hydroplaning, the “Shark Series” floats are built to withstand impacts in excess of 3,000 lbs. per square inch and are rated for up to 1,600 lbs.

With an average empty weight of 565 lbs., the Genesis equipped with the standard Rotax 582 has a useful load of 635 lbs. With any of the larger optional powerplants, and the gross weight capability increases to 1400 lbs., providing for a larger useful load. The HD option has a “beefed up” airframe capable of safely carrying up to 1600 lbs. and a useful load envelope of over 800 lbs.

The Genesis typically will take about 400 hours to complete. All of the welding and fabrication is done before the kits leaves the factory, and the manuals are written with step by step instructions, and numerous photos, illustrations and CAD drawings.

The Genesis airframe sold for US$11,073 in 2009, and includes all of the flight surfaces, fuselage, fiberglass enclosure, landing gear, wheels and tires, control system and doors. Among the options are custom hydraulic brakes, cabin heating, floats, wheel pants, strut fairings, complete instruments packages, and finishing systems.

A complete Genesis aircraft, ready to fly, typically runs from $21,000 to $32,000, depending on your powerplant and choice of options.

Stall: 41 kt / 47 mph / 76 kmh
Cruise: 87 kt / 100 mph / 161 kmh
VNE: 104 kt / 120 mph / 193 kmh
Empty Weight: 295 kg / 650 lbs
MTOW Weight: 590 kg / 1300 lbs
Climb Ratio: 800 ft/min / 4 m/s
Take-off distance: 350 ft / 107 m

Innovation Engineering Genesis
Engine: Rotax 503, 53 hp.
HP range: 53-100.
Speed max: 90 mph.
Cruise: 85 mph.
Range: 225 sm.
Stall: 40 mph.
ROC: 800 fpm.
Take-off dist: 150 ft.
Landing dist: 100 ft.
Service ceiling: 10,000 ft.
Fuel cap: 13.5 USG.
Weight empty: 490 lbs.
Gross: 1000 lbs.
Height: 6.92 ft.
Length: 19.33 ft.
Wing span: 26.67 ft.
Wing area: 155 sq.ft.
Seats: 2.
Landing gear: nose wheel.

Slepcev Storch

The Slepcev Storch is a kit plane designed by Nestor Slepcev and is produced at the factory in Beechwood, Port MacQuarie, Australia. The Slepcev Storch is a dual control 75% scale replica of the Feisler Fi-156 Storch modified for simplicity. Initially designed in 1992 as a single seater, the Slepcev Storch is produced as a two seat tandem Ultralight STOL aircraft.

The Slepcev Storch is JAR-VLA certified, Type Certificate No.VA505 issued by the Australian CASA on 14 October 1991. It also meets Australian Noise Certification to standard 66.8dBA.

The plane was designed around a light fuselage rated at +6/-3G. Reportedly it will fly as slow as 20 mph with full flaps and 30% power. The construction is 4130 chromemoly steel tubing for the fuselage, rudder and elevator. The wings are all-aluminium and the main landing gear is made of 4130 tubing with 10 inches of travel. Standard wheels are 8.00 x 6 mains, and a Maule tailwheel. Brakes are hydraulic disc, and the fuel is contained in the wings.

The kit consists of JAR-VLA certified components and is fully welded with the fuselage and empennage primed for protection against corrosion. Also supplied are upholstered seats, the main landing gear, wheels, hydraulic disc brakes and the Maule tailwheel. The aluminium wingspars and ribs are pre-drilled and the lightening holes are flanged. All the hardware is included, as are the wingskins. Much of the control system is installed, including the stick and all of the fuselage pushrods. The Lexan windows are supplied, and all hardware. No special tools are required.

Slepcev Storch Mk.4

The interior measures 2.6 ft wide, 3.3 ft high, and 4.9 ft long. The fuel tank holds three hours and an optional 26.4 gallon belly tank can add another four hours.

The controls are aluminium pushrods, through the rudder and the elevator trim trim are controlled by cables. The brakes are toe-operated.

Avaliable ready to fly or as an advanced kit 2009 Price: A$44,000.

Slepcev Microlight Storch
Stall: 22 kt / 25 mph / 41 kmh
Cruise: 72 kt / 83 mph / 133 kmh
VNE: 80 kt / 92 mph / 148 kmh
Empty Weight: 289 kg / 637 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 800 ft/min / 4 m/s
Take-off distance (50ft obstacle): 30 ft / 9 m
Landing distance (50ft obstacle): 30 ft / 9 m

Engine: Rotax 618, 75 hp
HP range: 65-100
Height: 7.5 ft
Length: 21.33 ft
Wing span: 33.5 ft
Wing area: 160 sq.ft
Weight empty: 618 lb
Gross: 1056 lb
Fuel cap: 14 USG
Speed max: 78 mph
Cruise: 65 mph
Range: 300 sm
Stall: 16 mph
ROC: 1200 fpm
Take-off dist: 30 ft
Landing dist: 50 ft
Service ceiling: 16,500 ft
Seats: 2
Landing gear: tail wheel

Engine: Rotax 912, 80 hp
HP range: 80-120
Height: 7.5 ft
Length: 24 ft
Wing span: 33.7 ft
Wing area: 180 sq.ft
Empty weight: 650 lb
Gross weight: 1200 lb
Fuel capacity: 18 USG
Top speed: 95 mph
Cruise: 75 mph
Stall: 16 mph
Range: 250 sm
Rate of climb: 1200 fpm
Takeoff dist: 30 ft
Landing dist: 50 ft
Service ceiling: 15,000 ft
Seats: 2 tandem
Landing gear: tailwheel

Engine: Rotax 912S, 100 hp
Length: 22.3 ft
Wing span: 32.8 ft
Wing area: 172.2 sq.ft
Empty weight: 771.6 lb
Gross weight: 1212.5 lb
Fuel capacity: 19.8 Gal
Top speed: 78 kt
Cruise: 70 kt
Stall: 25 kt
Rate of climb: 700 fpm
Takeoff dist: 50-100 ft
Landing dist: 50-100 ft
Service ceiling: 15,000 ft
Seats: 2
2009 price (JAR-VLA) fly away: A$63,000
2009 price (JAR-VLA) Advanced kit: A$44,000
2009 price (JAR-VLA) kit: A$35,000

Slepcev Storch Mk.4
Engine: Rotax 912, 80 hp
Wing span: 10 m
Wing area: 16 sq.m
MAUW: 450 kg
Empty weight: 289 kg
Fuel capacity: 75 lt
Max speed: 150 kph
Cruise speed: 125 kph
Minimum speed: 27 kph
Climb rate: 6 m/s
Seats: 2
Fuel consumption: 11 lt/hr
Price (1998): 77,000 DM
Kit price (1998): 29,650 DM

Skyway Moondial

These backpacks feature a carbonfbre shell holding an ergonomically designed tank, electric start, and the option of 2 or 3 blade prop.

Moondial Light
Empty weight: 17 kg
Engine: K160, 17 hp
Reduction: 1:2.7
Prop diameter: 109 cm
Fuel capacity: 12 lt
Price (1998): 6900 DM