Sorrell SNS-9 EXP II

The SNS-9 is a two-seat, side-by-side version of the SNS-8, powered by a Rotax 503 or Rotax 447.

The first, N9EX, first flew on 22 May 1985.

The SNS-9 airframe kit price was US$19,900. 2009 Price: US$24900

SNS-9
Engine: 42hp Rotax 447
Wingspan: 23’4″
Length: 18’0″
Useful load: 454 lb
Cruise: 85 mph
Stall: 39 mph
Range: 255 mi
Seats: 2

Engine: Rotax 503, 52 hp
Height: 5.3 ft
Length: 18 ft
Wing span: 23.3 ft
Wing area: 148 sq.ft
Weight empty: 360 lb
Gross: 810 lb
Fuel cap: 10 USG
Speed max: 105 mph
Cruise: 80 mph
Range: 300 sm
Stall: 39 mph
ROC: 600 fpm
Take-off dist: 300 ft
Landing dist: 300 ft
Service ceiling: 12,000 ft
Seats: 2
Landing gear: tail wheel

Thunderbird Aviation Hiperlight SNS-9
Engine: Rotax 503
HP range: 50-100
Length: 18 ft
Wing span: 23.4 ft
Wing area: 148 sq.ft
Empty weight: 163 kg / 360 lb
Gross weight: 369 kg / 814 lb
Fuel capacity: 10 USG
VNE: 98 kt / 113 mph / 182 kmh
Cruise: 74 kt / 85 mph / 137 kmh
Stall: 34 kt / 39 mph / 63 kmh
Range: 350 sm
Rate of climb: 600 fpm / 3 m/s
Glide Ratio: 12:1
Takeoff dist: 300 ft / 91 m
Landing dist: 300 ft / 91 m
Seats: 2
Cockpit width: 40 in
Landing gear: tailwheel

Sorrell SNS-8 Hyperlight

In the early ’80s—at the height of the ultralight boom—one of Hobie’s sons, Tim Sorrell, designed a lighter, all-metal ultralight version of the Guppy and named it the SNS-8 Hiperlight. Siblings Mark, John and Lisa joined Tim in a company that marketed the all-metal, single-seat negative stagger biplane Hiperlight, which was quite different from other ultralights.

The kit can be licensed it in the Experimental/Amateur-Built or ultralight category LSA. The kit features a finished and powder-coated 4130 welded-tube forward fuselage and a welded 6061-T6 aluminum aft fuselage. The strut braced equal span wings and tail were built from premade welded aluminium alloy tube parts, and presewn slip-on covering made finishing the airplane easy. Originally powered by a single-cylinder, 28-hp two-stroke Rotax 277 with a Hegar belt reduction drive, later kits features a 28-hp MZ 201 two-stroke engine.

Full span flaperons are fitted to the lower wing. Centre mounted joy stick, rudder pedals, tailwheel steerable through rudder pedals.

The Sorrells were able to convince the FAA to grant an exemption to the ultralight speed limit (55 knots level at full power) as the Hiperlight easily flew at 65 knots. The Hiperlight has full-span sheet-metal ailerons providing a snappy roll rate, and controls are nicely balanced. As with many ultralight designs, the stall is without a break; it is simply a mush easily controllable in all three axes.

In 1984 the Sorrell Hyperlight sold for $8500 pre-fabricated or for $6500 as a kit, both with a 28 hp engine.

The SNS-8 can be landed gracefully in any pitch attitude from a nose-really-high, tailwheel-first one-pointer to a fly-it-on-level wheels landing.

SNS-8
Engine: Rotax 277 (268 cc) 28 hp
Empty weight: 252 lbs
Wing span: 22 ft
Wing area: 140 sq.ft
Height: 5 ft 3 in
Length: 15 ft 6 in
Fuel cap; 5 USG
Construction: Aluminium, Dacron, Steel
Max wt: 500 lb
Stall: 27 mph
Max speed: 63 mph
Vne: 95 mph
Climb rate: 600 fpm @ 38 mph
Design limit: +6, -4g
Glide ratio: 10-1
Wing loading: 3.57 lbs/sq.ft
Power loading: 17.86 lbs/hp
Seats: 1
Takeoff run 175 ft
Landing roll 175 ft

SNS-8 EXP
Engine: Rotax 447, 42 hp
Speed max: 90 mph
Cruise: 75 mph
Range: 150 sm
Stall: 30 mph
ROC: 1200 fpm
Take-off dist: 125 ft
Landing dist: 150 ft
Service ceiling: 12,000 ft
Fuel cap: 5 USG
Weight empty: 300 lb
Gross: 550 lb
Height: 5.25 ft
Length: 15.6 ft
Wing span: 22 ft
Wing area: 140 sq.ft
Seats: 1
Landing gear: tail wheel

Thunderbird Aviation Hiperlight SNS-8
Cruise: 60 mph
Stall: 27 mph
Range: 210 sm
Rate of climb: 700 fpm
Takeoff dist: 175 ft
Landing dist: 175 ft
Engine: MZ 201, 28 hp
HP range: 28-45
Fuel capacity: 5 USG
Empty weight: 247 lb
Gross weight: 500 lb
Length: 15.6 ft
Wing span: 22 ft
Wing area: 140 sq.ft
Seats: 1
Cockpit width: 22 in
Landing gear: tailwheel

Sorrell

Hobart C Sorrell & Sons (John, Mark, Tim),
Rochester WA.
USA

Markets kits to build SNS-7 Hiperbipe as two-seat aerobatic biplane with reverse-stagger wings.

1995: 16525 Tilley Road South, Tenino, WA 98589, USA.

1982: Sorrell Aviation,
Tenino WA.
USA

Sorrell Aircraft Co Ltd.

Soloy Pathfinder 21

The first flight of Soloy Corporation’s modified Cessna 208B Cara¬van, Pathfinder 21, was successfully made on 30 April at Olympia, United States. Flying the aircraft was Soloy’s chief test pilot Paul Haggland and on board for the milestone was crew chief Dan Wright and company president Joe Soloy. The Pathfinder 21 is equipped with two Pratt & Whitney Canada PT6D-114A engines powering a single propeller. The arrangement incorporates a Soloy Dual Pac gearbox assembly, which was certified by the FAA on 18 November 1997. The aircraft’s wings, struts and landing gear have been reinforced to enable its gross ramp weight to be increased to 5,675 kgs (12,500 lbs). The aircraft’s fuselage length has also been increased to almost 2 m more than Cessna’s design.

Engines: 2 x Pratt & Whitney Canada PT6D-114A
Max ramp wt: 5,675 kgs (12,500 lbs)

Solo 2350

A two-stroke, two-cylinder, in-line air cooled light sport engine.

The Solo 2350 D features a mixture control via two diaphragm carburettors, CDI ignition. A crank-case pressure operated fuel pump and crankshaft mounted propeller. With no engine starter, the Solo 2350 D has Type Certificate LBA 4603.

2350 C

Engine: Solo 2350 D
Without Muffler
Cruise power: 19.6 kW at 5,500 1/min
Max rpm: 6,000 1/min
Recommended rpm: 5,000 1/min
Cylinder head temp: Max. 275°C (measured at spark plug)
Fuel consump. at cruise: Approx 2,24 US gal./hr (8,5 l/h)

Engine: Solo 2350 D
With Muffler
Cruise power:
15.3 kW at 5,500 1/min
Max rpm: 6,500 1/min
Recommended rpm: 5,000 1/min
Cylinder head temp: Max. 275°C (measured at spark plug)
Fuel consump. at cruise: Approx 2,24 US gal./hr (8,5 l/h)

Solid Air Diamant

Diamant Twin Hazard

Also available as a single seater, the two seater seats side-by-side.

Diamant LP

The Solid Air Diamant LP (English: Diamond, Light Performance) is a German ultralight trike, designed and produced by Solid Air UL-Bau Franz of Hundheim, Rheinland-Pfalz. The aircraft was supplied as a complete ready-to-fly-aircraft.

The Solid Air Diamant Twin (English: Diamond) ultralight trike was supplied as a complete ready-to-fly-aircraft.

Diamant Twin

Diamant Twin Hazard
Empty weight: 170 kg
Wing span: 10.50 m
Wing area: 13 sq.m
Fuel capacity: 40-60 lt
Certification: Vz
Engine: Hirth F 30, 60 hp
MAUW: 383 kg
Seats: 2
Max speed: 120 kph
Cruise speed: 110 kph
Minimum speed: 50 kph
Climb rate: 3.5 m/s
Fuel consumption: 8 lt/hr
Price (1998): 41 000 DM

Solar Wings Whisper

The 1993 Whisper was designed to blend good performance with ease of handling for intermediate pilots. It is distinguished from the Rumour by the lack of double surface at the tips.

The Whisper was priced at £1695 with round uprights, and £1825 with aerofoil uprights.

Whisper
Sail area: 158 sq ft
Nose angle: 124°