Schweizer SGU 2-22

Designed by Ernest Schweizer, the two-seater 2-22 first flew in 1947 and entered service the following year and became (until superseded by the 2-23) the most used two- place trainer in America. It was derived from the SGU 1-7 and developed through A, B, C, D and E models.

Of all-metal construction with metal and fabric covering, the 2-22 has strut-braced constant chord aluminium alloy hjgh-set wings, with a metal D-tube leading edge ahead of the main spar and fabric covering aft of it; there are no flaps or spoilers. The fuselage is a welded chrome-molybdenum steel tube structure with fabric covering, and there is a non-retractable and unsprung Goodyear mono-wheel with brake immediately aft of a nose skid mounted on rubber blocks; there is also a rubber-mounted tailskid. The fin and rudder are of aluminium with fabric covering, while the strut-braced tailplane and elevators are steel tube frameworks with fabric covering. The two pilots are seated in tandem with dual controls under a transparent, sideways-opening canopy, and in its initial form the 2-22 had tandem open cockpits with provision for an enclosed canopy.

The original 2-22 had a 204 kg / 450 lb empty weight and 377 kg / 830 lb gross with no rear side windows and no doors.

The SGU 2-22A (3 built) which appeared in 1957 featured several changes in the cockpit section, a redesign for the U.S. Air Force Academy with lengthened nose, full canopy and 409 kg / 900 lb gross weight.

The B is the original modified for 409 kg / 900 lb gross weight.

The C incorporated the A and B changes plus smaller ailerons; 103 built, including 28 kits (described as the 2-22CK). The D is the original model with small ailerons. The E was the last production model, with larger spoilers, roomier cockpit, new canopy with wing root changes to provide for a skylight.

Schweizer 2-22E

No. Built: 258, including kits sold for amateur construction.

The 2-33 was designed to succeed the 2-22 as something a little plusher and better performing, thereby making it easier to attract new students into soaring.

2-22E
Wing span: 13.11 m / 43 ft 0 in
Wing area: 19.51 sq.m / 210 sq.ft
Aspect ratio: 8.81
Airfoil: NACA 4301 2A
Length: 25 ft 8.5 in
Height: 9 ft 0 in
Empty Weight: 213 kg / 470 lb
Payload: 195 kg / 430 lb
Gross Weight: 408 kg / 900 lb
Wing Load: 20.91 kg/sq.m / 4.8 lb/sq.ft
Max speed: 89 mph (in smooth air)
L/DMax: 17 76 kph / 41 kt / 47 mph
MinSink: 1.07 m/s / 3.5 fps / 2.07 kt
Min sinking speed (solo): 2.8ft/sec
Seats: 2

Schweizer SGS 1-21

Designed by Ernest Schweizer and built in 1947, the 1-21 won the Nationals that year flown by Dick Comey, whose 483 km / 300 miles flight was a National distance record at the time.

Stan Smith flew a 1-21 in the 1952 World Championships at Madrid Cuatro Vientos in Spain. The ship features triple spoilers (2 on top, 1 on bottom) and water ballast tank in the wing.

The structure was all metal, with some fabric on the tail and trailing edge of wing.

There was no market at the 1947 price so a simpler model, the 1-23, was produced instead.

Wing span: 15.54 m / 51 ft
Wing area: 15.33 sq.m / 165 sq.ft
Aspect ratio: 15.75
Airfoil: NACA 23012
Empty Weight: 213 kg / 470 lb
Payload: 113 kg / 250 lb
Gross Weight: 326 kg / 720 lb
Wing Load: 21.26 kg/sq.m / 4.26 lb/sq.ft
Water Ballast: 121 kg / 266 lb
L/DMax: 27 80 kph / 43 kt / 50 mph
MinSink: 0.76 m/s / 2.5 fps / 1.48 kt
Seats: 1
No. Built: 2

Schweizer SGU 1-20

Designed by Ernest Schweizer, the 1-20 long wing version of the 1-19 first flew in 1946.

The structure was wood/ fabric, 2-spar, 2-strut-braced wings; metal/ fabric tail; steel-tube/ fabric fuselage.

Plans were offered for the new wings and canopy, and several 1-19’s in the U.S. were modified.

The prototype was flown 222 km/ 138 miles by Paul A. Schweizer in 1947.

Wing span: 13.11 m / 43 ft
Wing area: 16.91 sq.m / 182 sq.ft
Aspect ratio: 10.15
Airfoil: NACA 4301 2A
Empty Weight: 181 kg / 400 lb
Payload: 104 kg / 230 lb
Gross Weight: 285 kg / 630 lb
Wing Load: 16.85 kg/sq.m / 3.5 lb/sq.ft
L/DMax: 18 68 kph / 36 kt / 42 mph
MinSink: 0.92 m/s / 3.0 fps / 1.78 kt
Seats: 1

Schweizer Aircraft Corp

The Schweizer Aircraft Corporation was an American manufacturer of sailplanes, agricultural aircraft and helicopters located in Horseheads, New York. The company grew out of the Mercury Glider Club which produced the first two Schweizer gliders in the Schweizers’ barn. The company was originally called the Schweizer Metal Aircraft Company. Attorney Bob McDowell indicated to the Schweizers that they should move their manufacturing operation out of their father’s barn and relocate to the Elmira, New York area. The Schweizers received the suggestion positively as they needed more space to produce gliders, but they had no money with which to make the move.

It was incorporated in 1939 by three Schweizer brothers (Paul, William, and Ernest), who built their first glider in 1930.

McDowell convinced Elmira Industries Inc, the local business development corporation, to provide space for the Schweizers on the second floor of the Elmira Knitting Mill Building in return for stock in the company. This resulted in the Schweizer Metal Aircraft Company becoming the Schweizer Aircraft Corporation in 1939, with a sale of shares to Elmira Industries, local businessmen and soaring pilots.

Schweizer primarily produced light, piston-engined helicopters for use in utility and flight-training roles. The Schweizer 300CBi, originally designed and manufactured by Hughes aircraft as the Hughes 269 for the United States Army, is one of the most widely used training helicopters in the world. In 1986, Schweizer acquired all rights to the helicopter from McDonnell Douglas, who had purchased Hughes Helicopters in 1984. After Schweizer acquired the FAA Type Certificate, the helicopter was known for a short time as the Schweizer-Hughes 300C and then simply, the Schweizer 300C.

Schweizer is perhaps known best for its popular line of gliders (sailplanes), the earliest of which (the model SGP 1-1) was produced in 1930. Although very few of the early gliders were built, later models gained popularity, such as the SGS 2-8 and 2-12, which were adopted by the U.S. Army Air Corps for training as the TG-2 and TG-3, respectively.

The Schweizer SGS 1-23 was a world class competition and record setting glider between its first flight in 1948 and the end of its production in 1967.

In the 1950s and 60s the Schweizer Aircraft Corporation designed and manufactured the very popular SGS 1-26 and SGS 2-33 gliders. They are easy to fly, with simple construction, and are quite rugged and forgiving. A powered light aircraft, the Schweizer SA 1-30 was tested, but did not go into production.

The 2-33 was adopted by the United States Air Force Academy as the TG-4, for use in introductory airmanship training. The Academy used over a dozen such gliders until 2002 when they were replaced by more modern sailplanes. The Royal Canadian Air Cadets continue to operate a fleet of over seventy 2-33As.

Other popular Schweizer gliders include the single-seat SGS 1-26 and the two or three-seat 2-32, both of which can be found in many soaring clubs and in private ownership across the United States.

Primarily designers and makers of sailplanes, one of which (SGS 2-32) fitted with piston engine was tested by Lockheed Aircraft Corporation as Q-Star for ‘quiet reconnaissance’ in Vietnam. On Q-Star was based the Lockheed YO-3A, using Schweizer wings and tail, new fuselage and muffled engine.

Company also built for Grumman the Ag-Cat agricultural biplane, later for Gulfstream, before acquiring the rights in 1981 (Ag-Cat subsequently produced by Ag-Cat Corporation).

Schweizer produced the Grumman G-164 Ag Cat, a single-engine biplane agricultural aircraft originally developed by Grumman in the 1950s. Under the contract with Grumman the airplane was built almost continuously between 1957 and 1981. During this period of time Schweizer built 2,455 of the airplanes.

In 1981 Schweizer bought the rights to the design and continued production under the name Schweizer Ag Cat. In 1995 Schweizer sold the rights to the Ag Cat to Ag-Cat Corp. of Malden, Texas. In February 2001 the design was sold to Allied Ag-Cat Productions Inc. of Walnut Ridge, Arkansas. Allied Ag-Cat is not producing new aircraft although a related company operates a large fleet of Ag-Cats.

The basic airframe incorporates many safety innovations, including a pressurized cockpit to keep pesticides out, air conditioning and a fuselage structure that is designed to progressively collapse in the event of a collision.

The basic designof Schweizer S269C remained unchanged over the years. Between Hughes and Schweizer, nearly 3,000 copies of the Model 269/300 have been built and flown over the last 50 years. Schweizer continued to develop the Model 300 by adding a turbine and redesigning the body to create the Schweizer 330, and then further developments led to the development of the Schweizer 333.

An improved version in the series, the Sikorsky S-434, was released in 2008.

In 1972 Schweizer hired David Thurston and production of his Thurston Teal was part of the agreement to work at Schweizer. The company produced three Schweizer TSC-1A1 Teals and nine TSC-1A2 Teal IIs before production was moved to Teal Aircraft in 1976.

The development of the Schweizer SGM 2-37 two-place motor glider for the United States Air Force Academy in 1982 led to a new area of expertise for the company. In the mid-1960s Lockheed had used the Schweizer SGS 2-32 sailplane as the basis for its YO-3 quiet reconnaissance aircraft. Schweizer decided to develop the SGM 2-37 into a similar concept aircraft as the YO-3. The result was the SA 2-37A and B, known as the RG-8A in military use.

The RG-8A was later developed by the company into the twin piston-engined and twin-boom SA 2-38 Condor with the US military designation of RU-38A Twin Condor. This design was further refined into the turboprop-powered RU-38B Twin Condor. The RU-38 was still in production in 2008.

It is believed the US Drug Enforcement Administration purchased aircraft designated Shadowhawk from Schweizer. The aircraft had a poor operational history. They may be designated SA 38B.
Other projects

In partnership with Northrop Grumman (formerly Ryan Aeronautical), Schweizer is developing the MQ-8 Fire Scout helicopter UAV.

Schweizer is currently participating in development of Sikorsky’s X-2 Demonstrator, a prototype aircraft using co-axial rotor blades with a pusher propeller for extra forward thrust.

Makes fuselage assemblies for Piper Aircraft Corporation and structures for Bell Helicopters. Became license-holder for Hughes 300 helicopter in 1983, producing piston-engined three-seat Model 300C from 1984 to present day and developing new 3/4-seat Model 330 turboshaft-powered helicopter (first flown June 1988); also supports Hughes Model 269s.

In 1986 flew the SA 2-37A low-noise special-missions aircraft suited to surveillance and other roles, followed in May 1995 by a radical twin-boom SA 2-37A conversion known as SA 2-38A. Two joined the U.S. Coast Guard as RU-38A Twin Condors for covert patrol and surveillance (one by conversion, one built as new).

In December 1999, Schweizer Aircraft celebrated its 60th Anniversary, and had built more than 2,160 sailplanes. Schweizer was a major U.S. aerospace contractor and no longer manufactured gliders.

Helicopter products offered by the company as of February 2009 included the 300C, 300CBi, and 333.

Previously the oldest privately owned aircraft company in the United States, Schweizer was acquired by Sikorsky Aircraft Corporation of Stratford, Connecticut, in 2004, and became a diversified aerospace company.

In 2011 and 2012 Sikorsky Aircraft Corporation laid off all the workers and closed the plant.

Schultz Nucleon

The Nucleon designed by Art Schultz, which first flew in 1954, has a wing bult of Styrofoam around a spar and convered with a fiberglass shell. To save weight, struts were used with cuffs at both ends. It has full span flaps, with drooping ailerons, and a horizontal tail which folds up for trailing.

The structure was I-strut braced all-wood wings, steel-tube/ fabric wings and braced tail.

Wing span: 14 m / 46 ft
Wing area: 12.17 sq.m / 131 sq.ft
Aspect ratio: 16
Airfoil: NACA 65 (2)-415
Empty Weight: 156 kg / 345 lb
Payload: 86 kg / 190 lb
Gross Weight: 242 kg / 535 lb
Wing Load: 19.88 kg/sq.m / 4.1 lb/sq.ft
L/DMax: 22 76 kph / 41 kt / 47 mph
MinSink: 1.00 m/s / 3.3 fps / 1.96 kt
Seats: 1

Schroeder Dragontail

The 1950 Schroeder Dragontail Goodyear racer (N60298 and race # 50) was all-metal and fitted with a Y-tailed.

The all-metal Goodyear racer built by Paul Schroeder in Rochester, N.Y. The Continental C-85 engine was behind the pilot.

With race number No. 50, it never raced but qualified in January, 1950, at the Miami races at 102 mph.

It was destroyed in testing on 2 August 1950.

Engine: Continental C-85, 85hp pusher
Wingspan: 20’4″
Length: 18’6″
Seats: 1