CAB Minicab

Last updated
GY-20 Minicab
Gardan GY-201 Minicab G-BGMR Wroughton 04.07.93 edited-2.jpg
GY-201 Amateur-built in the UK
Rolelight aircraft
Manufacturer Constructions Aéronautiques du Béarn
Designer Yves Gardan
First flight1 February 1949
Number built65 [1] + ca. 130 homebuilt
Variants GY-30 Supercab

The CAB GY-20 Minicab is a two-seat light aircraft designed by Yves Gardan and built in France by Construction Aeronautiques du Bearn (CAB) [2] in the years immediately following World War II. CAB was formed in 1948 by Yves Gardan, Max Lapoerte and M. Dubouts. [3]

Contents

Design and development

The Minicab is a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage, powered by a Continental A65 engine. Its design was a scaled-down version of the aircraft that Yves Gardan had designed for SIPA, the SIPA S.90. The pilot and passenger sit side by side and access to the cockpit is via a one-piece perspex canopy that hinges forwards. Gardan's intention was to produce a low-cost, easy-to-fly, easy-to-maintain aircraft with the possibility of homebuilding. [4]

Production

The prototype Minicab first flew at Pau-Idron on 1 February 1949 with Max Fischl at the controls. CAB manufactured a total of about 65 Minicabs when production ended in 1955. [1] [5] The rights for the plans were then acquired by Arthur Ord-Hume in the United Kingdom who anglicised the drawings and made various minor improvements for home-builders. [2] A large number were completed by amateur builders in the United Kingdom, France and other countries around the world. [4] There is about 20 Minicabs currently active in the United Kingdom, many of which were built (or rebuilt) to the JB.01 standard, developed by M. Jean Barritault, usually with a Continental C90 engine.

Falconar sold plans for a tricycle gear homebuilt model named the Minihawk. [6] Another development is the K&S or Squarecraft Cavalier which is a redesigned Minicab in several versions with plans translated from French to English and modified by Stan Mcleod. The plans were marketed by K&S Aircraft of Calgary, Alberta and later MacFam. [7]

Operational history

Minicab built to Barritault JB.01 standard at Cranfield in 1960 Gardan GY-20 F-PJKA Cranfield 09.60 edited-1.jpg
Minicab built to Barritault JB.01 standard at Cranfield in 1960

Type certification was obtained in mid-April 1949. By the end of 1950, a Minicab had won the Coupe de Vitesse de Deauville (Deauville Cup for speed), and the Grand Prix Aérien de Vichy (Vichy Aerial Prize). [1] The following year, a Minicab broke the world air distance record for its class (1,825 km, 1,138 miles) and in 1952 it attained the world airspeed record for its class over a 2,000 km circuit, with an average speed of (183 km/h, 114 mph).

One Minicab, G-AWEP, was flown by the ex-RAF fighter pilot Roland Beamont who was a test pilot at BAC Samlesbury. He made its first flight in 1969 and wrote that "the Minicab felt light and very responsive... landing required the delicate touch of a Spitfire pilot. In fact the overall control harmony is not dissimilar to that classic aeroplane". [8]

Variants

GY-20 Minicab
CAB first production model. [4]
GY-201 Minicab
refined version with increased fuel capacity, reduced wingspan, strengthened undercarriage, split flaps, and castoring tailwheel. [5] CAB final production model and also principal homebuilt version. [4]
Barritault JB.01 Minicab
built to the modified design of Jean Barritault.
Falconar Hawk
Minicabs built to plans supplied by Falconar
Falconar MiniHawk
plans-built design from Falconar with tricycle undercarriage.
MacFam Cavalier (K&S or Squarecraft Cavalier)
Redesigned in several versions principally with tricycle and swept tail surfaces, and strengthened for a more powerful engine. [7]

Specifications (GY-20)

Data from Jane's All The World's Aircraft 1956–57 [9]

General characteristics

Performance

See also

Related Research Articles

Luton Major Type of aircraft

The Luton L.A.5 Major was a 1930s British two-seat high-wing cabin monoplane. Following World War II, plans were made available to suit construction as a homebuilt aircraft.

CAB Supercab Light aircraft

The CAB GY-30 Supercab was a two-seat light aircraft built in France in 1954, as a further development of the CAB Minicab. The design was performed by Yves Gardan, a onetime employee of French aeronautical company SIPA. Changes incorporated in the Supercab included a more powerful engine, greater wingspan, manually retractable undercarriage, and slotted flaps that replaced the split flaps of the Minicab.

Constructions Aéronautiques du Béarn (CAB) was a French aircraft manufacturer established by Max Laporte and Yves Gardan in Pau, Béarn in 1948. Its main product was the Minicab, a two-seat low-wing monoplane light aircraft of Gardan's design constructed in wood with a fabric covering, and equipped with a fixed tailwheel undercarriage, while the similar Supercab had a retractable undercarriage and detail refinements. The company ceased business in the mid-1950s.

Praga E.114 Type of aircraft

The Praga E.114 was a single-engine sport airplane, designed and manufactured by the Czechoslovakian company ČKD-Praga. Due to its light weight it was also called Air Baby.

The Falconar Teal was a two-seat homebuilt, amphibious airplane designed by Chris Falconar of Edmonton, Alberta, Canada. From the 1970s to the 1990s plans were sold by Falconar Aviation of Edmonton. A handful were built by amateur aircraft constructors in Canada and the United States. Most were powered by certified Lycoming or Continental engines.

The Falconar AMF-S14 Maranda is a two-seat, light aircraft first flown in Canada in 1961 and originally marketed for amateur construction by Falconar Avia.

The Fletcher FBT-2 was a military trainer aircraft built in the United States in the early 1940s. Although it was never entered production as a trainer, it was ordered in small numbers as a target drone but when that was cancelled played a small part in the development of guided bombs.

Malmö MFI-10 Vipan Type of aircraft

The Malmö MFI-10 Vipan was a four-seat light utility monoplane designed and built in Sweden by Malmö Flygindustri. Only three aircraft were built and the type did not enter quantity production.

SOCATA Horizon Type of aircraft

The GY-80 Horizon is a French four-seat touring monoplane of the 1960s designed by Yves Gardan and built under licence, first by Sud Aviation, and later by that company's SOCATA subsidiary.

SIPA S.90 Type of aircraft

The SIPA S.90 was a French-built two-seat light touring and training aircraft of the 1940s and 1950s.

SIPA S.1000 Coccinelle Type of aircraft

The SIPA S.1000 Coccinelle was a French-built light civil utility aircraft of the 1950s.

SNCASO SO.7060 Deauville Type of aircraft

The SNCASO S.O.7050, S.O.7055, S.O.7056 and S.O.7060 Deauville were single-engine light French civil utility aircraft of the 1940s. Only two airframes were built but were modified with different undercarriages, engines and seating.

RAE Scarab Type of aircraft

The RAE Scarab was a light single-engined single-seat parasol winged modification of the de Havilland Humming Bird, flying in the United Kingdom in 1932. Only one was built.

Carden-Baynes Bee Type of aircraft

The Carden-Baynes Bee was a 1930s British two-seat aircraft, with twin engines in pusher configuration buried in the wings. The wings rotated for storage. Financial problems limited the Bee to a single flight.

The SITAR GY-100 Bagheera was a light aircraft designed and built in France in the late 1960s. Designed by Yves Gardan, it was a low-wing, cantilever monoplane of conventional layout with fixed, tricycle undercarriage. The fully enclosed cabin had seating for up to four people in 2+2 configuration. Construction was of metal throughout.

The SITAR GY-90 Mowgli was a light aircraft designed in France in the late 1960s and marketed for homebuilding. Designer Yves Gardan intended it to be a smaller and simpler version of his Bagheera, a conventional low-wing, cantilever monoplane with fixed tricycle undercarriage and a fully enclosed cabin. However, although the Bagheera had seating for up to four people in 2+2 configuration, the Mowgli had no rear seat and could seat only two people, with space behind the seats for luggage. Like the Bagheera, construction was of metal throughout. The Mowgli was designed to use either a 67-kW (90-hp) or 75-kW (100-hp) Continental flat-4 engine.

The SITAR GY-110 Sher Khan was a light aircraft designed in France in the late 1960s as a larger and more powerful version of designer Yves Gardan's Bagheera. Like the Bagheera, it was to be a conventional low-wing, cantilever monoplane with a fully enclosed cabin. However, although the Bagheera had seating for up to four people in 2+2 configuration, the Sher Khan was to have a stretched fuselage with full seating for four people. The wingspan was also to be enlarged, and unlike the Bagheera, whose tricycle undercarriage was fixed, the Sher Khan's was to be retractable.

MacFam Cavalier Canadian-French light aircraft

The MacFam Cavalier is a homebuilt aircraft designed by Stan McLeod, developed through a progressing series of models, all using all-wooden construction. The model range includes the SA102, SA102.5, SA103, SA104 and the SA105.

The Gardan GY-120 was a single engine, parasol wing ultralight seating two in tandem, designed and built in France in the 1980s. It did not go into production.

Falconar F11 Sporty Canadian homebuilt light aircraft

The Falconar F11 Sporty is a Canadian amateur-built aircraft, that was designed by Chris Falconar and produced by Falconar Avia. Falconar supplied it as a kit or as plans for amateur construction. Today both the F11A and E models are available as plans from Manna Aviation.

References

Notes
  1. 1 2 3 Canal Blog "Le Minicab"
  2. 1 2 Jackson Vol II, 1988, p.377
  3. Bruno Parmentier (2000-06-17). "C.A.B. GY-20 'Minicab' - Tourisme - Un siècle d'aviation française". Aviafrance.com. Retrieved 2022-08-31.
  4. 1 2 3 4 Ord-Hume, 2013, pp.204-205
  5. 1 2 Oldtimer-Homepage der Segel- und Motorfluggruppe Veterano, Birrfeld
  6. "Falconar Plans" . Retrieved 2 September 2013.
  7. 1 2 Jackson Vol III, 1988, p.442
  8. Beamont, 1980, p.153
  9. Bridgman 1956, pp. 132–133.
Bibliography