Sonaca 200

The Sonaca 200 is a Belgian two-seat training aircraft designed and built by Sonaca Aircraft.

Sonaca 200
Sonaca 200's initial demonstrator assembled in 2015
Role Very Light Aircraft
Manufacturer Sonaca Aircraft
First flight 2017
Introduction 2017
Number built 10 (1 Prototype)
Developed from The Airplane Factory Sling 2

Design and development

The Sonaca 200 is a low-wing cantilever monoplane made from aluminium alloy, it has an enclosed cabin with two side-by-side seats. It is powered by a 115 hp Rotax 914 and has a fixed tricycle landing gear.

In late 2015, the Sonaca group announced the creation of the subsidiary “Sonaca Aircraft” dedicated to the development, certification and market launch of a new training aircraft based on TAF's Sling 2. Later the aircraft was renamed as Sonaca 200. The single-engine two-seater, specifically designed for pilots' training and leisure flights, was certified in June 2018.[1] Sonaca 200 is EASA-certified for a maximum take-off weight of 750 kg and a cruise speed of 115 knots. In addition to the obtention of the type certification, Sonaca Aircraft has obtained a Design Organisation Approval (DOA) and Production Organisations Approvals (POA) certification.[1]

An initial demonstrator was assembled in April 2015, at Johannesburg by The Airplane Factory. In April 2017, Sonaca Aircraft unveiled the new version of the Sonaca 200 in which 80% of the structure has been redesigned compared to the initial "Amateur Construction" prototype version.

In 2018, after obtaining the Type Certification of the S200, Sonaca Aircraft announced the development of a Glass Cockpit variant, named the S201.[1]

Variants
S200
Production variant certified under EASA CS-VLA requirements with analogue flight instruments.[2]
S201
Glass cockpit model to be certified in 2019, using Garmin G500 TXi suite.[1]

Specification
Roll out of the first Sonaca 200 produced by Sonaca Aircraft
OO-NEW before display at BAFD 2018, Kleine Brogel air base

Data from TCDS[2]

General characteristics

  • Crew: 1 pilot
  • Capacity: 1 passenger or trainee
  • Length: 6.74 m (22 ft 1 in)
  • Wingspan: 9.24 m (30 ft 4 in)
  • Height: 2.56 m (8 ft 5 in)
  • Wing area: 11.85 m2 (127.6 sq ft)
  • Max takeoff weight: 750 kg (1,653 lb)
  • Fuel capacity: 140 L
  • Powerplant: 1 × Rotax 914F four-stroke piston engine, 86 kW (115 hp)
  • Propellers: 3-bladed DUC Helices FLASH-R, 1.75 m (5 ft 9 in) diameter Clockwise rotation (pilot;s view)

Performance

  • Cruise speed: 213 km/h (132 mph, 115 kn)
  • Never exceed speed: 250 km/h (155 mph, 135 kn)
  • Service ceiling: 4,000 m (13,000 ft)
  • Rate of climb: 3.8 m/s (750 ft/min)

References
  1. "Sonaca Aircraft Website".
  2. EASA Type Certificate A.626 Sonaca S2
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