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SIAI-Marchetti XY / Silvercraft SH-4

Silver-SH4

 

In October 1963 Silvercraft SpA flew the XY prototype light helicopter further developed with financial and technical assistance of shareholder SIAI-Marchetti as the all-metal three-seat SH-4, the prototype of which (I-SILX) made its first flight in March 1965.

The SH-4 had a skid undercarriage and a high-set tubular corrugated tailboom with a small fin and tailplane and a two-blade tail rotor and powered by a 235hp (derated to 170hp) Franklin 6A-350-D1B piston engine. The main rotor had two blades and a transverse mass-balanced stabiliser bar.

A pre-production model was displayed at the 1967 Paris Air Show, certification was achieved in September 1968. The first helicopter of all-Italian design and construction to receive both Italian and U.S. certification. The SH-4 went into production at Silvercraft's works at Sesto Calende in basic form. Variations were the SH-4/A for agricultural use and as the SH-4/C with a supercharged Franklin 6AS-350-D1 engine.

Serious production had begun as SIAI-Marchetti/Silvercraft SH-4, but under name Silvercraft alone deliveries began 1970. Production ceased 1977. Production of a batch of about 50 SH-4s was started at the Sesto Calende works with the aid of Fiat Aviazione (Motori), who manufactured mechanical parts for the rotor transmission, but the firm ran into difficulties over the Franklin engine, which had gone out of production.

A total of 21 SH-4s were completed with individual examples being exported to Brazil, South Africa, France and Holland. One aircraft was delivered to the Italian Air Force.

The company ceased operations in the late 1970s.

 

SH-4
Engine: Franklin 6A-350-D1B, 235hp/175kW (derated to 170hp)
Main rotor diameter: 9.0m
Length: 7.50m
Height: 2.7m
Max take-off weight: 862kg
Empty weight: 510kg
Max speed: 161km/h
Cruising speed: 140km/h
Ceiling: 4000m
Range with max fuel: 360km

 

Silver-SH4-ld

 

 

 

 

 

 

 


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