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Silvercraft SH-4

The Silvercraft SH-4 is an Italian three-seater light helicopter designed and built by Silvercraft SpA.

Silvercraft SH-4
The first Silvercraft SH-4 exhibited at the Paris Air Salon at Le Bourget airport in June 1965
Role Light helicopter
National origin Italy
Manufacturer Silvercraft SpA
First flight 1963
Number built 21

Design and production edit

The Silvercraft SH-4 was the first Italian designed helicopter to gain Italian and FAA certification. The prototype was first flown in October 1963 with development assisted with both financial and technical help from SIAI-Marchetti. The helicopter was a conventional design with two-blade main rotor and tail rotor, a skid landing gear and a high-set tubular corrugated tailboom. It is powered by either a 200 hp (149 kW) or 235 hp (175 kW) Franklin 6A-350 engines which have been flat-rated to 170 hp (127 kW). Some SH-4s were equipped with Lycoming LHIO-360-C1A engines of 205 hp (153 kW).[1]

Two aircraft were evaluated by the Italian Air Force.

An upgraded development, the SH-200 was developed from the SH-4 but was only flown as a prototype.

Operators edit

  Italy

Variants edit

SH-4
Standard production variant.
SH-4A
Agricultural variant.
SH-4L
Lycoming powered variant
SH-4T
Turbine powered variant

Specifications (SH-4) edit

Data from Jane's All The World's Aircraft 1976–77[4]

General characteristics

  • Crew: One
  • Capacity:
    • Two passengers or
    • 200 L (53 US gal; 44 imp gal) chemicals (crop-spraying version)
  • Length: 7.65 m (25 ft 1 in) (fuselage length)
  • Height: 2.98 m (9 ft 9 in)
  • Empty weight: 518 kg (1,142 lb)
  • Max takeoff weight: 862 kg (1,900 lb)
  • Fuel capacity: 130 L (34 US gal; 29 imp gal)
  • Powerplant: 1 × Franklin 6A-350-D1B air-cooled flat-six engine, 175 kW (235 hp) (derated to 130 kW (170 hp))
  • Main rotor diameter: 9.03 m (29 ft 8 in)
  • Main rotor area: 64.04 m2 (689.3 sq ft)

Performance

  • Maximum speed: 161 km/h (100 mph, 87 kn)
  • Cruise speed: 117 km/h (73 mph, 63 kn) (econ. cruise)
  • Range: 320 km (200 mi, 170 nmi)
  • Endurance: 3 hours
  • Service ceiling: 4,600 m (15,100 ft)
  • Rate of climb: 6.0 m/s (1,180 ft/min)
  • Hover ceiling: 3,000 m (9,800 ft) (in ground effect)

References edit

  1. ^ Federal Aviation Administration (February 2007). . Archived from the original on 2011-07-13. Retrieved 2009-03-09.
  2. ^ aviastar Silvercraft SH-4
  3. ^ all-aero Silvercraft SH-4
  4. ^ Taylor 1976, pp. 119–120
  • Taylor, John W. R. (1976). Jane's All The World's Aircraft 1976–77. London: Janee's Yearbooks. ISBN 0-354-00538-3.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.

silvercraft, italian, three, seater, light, helicopter, designed, built, silvercraft, first, exhibited, paris, salon, bourget, airport, june, 1965role, light, helicopternational, origin, italymanufacturer, silvercraft, spafirst, flight, 1963number, built, cont. The Silvercraft SH 4 is an Italian three seater light helicopter designed and built by Silvercraft SpA Silvercraft SH 4The first Silvercraft SH 4 exhibited at the Paris Air Salon at Le Bourget airport in June 1965Role Light helicopterNational origin ItalyManufacturer Silvercraft SpAFirst flight 1963Number built 21 Contents 1 Design and production 2 Operators 3 Variants 4 Specifications SH 4 5 ReferencesDesign and production editThe Silvercraft SH 4 was the first Italian designed helicopter to gain Italian and FAA certification The prototype was first flown in October 1963 with development assisted with both financial and technical help from SIAI Marchetti The helicopter was a conventional design with two blade main rotor and tail rotor a skid landing gear and a high set tubular corrugated tailboom It is powered by either a 200 hp 149 kW or 235 hp 175 kW Franklin 6A 350 engines which have been flat rated to 170 hp 127 kW Some SH 4s were equipped with Lycoming LHIO 360 C1A engines of 205 hp 153 kW 1 Two aircraft were evaluated by the Italian Air Force An upgraded development the SH 200 was developed from the SH 4 but was only flown as a prototype Operators edit nbsp ItalyItalian Air Force operated one Silvercraft SH 4 for evaluation test 2 3 Variants editSH 4 Standard production variant SH 4A Agricultural variant SH 4L Lycoming powered variant SH 4T Turbine powered variantSpecifications SH 4 editData from Jane s All The World s Aircraft 1976 77 4 General characteristicsCrew One Capacity Two passengers or 200 L 53 US gal 44 imp gal chemicals crop spraying version Length 7 65 m 25 ft 1 in fuselage length Height 2 98 m 9 ft 9 in Empty weight 518 kg 1 142 lb Max takeoff weight 862 kg 1 900 lb Fuel capacity 130 L 34 US gal 29 imp gal Powerplant 1 Franklin 6A 350 D1B air cooled flat six engine 175 kW 235 hp derated to 130 kW 170 hp Main rotor diameter 9 03 m 29 ft 8 in Main rotor area 64 04 m2 689 3 sq ft Performance Maximum speed 161 km h 100 mph 87 kn Cruise speed 117 km h 73 mph 63 kn econ cruise Range 320 km 200 mi 170 nmi Endurance 3 hours Service ceiling 4 600 m 15 100 ft Rate of climb 6 0 m s 1 180 ft min Hover ceiling 3 000 m 9 800 ft in ground effect References edit nbsp Wikimedia Commons has media related to Silvercraft SH 4 Federal Aviation Administration February 2007 Docket No FAA 2006 25948 Directorate Identifier 2006 NE 32 AD Amendment 39 14951 AD 2007 04 19 Archived from the original on 2011 07 13 Retrieved 2009 03 09 aviastar Silvercraft SH 4 all aero Silvercraft SH 4 Taylor 1976 pp 119 120 Taylor John W R 1976 Jane s All The World s Aircraft 1976 77 London Janee s Yearbooks ISBN 0 354 00538 3 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions The Illustrated Encyclopedia of Aircraft Part Work 1982 1985 Orbis Publishing Retrieved from https en wikipedia org w index php title Silvercraft SH 4 amp oldid 1068471293, wikipedia, wiki, book, books, library,

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