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Airmak J4

The Airmak J4 is an Italian ultralight and light-sport aircraft designed and produced by Airmak S.r.l. of Capua. The design's first flight was in early 2011. The aircraft is supplied complete and ready-to-fly.[1]

J4
Role Ultralight aircraft and Light-sport aircraft
National origin Italy
Manufacturer Airmak S.r.l.
First flight early 2011
Status In production (2015)
Produced 2012-present

Design and development Edit

The aircraft is produced by Airmak S.r.l., a joint venture between Rafaelle Violetti and Valter Proietti of OMA Sud. It is manufactured at OMA Sud's Italian facility. Production commenced in the middle of 2012.[1][2]

The J4 was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin accessed by doors, fixed tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft fuselage is made from welded steel tubing, with riveted aluminium tail and wings. Its 9.44 m (31.0 ft) span wing has an area of 11.6 m2 (125 sq ft), employs a custom Iannotta airfoil and mounts flaps. The standard engine used is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant.[1][3]

As of January 2017 the design does not appear on the Federal Aviation Administration's list of approved special light-sport aircraft.[4]

Operational history Edit

Reviewer Marino Boric described the design in a 2015 review as "elegant".[1]

Specifications (J4) Edit

Data from Tacke and manufacturer[1][3]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 7.40 m (24 ft 3 in)
  • Wingspan: 9.44 m (31 ft 0 in)
  • Height: 2.49 m (8 ft 2 in)
  • Wing area: 11.6 m2 (125 sq ft)
  • Airfoil: Iannotta
  • Empty weight: 330 kg (728 lb)
  • Gross weight: 600 kg (1,323 lb)
  • Fuel capacity: 108 litres (24 imp gal; 29 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
  • Propellers: 3-bladed composite

Performance

  • Cruise speed: 200 km/h (120 mph, 110 kn)
  • Stall speed: 60 km/h (37 mph, 32 kn) flaps down
  • Never exceed speed: 280 km/h (170 mph, 150 kn)
  • Range: 1,070 km (660 mi, 580 nmi)
  • Service ceiling: 6,100 m (20,000 ft)
  • g limits: +3.8/-2,2
  • Rate of climb: 4.5 m/s (890 ft/min)
  • Wing loading: 51.7 kg/m2 (10.6 lb/sq ft)

Avionics

References Edit

  1. ^ a b c d e f Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 24. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ^ Airmak. . Archived from the original on 10 January 2017. Retrieved 9 January 2017.
  3. ^ a b Airmak. . Archived from the original on 9 January 2017. Retrieved 8 January 2017.
  4. ^ Federal Aviation Administration (26 September 2016). "SLSA Make/Model Directory". Retrieved 8 January 2017.

External links Edit

  • Official website

airmak, italian, ultralight, light, sport, aircraft, designed, produced, airmak, capua, design, first, flight, early, 2011, aircraft, supplied, complete, ready, j4role, ultralight, aircraft, light, sport, aircraftnational, origin, italymanufacturer, airmak, fi. The Airmak J4 is an Italian ultralight and light sport aircraft designed and produced by Airmak S r l of Capua The design s first flight was in early 2011 The aircraft is supplied complete and ready to fly 1 J4Role Ultralight aircraft and Light sport aircraftNational origin ItalyManufacturer Airmak S r l First flight early 2011Status In production 2015 Produced 2012 present Contents 1 Design and development 2 Operational history 3 Specifications J4 4 References 5 External linksDesign and development EditThe aircraft is produced by Airmak S r l a joint venture between Rafaelle Violetti and Valter Proietti of OMA Sud It is manufactured at OMA Sud s Italian facility Production commenced in the middle of 2012 1 2 The J4 was designed to comply with the Federation Aeronautique Internationale microlight rules and US light sport aircraft rules It features a strut braced high wing a two seats in side by side configuration enclosed cabin accessed by doors fixed tricycle landing gear and a single engine in tractor configuration 1 The aircraft fuselage is made from welded steel tubing with riveted aluminium tail and wings Its 9 44 m 31 0 ft span wing has an area of 11 6 m2 125 sq ft employs a custom Iannotta airfoil and mounts flaps The standard engine used is the 100 hp 75 kW Rotax 912ULS four stroke powerplant 1 3 As of January 2017 the design does not appear on the Federal Aviation Administration s list of approved special light sport aircraft 4 Operational history EditReviewer Marino Boric described the design in a 2015 review as elegant 1 Specifications J4 EditData from Tacke and manufacturer 1 3 General characteristicsCrew one Capacity one passenger Length 7 40 m 24 ft 3 in Wingspan 9 44 m 31 ft 0 in Height 2 49 m 8 ft 2 in Wing area 11 6 m2 125 sq ft Airfoil Iannotta Empty weight 330 kg 728 lb Gross weight 600 kg 1 323 lb Fuel capacity 108 litres 24 imp gal 29 US gal Powerplant 1 Rotax 912ULS four cylinder liquid and air cooled four stroke aircraft engine 75 kW 101 hp Propellers 3 bladed compositePerformance Cruise speed 200 km h 120 mph 110 kn Stall speed 60 km h 37 mph 32 kn flaps down Never exceed speed 280 km h 170 mph 150 kn Range 1 070 km 660 mi 580 nmi Service ceiling 6 100 m 20 000 ft g limits 3 8 2 2 Rate of climb 4 5 m s 890 ft min Wing loading 51 7 kg m2 10 6 lb sq ft Avionics Garmin Geopilot Plus 2References Edit a b c d e f Tacke Willi Marino Boric et al World Directory of Light Aviation 2015 16 page 24 Flying Pages Europe SARL 2015 ISSN 1368 485X Airmak Chi Siamo Archived from the original on 10 January 2017 Retrieved 9 January 2017 a b Airmak J4 Archived from the original on 9 January 2017 Retrieved 8 January 2017 Federal Aviation Administration 26 September 2016 SLSA Make Model Directory Retrieved 8 January 2017 External links EditOfficial websitePortals nbsp Italy nbsp Companies nbsp Aviation Retrieved from https en wikipedia org w index php title Airmak J4 amp oldid 1149680975, wikipedia, wiki, book, books, library,

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