Английская Википедия:Coavio DF 2000

Материал из Онлайн справочника
Перейти к навигацииПерейти к поиску

The Coavio DF 2000 is a single-engine, high-wing all-metal ultralight aircraft with side-by-side seating for two. Built in Italy, production began in 2004.[1]

Design and development

The DF 2000 was designed to provide a fast, robust, comfortable, low-cost side-by-side two-seat ultralight with a short take-off run. It has a conventional layout not unlike that of, for example, the Cessna 152, with a high wing, swept vertical tail and tricycle undercarriage.[1][2]

Structurally, it is mostly built from aluminium alloy, reinforced with TIG-welded 4130 steel tubing in the cockpit area. The wing has constant chord and is braced on each side by a single, broad streamlined strut from the bottom of the fuselage. The shallow, turned-up wing tips are formed from composites. Inboard flaps are fitted. The cockpit area, under the wings and fitted with dual controls, is accessed by upward-hinged doors with deep glazing. Aft, the fuselage becomes more slender, though the swept fin has a long fillet. The rudder has a trim tab and the low-set, parallel-chord tailplane carries a balanced elevator. The tricycle undercarriage has main wheels which are cantilever spring-mounted from the lower fuselage and a steerable nose wheel. All wheels are usually spatted.[1][2][3]

The DF 2000 family uses several engine/propeller combinations, mostly from the Rotax 912 series of Шаблон:Convert flat-4s but also the Шаблон:Convert Jabiru 2200 and Шаблон:Convert Jabiru 3300 powerplants.[2][1][3]

The DF 2000 first flew in about 2001 and went into production three years later. .[2]

Operational history

54 DF 2000 series aircraft have been built up to 2021.

Variants

Details from the manufacturer.[4]

Spartan
Lightest DF 2000, 60 kW (80 hp) Rotax 912 UL engine, 2-blade wooden propeller. Mechanical trim control and flap actuation.
DF 2000 Light (or Base[2])
Standard version, as Spartan but painted and with oil pressure gauge.
DF 2000 Plus
75 kW (100 hp) Rotax 912 ULS engine, composite 3-bladed propeller with ground-adjustable pitch. Electrical elevator trim control and flap actuation, flap hinge fairing, partial cabin ventilation and additional instrumentation. Wheel spats and landing light.
DF 2000 Top
As Plus with a bigger oil cooler, radio and further instrumentation, upholstered seats and cabin panelling. Landing lights, radio and cockpit heater standard. Two-colour external paintwork. Flight-adjustable pitch propeller an option.
DA Evolution
de Luxe version with either 75 kW (100 hp) Rotax 912 ULS or 64 kW (86 hp) Jabiru 2200[2] engine. As Top, but with full cabin ventilation, improved seating and electrical aileron trim control. Improved external lighting. Three colour external paintwork and bigger spinner.

Specifications (DF 2000 Top)

Шаблон:Aircraft specs Шаблон:Aircontent

References

Шаблон:Reflist Шаблон:Refbegin Шаблон:Refend


Шаблон:Portal bar

Партнерские ресурсы
Криптовалюты
Магазины
Хостинг
Разное

  1. ↑ 1,0 1,1 1,2 1,3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 35. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ↑ 2,0 2,1 2,2 2,3 2,4 2,5 Ошибка цитирования Неверный тег <ref>; для сносок JAWA10 не указан текст
  3. ↑ 3,0 3,1 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 38. Flying Pages Europe SARL, 2015. Шаблон:ISSN
  4. ↑ Ошибка цитирования Неверный тег <ref>; для сносок CoVar не указан текст
Источник — http://wikihandbk.com/ruwiki/index.php?title=Английская_Википедия:Coavio_DF_2000&oldid=14003437