Danieli Piuma

Italian motorglider


title: "Danieli Piuma" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1990s-italian-sailplanes", "homebuilt-aircraft", "aircraft-first-flown-in-1990", "single-engined-pusher-aircraft", "motor-gliders", "high-wing-aircraft"] description: "Italian motorglider" topic_path: "geography/italy" source: "https://en.wikipedia.org/wiki/Danieli_Piuma" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary Italian motorglider ::

::data[format=table title="Infobox aircraft"]

FieldValue
namePiuma
aircraft_typeMotor glider
national_originItaly
designerTiziano Danieli
statusPlans available
number_built13 (all models 2003)
introduction1990
first_flight1990
::

| name = Piuma | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Motor glider | aim = | outcome = | related = | national_origin = Italy | manufacturer = | design_group = | designer = Tiziano Danieli | builder = | issuer = | status = Plans available | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 13 (all models 2003) | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = 1990 | retired = | first_flight = 1990 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = The Danieli Piuma () is a family of Italian high-wing, strut-braced, pusher configuration single-seat motor gliders that was designed by Tiziano Danieli of Schio and supplied as plans for amateur construction.

Design and development

The Piuma was designed to be an inexpensive, easy-to-fly and easy-to-build ultralight motor glider. The first model was initially just called the Piuma, but as other models were developed it became known as the Piuma Original.

The Piuma is constructed from wood and finished with doped fabric. The semi-tapered 11.89 m span wing is supported by a single lift strut on each side and has air brakes. The engine is mounted behind the cockpit. The specified engine is the 22 kW KFM 107er, but engines of 15 to can be fitted. The landing gear is of tricycle configuration and made from steel with rubber shock-absorbers, with an auxiliary tailwheel and fits wheel pants to reduce drag. The tail is cruciform. The aircraft has a glide ratio of 17:1 at 64 km/h. Cabin width is 58 cm

The designer estimated that it would take a builder 1000 hours to complete the aircraft from the plans. The plans cost US$220 in 1998 and included a 30-page construction manual.

Variants

;Piuma Original :Initial version with 11.89 m span wing, first flown in 1990. Eight reported completed in 2003. ;Piuma E :Improved model with glide ratio of 20:1 at 71 km/h and other refinements. ;Piuma Evolution :Improved model with a wider cockpit, more streamlined fuselage, redesigned tail, new lift struts, electrically retractable nose wheel. main landing gear made from a wood/fibreglass sandwich and a more reclined seat. Four reported completed in 2003. ;Piuma Tourer :Model optimized for cross country powered flight with shorter wing of 10.39 m and a NACA 4415 airfoil used in the rectangular portion of the wing and a NACA 2R1-12 airfoil in the tapered wing tip. Cruises at 135 km/h and has a 10:1 glide ratio. One reported completed in 2003. ;Piuma Twin Evolution :Two seat model with side-by-side configuration seating, introduced in 1998 and inspired by the Tourer. The recommended engine is the Rotax 503 of 37 kW.

Specifications (Piuma Original)

|ref=Purdy and Danieli |prime units?=met General characteristics

|genhide=

|crew=one |capacity= |length m= |length ft=19.70 |length in= |length note= |span m= |span ft=39.00 |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft=125.0 |wing area note= |aspect ratio=11:1 |airfoil=Rhode St. Genese 36 |empty weight kg= |empty weight lb=320 |empty weight note= |gross weight kg= |gross weight lb=530 |gross weight note= |fuel capacity=15 L |more general=

Powerplant

|eng1 number=1 |eng1 name=KFM 107er |eng1 type=two-cylinder, two-stroke, single ignition, horizontally opposed aircraft engine |eng1 kw=22 |eng1 hp=

|prop blade number=2 |prop name=wooden |prop dia m= |prop dia ft= |prop dia in= |prop note=

Performance

|perfhide=

|max speed kmh= |max speed mph=62 |max speed kts= |max speed note= |cruise speed kmh= |cruise speed mph=50 |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph=30 |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |range km= |range miles=250 |range nmi= |range note= |endurance= |ceiling m= |ceiling ft=10000 |ceiling note= |g limits= |roll rate= |glide ratio=17:1 at 64 km/h |climb rate ms= |climb rate ftmin= |climb rate note= |sink rate ms= |sink rate ftmin=500 |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft=4.24 |wing loading note= |more performance= |avionics=

References

References

  1. Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook'', page 306. BAI Communications, July 1998. {{ISBN. 0-9636409-4-1
  2. Downey, Julia: ''2001 Plans Aircraft Directory'', Kitplanes, Volume 18, Number 1, January 2001, page 18. Kitplanes Acquisition Company. ISSN 0891-1851
  3. Downey, Julia: ''2002 Plans Aircraft Directory'', Kitplanes, Volume 19, Number 1, January 2002, pages 15-16. Kitplanes Acquisition Company. ISSN 0891-1851
  4. Downey, Julia: ''2003 Plans Aircraft Directory'', Kitplanes, Volume 20, Number 1, January 2003, page 19. Primedia Publications. ISSN 0891-1851
  5. Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 56. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X
  6. Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 134. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  7. Danieli, Elia. (2010). "Piuma Original".
  8. Danieli, Elia. (2010). "Piuma Evolution".
  9. Danieli, Elia. (2010). "Piuma Tourer".
  10. Danieli, Elia. (2010). "Piuma Twin Evolution".

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1990s-italian-sailplaneshomebuilt-aircraftaircraft-first-flown-in-1990single-engined-pusher-aircraftmotor-glidershigh-wing-aircraft