Jump to content

Tecnam P2004 Bravo

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by KolbertBot (talk | contribs) at 15:01, 15 September 2017 (Bot: HTTP→HTTPS). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

P2004
Role Two-seat ultralight monoplane
National origin Italy
Manufacturer Tecnam
First flight 2002

The Tecnam P2004 Bravo is a high-wing, light aircraft built by the Tecnam aircraft company. It is similar to the Tecnam P92 Echo Super, but has a cantilevered wing rather than the P92's strut-braced wing.[1]

Specifications (P2004 Bravo)

Data from https://web.archive.org/web/20071107011240/http://www.tecnam.com:80/ing/p_2004Bravo.cfm

General characteristics

  • Crew: one, pilot
  • Capacity: one passenger

Performance

  • Take off run: 140 m (460 ft)
  • Landing distance: 120 m (394 ft)

See also

Aircraft of comparable role, configuration, and era

References

  1. ^ Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 80. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

External links