Tecma FX
{{Short description|French glider}}
{{Use dmy dates|date=June 2021}}
{{Use British English|date=June 2021}}
{{Infobox aircraft begin
| name=Tecma FX | image= | caption= }}{{Infobox aircraft type | type=Hang glider | national origin=France | manufacturer=Tecma Sport | designer= | first flight= | introduced= | retired= | status=Production completed | primary user= | more users= | produced= mid-2000s | number built= | developed from= | variants with their own articles= }} |
The Tecma FX is a French high-wing, single-place, hang glider that was designed and produced by Tecma Sport of La Roche-sur-Foron. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 50. Pagefast Ltd, Lancaster OK, 2003. {{ISSN|1368-485X}}
Design and development
The FX is made from aluminum tubing, with the double-surface wing covered in Dacron sailcloth. Its wing is cable braced from a single kingpost. The nose angle is 130° for both models.
The models are each named for their wing area in square metres and decimals of square metres.
Variants
;FX 136
:Small-sized model for lighter pilots. Its {{convert|10.3|m|ft|1|abbr=on}} span wing is cable braced from a single kingpost. The nose angle is 130°, wing area is {{convert|13.6|m2|sqft|abbr=on}} and the aspect ratio is 7.8:1. The pilot hook-in weight range is {{convert|60|to|80|kg|lb|0|abbr=on}}.
;FX 142
:Large-sized model for heavier pilots. Its {{convert|10.6|m|ft|1|abbr=on}} span wing is cable braced from a single kingpost. The nose angle is 130°, wing area is {{convert|14.2|m2|sqft|abbr=on}} and the aspect ratio is 7.9:1. The pilot hook-in weight range is {{convert|75|to|90|kg|lb|0|abbr=on}}. The glider model is DHV certified.
Specifications (FX 136)
{{Aircraft specs
|prime units?=met
|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=10.3
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=13.6
|wing area sqft=
|wing area note=
|aspect ratio=7.8:1
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|more general=
|perfhide=Y
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|g limits=
|roll rate=
|glide ratio=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|more performance=
}}