Soaring Concepts Sky Trek

{{Short description|American powered parachute}}

{{Use mdy dates|date=January 2022}}

{{Use American English|date=January 2022}}

{{Infobox aircraft begin

| name= Sky Trek

| image=

| caption=

}}{{Infobox aircraft type

| type=Powered parachute

| national origin=United States

| manufacturer=Soaring Concepts

| designer=

| first flight=

| introduced=2000

| retired=

| status=In production (2015)

| primary user=

| more users=

| produced= 2000-present

| number built=at least 25

| developed from=

| variants with their own articles=

}}

The Soaring Concepts Sky Trek is an American powered parachute, designed and produced by Soaring Concepts Inc of Sturgis, Michigan and introduced in 2000. The aircraft is supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 86. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X{{cite web|url=http://soaringconcepts.com/aboutus.html|title=About Us|work=soaringconcepts.com|accessdate=20 August 2015}}

Design and development

The Sky Trek was designed to comply with the US light-sport aircraft rules and is on the list of Federal Aviation Administration accepted LSAs. It features a {{convert|500|sqft|m2|abbr=on}} parachute-style wing, two-seats-in-tandem accommodation, tricycle landing gear and a single {{convert|64|hp|kW|0|abbr=on}} Rotax 582 engine in pusher configuration.{{cite web|url = http://www.faa.gov/aircraft/gen_av/light_sport/media/SLSA_Directory.xls|title = SLSA Make/Model Directory|accessdate = 20 August 2015|last = Federal Aviation Administration|date = 30 April 2015}}{{cite web|url=http://soaringconcepts.com/specifications.html|title=Specifications|work=soaringconcepts.com|accessdate=20 August 2015}}

The aircraft carriage is built from large-diameter 4130 steel tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The main landing gear incorporates adjustable gas shock suspension.{{cite web|url=http://soaringconcepts.com/|title=Soaring Concepts|work=soaringconcepts.com|accessdate=20 August 2015}}

The aircraft has an empty weight of {{convert|384|lb|kg|0|abbr=on}} and a gross weight of {{convert|950|lb|kg|0|abbr=on}}, giving a useful load of {{convert|566|lb|kg|0|abbr=on}}. With full fuel of {{convert|10|u.s.gal}} the payload for crew and baggage is {{convert|506|kg|lb|0|abbr=on}}.

The standard day, sea level, no wind, take off with a {{convert|64|hp|kW|0|abbr=on}} engine is {{convert|200|ft|m|0|abbr=on}} and the landing roll is {{convert|100|ft|m|0|abbr=on}}.

Operational history

In August 2015, 24 examples were registered in the United States with the Federal Aviation Administration, although a total of 25 had been registered at one time.{{cite web|url = http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=SKY+TREK&PageNo=1|title = Make / Model Inquiry Results|accessdate = 20 August 2015|last = Federal Aviation Administration|date = 20 August 2015}}

Specifications (Sky Trek)

{{Aircraft specs

|ref=Bertrand and manufacturer

|prime units?=imp

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=10

|length in=2

|length note=

|span m=

|span ft=32.9

|span in=

|span note=

|height m=

|height ft=7

|height in=0

|height note=carriage only

|wing area sqm=

|wing area sqft=500

|wing area note=

|aspect ratio=2.17:1

|airfoil=

|empty weight kg=

|empty weight lb=385

|empty weight note=

|gross weight kg=

|gross weight lb=950

|gross weight note=

|fuel capacity={{convert|10|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Rotax 582

|eng1 type=twin cylinder, two-stroke, liquid-cooled aircraft engine

|eng1 kw=

|eng1 hp=64

|prop blade number=3

|prop name=PowerFin ground adjustable, composite

|prop dia m=

|prop dia ft=5

|prop dia in=3

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=32

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=30

|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=

|range km=

|range miles=

|range nmi=

|range note=

|endurance=

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=4:1

|climb rate ms=

|climb rate ftmin=900

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=1.9

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

{{reflist}}