Rainbow Cheetah

{{Short description|South African ultralight aircraft}}

{{Use dmy dates|date=December 2022}}

{{Use South African English|date=December 2022}}

{{Infobox Aircraft Begin

| name=Cheetah

| image=Rainbow Cheetah XLS N150RC.jpg

| caption=

}}{{Infobox Aircraft Type

| type=Ultralight aircraft and Light-sport aircraft

| national origin=South Africa

| manufacturer=Rainbow Aircraft

| designer=Vladimir Chechin

| first flight=

| introduced=

| retired=

| status=In production (2012)

| primary user=

| more users=

| produced=

| number built=

| developed from= Best Off Skyranger

| variants with their own articles=Rainbow Cheetah XLS

}}

The Rainbow Cheetah a South African ultralight and light-sport aircraft, designed by Vladimir Chechin and produced by Rainbow Aircraft. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 72. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

Design and development

The aircraft was derived from the Best Off Skyranger and designed to comply with Canadian Advanced Ultralight criteria and the US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit with optional doors for access, fixed tricycle landing gear or optionally conventional landing gear and a single engine in tractor configuration.{{cite web|url = http://www.sportpilot.org/learn/slsa/|title = EAA's Listing of Special Light-Sport Aircraft|accessdate = 1 June 2012|last = Experimental Aircraft Association|year = 2012|url-status = dead|archiveurl = https://web.archive.org/web/20140228070151/http://sportpilot.org/learn/slsa|archivedate = 28 February 2014}}

The aircraft is made from bolted-together aluminum tubing, with its flying surfaces covered in Dacron sailcloth. Its {{convert|9.6|m|ft|1|abbr=on}} span wing has an area of {{convert|13.25|m2|sqft|abbr=on}} and mounts flaps. Standard engines available are the {{convert|64|hp|kW|0|abbr=on}} Rotax 582 two-stroke, the {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL and the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS four-stroke powerplants.

The Cheetah XLS has been accepted by Transport Canada as an Advanced Ultralight as both a land plane and seaplane, powered by the Rotax 582 two-stroke, the Rotax 912UL, the Rotax 912ULS, the Verner VM133 and the {{convert|85|hp|kW|0|abbr=on}} Jabiru 2200A engines.{{cite web|url = http://www.tc.gc.ca/eng/civilaviation/standards/general-ccarcs-advancedullist-2036.htm|title = Listing of Models Eligible to be Registered as Advanced Ultra-Light Aeroplanes (AULA)|accessdate = 27 August 2012|last = Transport Canada|date = 15 August 2012}}

Operational history

By August 2012 there were three Cheetahs on the Federal Aviation Administration registry and two on the Transport Canada Civil Aircraft Register.{{cite web|url = http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=CHEETAH&PageNo=1|title = Make / Model Inquiry Results|accessdate = 27 August 2012|last = Federal Aviation Administration|date = 27 August 2012}}{{cite web|url = http://wwwapps2.tc.gc.ca/Saf-Sec-Sur/2/ccarcs/aspscripts/en/quicksearch.asp|title = Canadian Civil Aircraft Register|accessdate = 27 August 2012|last = Transport Canada|date = 27 August 2012|url-status = dead|archiveurl = https://web.archive.org/web/20110718042755/http://wwwapps2.tc.gc.ca/Saf-Sec-Sur/2/ccarcs/aspscripts/en/quicksearch.asp|archivedate = 18 July 2011}}

Variants

;Cheetah XLS

:Current production model (2012) with tricycle landing gear.{{cite web |url=http://www.rainbowaircraft.co.za/Products.html/3_axis_microlights.html/cheetah_xls.html/cheetah_xls.html |title=Rainbow Aircraft Cheetah XLS |publisher=Rainbowaircraft.co.za |accessdate=2012-08-27 |url-status=dead |archiveurl=https://web.archive.org/web/20120724104848/http://www.rainbowaircraft.co.za/Products.html/3_axis_microlights.html/cheetah_xls.html/cheetah_xls.html |archivedate=2012-07-24 }}

;Cheetah XLS Taildragger

:Current production model (2012) with conventional landing gear.{{cite web |url=http://www.rainbowaircraft.co.za/Products.html/3_axis_microlights.html/cheetah_xls_taildragger.html/cheetah_xls_taildragger.html |title=Rainbow Aircraft Cheetah XLS Taildragger |publisher=Rainbowaircraft.co.za |accessdate=2012-08-27 |url-status=dead |archiveurl=https://web.archive.org/web/20120724105013/http://www.rainbowaircraft.co.za/Products.html/3_axis_microlights.html/cheetah_xls_taildragger.html/cheetah_xls_taildragger.html |archivedate=2012-07-24 }}

Specifications (Cheetah XLS)

{{Aircraft specs

|ref=Bayerl and manufacturer{{cite web |url=http://www.rainbowaircraft.co.za/Products.html/specification.html/specification.html |title=Raindow Aircraft Cheetah XLS Specifications |publisher=Rainbowaircraft.co.za |accessdate=2012-08-27 |url-status=dead |archiveurl=https://web.archive.org/web/20120724104946/http://www.rainbowaircraft.co.za/Products.html/specification.html/specification.html |archivedate=2012-07-24 }}

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=5.67

|length ft=

|length in=

|length note=

|span m=9.6

|span ft=

|span in=

|span note=

|height m=1.9

|height ft=

|height in=

|height note=to top of wing

|wing area sqm=13.25

|wing area sqft=

|wing area note=

|aspect ratio=7.01

|airfoil=

|empty weight kg=248

|empty weight lb=

|empty weight note=

|gross weight kg=560

|gross weight lb=

|gross weight note=

|fuel capacity={{convert|100|L}}

|more general=

|eng1 number=1

|eng1 name=Rotax 912UL

|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine

|eng1 kw=60

|eng1 hp=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=177

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=135

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=35

|stall speed kts=

|stall speed note=flaps down

|never exceed speed kmh=

|never exceed speed mph=125

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=670

|range nmi=

|range note=with reserves

|endurance=7.5 hours

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=+6g/-4g

|roll rate=

|glide ratio=10:1

|climb rate ms=5.3

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=42.3

|wing loading lb/sqft=

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

{{reflist|30em}}