Team Tango Foxtrot

{{Short description|American homebuilt aircraft}}

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

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

{{Infobox aircraft begin

| name=Foxtrot

| image=Team Tango Foxtrot 4 N190KT.jpg

| caption=

}}{{Infobox aircraft type

| type=Amateur-built aircraft

| national origin=United States

| manufacturer=Team Tango

| designer=

| first flight=

| introduced=

| retired=

| status=In production (2012)

| primary user=

| more users=

| produced=

| number built=3 (2011)

| developed from= Team Tango Tango 2

| variants with their own articles=

}}

The Team Tango Foxtrot, or Foxtrot 4, is an American amateur-built aircraft, designed and produced by Team Tango of Williston, Florida. The aircraft is supplied as a kit for amateur construction, with or without factory builder assistance.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 123. WDLA UK, Lancaster UK, 2011. {{ISSN|1368-485X}}Vandermeullen, Richard: 2012 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 71. Belvoir Publications. {{ISSN|0891-1851}}

Design and development

The Foxtrot was developed as a four-seat version of the Tango 2 and shares many of the two-seater's features. The Foxtrot has a cantilever low-wing, a four-seat enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration. The rear seats have limited visibility.

The aircraft is made from composites. Its {{convert|32|ft|m|1|abbr=on}} span wing employs a NACA 64-415 airfoil, has an area of {{convert|128|sqft|m2|abbr=on}} and mounts flaps. The engines recommended are Lycoming Engines of {{convert|200|to|350|hp|kW|0|abbr=on}}.{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage|accessdate = 3 January 2012|last = Lednicer|first = David|authorlink = |year = 2010|archive-url = https://web.archive.org/web/20100420012244/http://www.ae.illinois.edu/m-selig/ads/aircraft.html|archive-date = 20 April 2010|url-status = dead}}

Operational history

By October 2012 three examples had been registered in the United States with the Federal Aviation Administration.{{cite web|url = http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=FOXTROT&PageNo=1|title = Make / Model Inquiry Results|accessdate = 24 October 2012|last = Federal Aviation Administration|date = 24 October 2012}}

Specifications (Foxtrot)

{{Aircraft specs

|ref=Bayerl

|prime units?=imp

|genhide=

|crew=one

|capacity=three passenger

|length m=

|length ft=

|length in=

|length note=

|span m=9.75

|span ft=

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=11.9

|wing area sqft=

|wing area note=

|aspect ratio=

|airfoil=NACA 64-415

|empty weight kg=634

|empty weight lb=

|empty weight note=

|gross weight kg=1170

|gross weight lb=

|gross weight note=

|fuel capacity={{convert|110|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Lycoming O-540

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

|eng1 kw=

|eng1 hp=350

|prop blade number=3

|prop name=constant speed

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=368

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=348

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=92

|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=

|climb rate ms=12

|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=98.3

|wing loading lb/sqft=

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

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