Airborne T-Lite

{{Short description|Australian ultralight trike}}

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

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

{{Infobox aircraft begin

| name=T-Lite

| image=

| caption=

}}{{Infobox aircraft type

| type=Ultralight trike

| national origin=Australia

| manufacturer=Airborne Windsports

| designer=

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| introduced=

| retired=

| status=In production (2013)

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The Airborne T-Lite is an Australian ultralight trike, designed and produced by Airborne Windsports of Redhead, New South Wales. The aircraft is supplied as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 201. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

Design and development

The T-Lite was designed as both a cross country powered aircraft and self-launching motor glider for soaring. The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category as well as the US FAR 103 Ultralight Vehicles rules. It features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat open cockpit, tricycle landing gear and a single engine in pusher configuration.

The aircraft is made from bolted-together aluminium tubing, with its double surface Airborne Core wing covered in Dacron sailcloth, with the top surface finished in mylar PX cloth. The {{convert|9.5|m|ft|1|abbr=on}} span Core wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a purpose-designed, single cylinder, air-cooled, four-stroke, {{convert|22|hp|kW|0|abbr=on}} Bailey B200 engine, with electric starting and a 3.2:1 reduction drive. The aircraft has an empty weight of {{convert|90|kg|lb|0|abbr=on}} and a gross weight of {{convert|210|kg|lb|0|abbr=on}}, giving a useful load of {{convert|120|kg|lb|0|abbr=on}}. With full fuel of {{convert|10|L}} the payload is {{convert|113|kg|lb|0|abbr=on}}. The permitted pilot weight range is {{convert|50|to|110|kg|lb|0|abbr=on}}.{{cite web|url = http://www.airborne.com.au/pages/ml_t-lite_specs.php|title = T-Lite Specifications |accessdate = 15 March 2013|last = Airborne Windsports|year = 2011}}

The T-Lite is designed to be quickly disassembled for ground transport. The {{convert|10|L}} fuel tank is located behind the pilot's seat and can be disconnected quickly to allow transporting it independently of the aircraft for refueling.

Specifications (T-Lite)

{{Aircraft specs

|ref=Bayerl and Airborne Windsports

|prime units?=met

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|crew=one

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|length m=2.2

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|span m=9.5

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|height m=3.4

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|wing area sqm=15.6

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|empty weight kg=90

|empty weight lb=

|empty weight note=

|gross weight kg=210

|gross weight lb=

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|fuel capacity={{convert|10|L}}

|more general=

|eng1 number=1

|eng1 name=Bailey B200

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

|eng1 kw=

|eng1 hp=22

|prop blade number=2

|prop name=Helix-Carbon H30F L-M-08-2

|prop dia m=1.3

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|max speed kmh=

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|cruise speed kmh=58

|cruise speed mph=

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|stall speed kmh=32

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=85

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|never exceed speed note=

|range km=239

|range miles=

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|endurance=

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits= +4/0g (flight limits) +6/-3g (ultimate load limits)

|roll rate=

|glide ratio=7.82:1

|climb rate ms=1.6

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=1.6

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|lift to drag=

|wing loading kg/m2=

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}}

References

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