Eagle EA-100

{{Short description|American light aircraft}}

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

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

{{Infobox aircraft begin

| name= EA-100 S-LSA

| image=Eagle EA-100 N700EW.jpg

| caption=

}}{{Infobox aircraft type

| type=Light-sport aircraft

| national origin=United States

| manufacturer=Eagle Aviation LLC

| designer=

| first flight=

| introduced=2008

| retired=

| status=Production completed

| primary user=

| more users=

| produced= 2008-2013

| number built=2

| developed from=

| variants with their own articles=

}}

The Eagle EA-100 is an American light-sport aircraft that was designed and produced by Eagle Aviation LLC of Oshkosh, Wisconsin and introduced in 2008. When it was available the aircraft was supplied as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 42. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

The company website expired in March 2013 and was not renewed. It is likely that the company is out of business and production has ended.{{Cite web|url=http://eaglesportplane.com/|archive-url=https://web.archive.org/web/20130501013854/http://eaglesportplane.com/|url-status=dead|archive-date=May 1, 2013|title=eaglesportplane.com|date=May 1, 2013}}

Design and development

The EA-100 was designed to comply with the US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed by two vertical-hinged doors, fixed tricycle 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|date = 2012|archive-url = https://web.archive.org/web/20140228070151/http://sportpilot.org/learn/slsa|archive-date = 28 February 2014|url-status = dead}}

The aircraft is made from aluminum sheet. Its {{convert|28.5|ft|m|1|abbr=on}} span wing has an area of {{convert|135|sqft|m2|abbr=on}} and features electrically operated flaps. The standard engine is the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS four-stroke powerplant while the standard propeller is a Sensenich composite ground adjustable type.{{cite web|url=http://eaglesportplane.com/ea100slsa.asp |title=Sport Aircraft for the Sport Pilot |publisher=Eaglesportplane.com |date= |accessdate=2012-06-08}}

Operational history

By August 2019 two examples had been registered with the US Federal Aviation Administration.{{cite web|url = https://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=EAGLE+AIRCRAFT+CO+LLC&Modeltxt=EA-100&PageNo=1|title = Make / Model Inquiry Results|accessdate = 1 August 2019|author = Federal Aviation Administration|date = 1 August 2019}}

Specifications (version)

{{Aircraft specs

|ref=Bayerl and Eagle Aviation LLC{{cite web|url = http://eaglesportplane.com/specsperf.asp|title = EA-100 S-LSA Specifications and Performance|accessdate = 5 June 2012|last = Eagle Aviation LLC|year = 2012}}

|prime units?=kts

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=20

|length in=9

|length note=

|span m=

|span ft=28

|span in=6

|span note=

|height m=

|height ft=7

|height in=3

|height note=

|wing area sqm=

|wing area sqft=135

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=825

|empty weight note=

|gross weight kg=

|gross weight lb=1320

|gross weight note=

|fuel capacity={{convert|75|L}}

|more general=

|eng1 number=1

|eng1 name=Rotax 912ULS

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

|eng1 kw=75

|eng1 hp=

|prop blade number=2

|prop name=Sensenich composite, ground adjustable

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=105

|cruise speed note=

|stall speed kmh=

|stall speed mph=

|stall speed kts=35

|stall speed note=flaps down

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=120

|never exceed speed note=

|range km=

|range miles=

|range nmi=335

|range note=

|endurance=

|ceiling m=

|ceiling ft=10000

|ceiling note=

|g limits=+5/-3g

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=1200

|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=

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

{{reflist}}