Arnet Pereyra Sabre II

{{Infobox Aircraft Begin

| name=Arnet Pereyra Sabre II

| image=

| caption=

}}{{Infobox Aircraft Type

| type=Kit aircraft

| national origin=United States

| manufacturer=Arnet Pereyra Inc

| designer=Jose Cryrillo Veraga

| first flight=July 1992

| introduced=

| retired=

| status=

| primary user=

| more users=

| produced= 1992-c2003

| number built=3 (2001)

| program cost=

| unit cost= US$18,600 (Kit price 2001, including engine, propeller and instruments)

| developed from= Advanced Aeromarine Buccaneer

| variants with their own articles=

}}

The Arnet Pereyra Sabre II is an American, two-seats in side-by-side configuration, conventional landing gear-equipped, strut-braced, high-wing ultralight trainer that was produced by Arnet Pereyra Inc of Rockledge, Florida in kit form for amateur construction.Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page B-99. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 117. BAI Communications. {{ISBN|0-9636409-4-1}}Downey, Julia: 1999 Kit Aircraft Directory, Kitplanes, Volume 15, Number 12, December 1998, page 36. Primedia Publications. ISSN 0891-1851Downey, Julia: 2001 Kit Aircraft Directory, Kitplanes, Volume 17, Number 12, December 2000, page 29. Kitplanes Acquisition Company. ISSN 0891-1851Downey, Julia: 2002 Kit Aircraft Directory, Kitplanes, Volume 18, Number 12, December 2001, page 21 & 86. Kitplanes Acquisition Company. ISSN 0891-1851

Design and development

First flown in July 1992, the Sabre II is a land version of the highly successful 1984-vintage Arnet Pereyra Buccaneer, which the company produced at the same time. The Sabre II was developed from the two seat Buccaneer II by removing the wing-tip floats, replacing the retractable landing gear with leaf-spring fixed landing gear, shortening the wing by {{convert|12|in|cm|0|abbr=on}} and replacing the boat-hull with a new fiberglass lower fuselage. The lower fuselage was more streamlined than the boat-hull and was lighter as well. Overall the Sabre II is more than {{convert|100|lb|kg|0|abbr=on}} lighter than the Buccaneer II, with an empty weight of {{convert|480|lb|kg|0|abbr=on}}.

The Sabre is constructed from bolted aluminium tubing, covered in pre-sewn Dacron sailcloth envelopes. Standard aircraft dope and fabric is optional. The standard engine is the {{convert|64|hp|kW|0|abbr=on}} liquid-cooled two-stroke Rotax 582 and the acceptable power range is {{convert|64|to|75|hp|kW|0|abbr=on}}. When in production a Ballistic Recovery Systems parachute was standard.

The Sabre II was not a commercial success, with only three reported delivered by 2001 and the aircraft was dropped from the company line when the company was renamed Aero Adventure Aviation circa 2003.Newby-Gonzalez, Tori: 2004 Kit Aircraft Directory, Kitplanes, Volume 20, Number 12, December 2003, page 37. Belvoir Publications. ISSN 0891-1851

Specifications (version)

{{Aircraft specs

|ref=Cliche

|prime units?=imp

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=22

|length in=4

|length note=

|span m=

|span ft=29

|span in=8

|span note=

|height m=

|height ft=7

|height in=0

|height note=

|wing area sqm=

|wing area sqft=156

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=480

|empty weight note=

|gross weight kg=

|gross weight lb=1100

|gross weight note=

|fuel capacity=12 US gallons (45litres)

|more general=

|eng1 number=1

|eng1 name=Rotax 582

|eng1 type=

|eng1 kw=

|eng1 hp=64

|prop blade number=2

|prop name=Ivoprop

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=90

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=70

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=32

|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=150

|range nmi=

|range note=

|endurance=

|ceiling m=

|ceiling ft=14000

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=500

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=7.05

|wing loading note=

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|avionics=

}}

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References