Falconar Minihawk

{{Short description|Canadian homebuilt light aircraft}}

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

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

{{Infobox aircraft begin

| name=Minihawk

| image=File:Falconar Minihawk Prototype.jpg

| caption=Minihawk prototype

}}{{Infobox aircraft type

| type=Amateur-built aircraft

| national origin=Canada

| manufacturer=Falconar Avia
Manna Aviation

| designer=

| first flight=

| introduced=

| retired=

| status=In production (2019)

| primary user=

| more users=

| produced=

| number built=At least one

| developed from=

| variants with their own articles=

}}

The Falconar Minihawk is a Canadian amateur-built aircraft, originally produced by Falconar Avia. The aircraft is supplied as a kit or plans for amateur construction.Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 162-164. BAI Communications. {{ISBN|0-9636409-4-1}}

Since the winding up of business by Falconar Avia in 2019, the plans are now sold by Manna Aviation.{{cite web|url = http://falconaravia.com/|title = Notification of Closure|access-date = 4 July 2019|author=Falconar Avia |work = falconaravia.com|date = 30 June 2019|archiveurl = https://web.archive.org/web/20190704172308/http://falconaravia.com/|archivedate =4 July 2019}}

Design and development

The aircraft features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a sliding canopy, fixed tricycle landing gear or, optionally, conventional landing gear, and a single engine in tractor configuration.

The Minihawk is made from wood, with its flying surfaces covered in doped aircraft fabric. Its {{convert|25.5|ft|m|1|abbr=on}} span wing has an area of {{convert|106|sqft|m2|abbr=on}} and mounts flaps. The cockpit is {{convert|40|in|cm|0|abbr=on}} wide. The aircraft's recommended engine power range is {{convert|65|to|100|hp|kW|0|abbr=on}} and standard engines used include the {{convert|100|hp|kW|0|abbr=on}} Continental O-200 four-stroke powerplant. Construction time from the supplied kit is estimated as 1500 hours.{{cite web|url = http://members.shaw.ca/falconark/FA/minihawk.htm|title = Minihawk|accessdate = 11 November 2012|last = Falconar Avia|date = 1 July 2012}}

Operational history

Even though a prototype was constructed, by November 2012 no examples were registered in its home country with Transport Canada.{{cite web|url=http://wwwapps2.tc.gc.ca/Saf-Sec-Sur/2/ccarcs/aspscripts/en/quicksearch.asp |title=Canadian Civil Aircraft Register |access-date=11 November 2012 |last=Transport Canada |date=11 November 2012 |url-status=dead |archive-url=https://web.archive.org/web/20110718042755/http://wwwapps2.tc.gc.ca/Saf-Sec-Sur/2/ccarcs/aspscripts/en/quicksearch.asp |archive-date=18 July 2011 |df= }}

Specifications (Minihawk)

{{Aircraft specs

|ref=Purdy

|prime units?=imp

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=18

|length in=0

|length note=

|span m=

|span ft=25

|span in=6

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=

|wing area sqft=106

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=

|empty weight lb=645

|empty weight note=

|gross weight kg=

|gross weight lb=1070

|gross weight note=

|fuel capacity={{convert|15|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Continental O-200

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

|eng1 kw=

|eng1 hp=100

|prop blade number=2

|prop name=metal

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=128

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=115

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=50

|stall speed kts=

|stall speed note=flaps down

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=570

|range nmi=

|range note=

|endurance=

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=1350

|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=10.0

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

See also

References

{{Reflist}}