Bushcaddy L-164

{{Short description|Canadian homebuilt light aircraft}}

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

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

{{Infobox aircraft begin

| name=Bushcaddy L-164

| image=

| caption=

}}{{Infobox aircraft type

| type=Kit aircraft

| national origin=Canada

| manufacturer=Canadian Light Aircraft Sales and Service (circa 2007-2011)
Bushcaddy (2011-present)

| designer=Sean Gilmore

| first flight=

| introduced=Circa 2007

| retired=

| status=In production

| primary user=

| more users=

| produced=

| number built=4 (December 2011)

| developed from= Bushcaddy L-162 Max

| variants with their own articles=

}}

The Bushcaddy L-164 is a Canadian kit aircraft that was designed by Sean Gilmore and produced by Canadian Light Aircraft Sales and Service and most recently by Bushcaddy. The aircraft is supplied as a kit for amateur construction.Vandermeullen, Richard: 2012 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 47. Belvoir Publications. ISSN 0891-1851{{cite web|url = http://bushcaddy.com/?page_id=113|title = L-164|accessdate = 21 May 2012|last = Bushcaddy|year = 2012|archiveurl = https://web.archive.org/web/20120208210646/http://bushcaddy.com/?page_id=113|archivedate = 8 February 2012|url-status = dead|df = }}Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 98. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XBertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 179. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 103. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

Design and development

The L-164 was developed from the Bushcaddy L-162 as a true four-seat aircraft. Unlike the L-160's designation, which indicates that the design engine for that model was originally a Lycoming O-320 of {{convert|160|hp|kW|0|abbr=on}}, the L-164 designation is just a numerical sequence and does not indicate horsepower.Hunt, Adam: Elegant Utility - Flying the CLASS R-80 BushCaddy, Canadian Flight July 2005, page B-1. Canadian Owners and Pilots Association.

The L-164 features a strut-braced high-wing, a four-seat enclosed cockpit, fixed conventional landing gear, or optionally tricycle landing gear, and a single engine in tractor configuration. Floats and skis can also be fitted.

The aircraft fuselage is made with a frame of welded 6061-T6 aluminum square tubing, covered in 6061-T6 sheet. Its {{convert|36|ft|m|1|abbr=on}} span wing employs V-struts with jury struts. The wing has an area of {{convert|189|sqft|m2|abbr=on}} and flaps. It can accept four-stroke powerplants from {{convert|180|to|250|hp|kW|0|abbr=on}}, with the Lycoming O-360 of {{convert|180|hp|kW|0|abbr=on}} and a Franklin Engine Company powerplant of {{convert|220|hp|kW|0|abbr=on}} commonly used. Cabin access is via two fold-up doors.

Construction time for the factory kit is estimated at 1200 hours or 300 hours from the quick-build kit. Four examples had been completed and flown by December 2011.

Variants

;L-164 B

:Passenger model.

;L-164 C

:All cargo model.

Specifications (L-164)

{{Aircraft specs

|ref=Kitplanes and Bushcaddy

|prime units?=imp

|genhide=

|crew=one

|capacity=three passengers

|length m=

|length ft=25

|length in=6

|length note=

|span m=

|span ft=36

|span in=0

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=

|wing area sqft=189

|wing area note=

|aspect ratio=

|airfoil=NACA 4413 (mod)

|empty weight kg=

|empty weight lb=1350

|empty weight note=

|gross weight kg=

|gross weight lb=2500

|gross weight note=

|fuel capacity={{convert|60|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Lycoming I0-360-L2A

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

|eng1 kw=

|eng1 hp=160

|prop blade number=2

|prop name=Sensenich 76EM8

|prop dia m=

|prop dia ft=6

|prop dia in=4

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=129

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=115

|cruise speed kts=

|cruise speed note=at 75% power

|stall speed kmh=

|stall speed mph=38

|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=750

|range nmi=

|range note=

|endurance=

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=+5.3/-3.2 (+3.8/-1.9 normal category)

|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=13.22

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

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