JPM 01 Médoc

{{Short description|French homebuilt aircraft}}

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

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

{{Infobox aircraft begin

| name=JPM 01 Médoc

| image=

| caption=

}}{{Infobox aircraft type

| type=Amateur-built aircraft

| national origin=France

| manufacturer=Avions Jean-Pierre Marie (JPM)

| designer=Jean-Pierre Marie

| first flight=

| introduced=1987

| retired=

| status=Plans available (2015)

| primary user=

| more users=

| produced=

| number built=

| developed from=

| variants with their own articles=

}}

The JPM 01 Médoc is a French amateur-built aircraft that was designed by Jean-Pierre Marie in 1987 and produced by Avions Jean-Pierre Marie (JPM) of Le Mesnil-Esnard. The aircraft is supplied as plans for amateur construction.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 105. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 112. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

The aircraft is named for the French community of Médoc.

Design and development

The Médoc features a cantilever low wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration.

The aircraft is made from wood with its flying surfaces covered in doped aircraft fabric. Its {{convert|7.50|m|ft|1|abbr=on}} span wing has an area of {{convert|9.30|m2|sqft|abbr=on}} and mounts flaps. Standard engines recommended are {{convert|60|kW|hp|0|abbr=on}}-class Volkswagen air-cooled engines, including the {{convert|60|kW|hp|0|abbr=on}} Limbach L2000 four-stroke powerplant.

Almost thirty years after its introduction the aircraft was redesigned and lightened, gaining slotted flaps to reduce stall speed.

Specifications (JPM 01 Médoc)

{{Aircraft specs

|ref=Bayerl, Tacke and JPM{{cite web|url = http://jpm.lamaiziere.net/photos_site_jpm/medoc.pdf|title = Le JPM 01 " Médoc "|accessdate = 4 October 2012|last = JPM|date = n.d.|archive-date = 4 March 2016|archive-url = https://web.archive.org/web/20160304001731/http://jpm.lamaiziere.net/photos_site_jpm/medoc.pdf|url-status = dead}}

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=6

|length ft=

|length in=

|length note=

|span m=7.50

|span ft=

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=9.30

|wing area sqft=

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=286

|empty weight lb=

|empty weight note=

|gross weight kg=496

|gross weight lb=

|gross weight note=

|fuel capacity={{convert|60|L}}

|more general=

|eng1 number=1

|eng1 name=Limbach L2000

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

|eng1 kw=60

|eng1 hp=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=210

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=175

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=70

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=247

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=700

|range miles=

|range nmi=

|range note= with no reserve

|endurance=4 hours plus 0.5 hour reserve

|ceiling m=4100

|ceiling ft=

|ceiling note=

|g limits=+3.5/–1.5

|roll rate=

|glide ratio=

|climb rate ms=4

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=53.3

|wing loading lb/sqft=

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

{{reflist}}