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Jean-Pierre Marie (JPM) JPM 01 Médoc / Tanagra



The JPM 01 Médoc is a French amateur-built aircraft that was designed by Jean-Pierre Marie in 1977 and produced by Les Avions Jean-Pierre Marie (JPM) of Le Mesnil-Esnard. The aircraft is supplied as plans for amateur construction, available in 2012 from Les Avions Jean-Pierre Marie (JPM).

The aircraft is named for the French community of Médoc.

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 7.50 m (24.6 ft) span wing has an area of 9.30 sq.m (100.1 sq ft) and mounts flaps. Standard engines recommended are 60 kW (80 hp)-class Volkswagen air-cooled engines, including the 60 kW (80 hp) Limbach L2000 four-stroke powerplant.

The first example was completed by Pierre-Claude Guillem, and registered F-PGMB. It first flew on September 8, 1987. Originally fitted with a 65 hp JPX 4T-60A engine, it later received an 80 hp Limbach L2000 and the aircraft was winner of the 1988 SFACT Trophy for best multi place design. The JPM-01 built by the designer himself was first flown in August 1993, registered as F-PJPM.

A diesel engine powered version was designated JPM-01 Médoc Provence and the first example was completed by Didier Davenna in 2005. He had it registered as F-PDVN under the designation JPM-01 DDI. By mid-2012 at least fourteen Médocs has been built.

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


JPM 01 Médoc /  JPM-01 Tanagra
Engine: 1 × Limbach L2000, 60 kW (80 hp)
Length: 6 m (19 ft 8 in)
Wingspan: 7.50 m (24 ft 7 in)
Wing area: 9.30 sq.m (100.1 sq ft)
Empty weight: 286 kg (631 lb)
Gross weight: 496 kg (1,093 lb)
Fuel capacity: 60 litres (13 imp gal; 16 US gal)
Maximum speed: 210 km/h (130 mph; 113 kn)
Cruising speed: 175 km/h (109 mph; 94 kn)
Stall speed: 70 km/h (43 mph; 38 kn)
Never exceed speed: 247 km/h (153 mph; 133 kn)
Range: 700 km (435 mi; 378 nmi) with no reserve
Endurance: 4 hours plus 0.5 hour reserve
Service ceiling: 4,100 m (13,451 ft)
g limits: +3.5/–1.5
Rate of climb: 4 m/s (790 ft/min)
Wing loading: 53.3 kg/m2 (10.9 lb/sq ft)
Crew: one
Capacity: one passenger


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