In the photo the P.M.01 is accompanied by the Stampe et Vertongen SV.4C (F-BCXK c/n 445) that was also in use with the Aero-Club du Canton de Sceaux.
TYPE. Single-seat light monoplane.
WINGS. High-wing braced monoplane. NACA 23012 wing section. Two-spar wood structure with fabric covering. V-bracing struts.
FUSELAGE. Wood framework with fabric covering.
TAIL UNIT. Cantilever monoplane type. Wood framework, fabric covering.
LANDING GEAR. Fixed tail-wheel type.
POWERPLANT. A 25 hp Volkswagen four-cylinder horizontally-opposed air-cooled engine. Merville two-blade wood airscrew. Two fuel tanks in wings. Total fuel capacity 11.9 gal (45 l).
ACCOMMODATION. Single open cockpit.
Span: 23 ft 3.5 in (7.10 m)
Length: 16 ft 5 in (5.00 m)
Wing area: 87.7 sq.ft (8.15 sq.m)
Wing chord, constant: 4 ft 1 in (1.25 m)
Empty weight: 275 lb (125 kg)
Loaded weight: 495 lb (225 kg)
Wing loading: 5.53 lb/sq.ft (27 kg/sq.m)
Max speed: 77.6 mph (125 kmh)
Cruise speed: 68.3 mph (110 kmh)
Climb: 262 ft (80 m)/min."