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Potez 25
History
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Technical details
Manufacturer Etablissements Henry Potez Class Light attack, army co-operation and tactical reconnaissance warplane Data for Potez 25TOE.2 Armament One 0.303 in (7.7 mm) Vickers or 7.5 mm (0.295 in) Darne fixed forward-firing machine gun in the forward fuselage with synchronization equipment to fire through the propeller disc, and two 0.303 in (7.7 mm) Lewis or 7.5 mm (0.295 in) Darne trainable rearward-firing machine guns in the rear cockpit
Up to 200 kg (441 lb) of disposable stores carried on four hardpoints (all under the wings with each unit rated at 50 kg/110 lb), and generally comprising four 50 kg (110 lb) bombsEquipment Standard communication and navigation equipment, plus optical sights and provision for a reconnaissance camera In service 1926 to early 1945 Crew Pilot and observer/gunner in tandem in open cockpits Speed Maximum: 208 km/h (129 mph; 112 kt) at sea level Range Maximum: 1260 km (783 miles; 680 nm)
typical: 630 km (391.5 miles; 340 nm)Ceiling 5800 m (19,030 ft) Climb 3000 meters (9,845 ft) in 5 minutes 41 seconds Engine One Lorraine-Dietrich 12Eb W-type piston engine rated at 450 hp (336 kW) at optimum altitude Internal fuel Length 9.10 meters (29 ft 10.25 in) Height 3.67 meters (12 ft 0.25 in) Wing Span: 14.14 meters (46 ft 4.75 in)
area 47.00 m2 (505.92 sq ft)Weight empty: 1510 kg (3,329 lb)
normal take-off 2238 kg (4,934 lb)
maximum take-off: 2500 kg (5,511 lb)Operators
China ? Estonia ? Ethiopia ? France 3,250+ Greece ? Latvia ? NDH 24 Paraguay ? Poland 300 Portugal 27 Rumania 70 Spain ? Switzerland ? Uruguay ? USSR ? Yugoslavia 200