"},"prime units?":{"wt":"met\n"},"genhide":{"wt":""},"crew":{"wt":"5"},"capacity":{"wt":""},"length m":{"wt":"18.20"},"length note":{"wt":""},"upper span m":{"wt":"31.70"},"upper span note":{"wt":""},"lower span m":{"wt":"24"},"lower span note":{"wt":""},"height m":{"wt":"6"},"height note":{"wt":""},"wing area sqm":{"wt":"180"},"wing area note":{"wt":""},"aspect ratio":{"wt":"9.1 upper wing, 6.9 lower wing"},"airfoil":{"wt":""},"empty weight kg":{"wt":"470"},"empty weight note":{"wt":""},"gross weight kg":{"wt":"7200"},"gross weight note":{"wt":""},"max takeoff weight kg":{"wt":""},"max takeoff weight lb":{"wt":""},"max takeoff weight note":{"wt":""},"fuel capacity":{"wt":"{{convert|1590|L|Impgal USgal|abbr=on}}"},"more general":{"wt":""},"eng1 number":{"wt":"3"},"eng1 name":{"wt":"[[Panhard-Levassor 12C]]b"},"eng1 type":{"wt":"water-cooled [[V-12 engine|V-12]]"},"eng1 hp":{"wt":"340"},"eng1 note":{"wt":""},"more power":{"wt":""},"prop blade number":{"wt":"4"},"prop name":{"wt":""},"prop dia m":{"wt":""},"prop dia ft":{"wt":""},"prop dia in":{"wt":""},"prop dia note":{"wt":""},"perfhide":{"wt":""},"max speed kmh":{"wt":"150"},"max speed note":{"wt":"at {{convert|500|m|ft|abbr=on}}"},"cruise speed kmh":{"wt":"120"},"cruise speed mph":{"wt":""},"cruise speed kts":{"wt":""},"cruise speed note":{"wt":""},"stall speed kmh":{"wt":""},"stall speed mph":{"wt":""},"stall speed kts":{"wt":""},"stall speed note":{"wt":""},"never exceed speed kmh":{"wt":""},"never exceed speed mph":{"wt":""},"never exceed speed kts":{"wt":""},"never exceed speed note":{"wt":""},"minimum control speed kmh":{"wt":""},"minimum control speed mph":{"wt":""},"minimum control speed kts":{"wt":""},"minimum control speed note":{"wt":""},"range km":{"wt":"950"},"range note":{"wt":"at cruising speed"},"ceiling m":{"wt":""},"ceiling ft":{"wt":""},"ceiling note":{"wt":""},"g limits":{"wt":""},"roll rate":{"wt":""},"glide ratio":{"wt":""},"climb rate ms":{"wt":""},"climb rate ftmin":{"wt":""},"climb rate note":{"wt":""},"time to altitude":{"wt":"19 min to {{convert|2000|m|ft|abbr=on}}"},"sink rate ms":{"wt":""},"sink rate ftmin":{"wt":""},"sink rate note":{"wt":""},"lift to drag":{"wt":""},"wing loading kg/m2":{"wt":""},"wing loading lb/sqft":{"wt":""},"wing loading note":{"wt":""},"fuel consumption kg/km":{"wt":""},"fuel consumption lb/mi":{"wt":""},"power/mass":{"wt":""},"more performance":{"wt":"*'''take-off distance and time at maximum load:''' {{convert|220|m|ft|abbr=on}}; 25 sec\n"},"guns":{"wt":"[[Machine gun]]s in nose and dorsal positions"},"bombs":{"wt":""}},"i":0}}]}" id="mwWA">Data from L'Aéronautique, November 1920 [1]
General characteristics
Performance
Armament
The Latécoère 4 was a three-engined, 15-passenger biplane built in France in the early 1920s. It proved difficult to fly and was discontinued, though a second machine was completed as the Latécoère 5 bomber.
The Caudron C.251 Et-2 was a French tandem seat, open cockpit biplane designed as an intermediate trainer and built in 1931. It did not go into production.
The Caudron C.140 was a French tandem cockpit sesquiplane designed in 1928 as a combination of liaison aircraft and observer and gunnery trainer.
The Caudron C.91 was a French single engine biplane with an enclosed passenger cabin seating four. It first flew in 1923.
The Caudron C.43 was the first French five-engined aircraft, a biplane intended for passenger transport or military use and multi-engined for safety. A development of the three-engined Caudron C.39, it had one tractor configuration engine in the nose and two push-pull pairs between the wings. It was capable of carrying eight passengers but was not developed.
The Caudron C.37 was a French three-engined biplane passenger transport, built in 1920. It could carry six passengers.
The Caudron C.33 "Landaulet Monsieur-Madame" was a French twin engined biplane with four seats, two in open cockpits and two in an enclosed cabin.
The Caudron C.25 was a large, three-engined, biplane airliner, designed and built in France soon after the end of World War I. Its enclosed cabin could accommodate up to eighteen passengers.
The Heinkel HD 20 was a twin engine, three seat German biplane built in 1926 for civil survey work.
The Latham HB.5 was a French biplane flying boat with four engines in push-pull configuration pairs. Ten were used by the French Navy.
The Latham E-5 was a large French Naval four engine biplane flying boat, flown in 1925. It was successfully tested but only one was built.
The CAMS 52 was a twin-engined floatplane torpedo-bomber. It was not ordered by the French Navy and only one CAMS 52 was completed. It first flew in the summer of 1930.
The Dornier Do S was a 22-passenger flying boat airliner flown in Germany in 1930.
The Latham L.1 was a French competitor in the 1923 Schneider Trophy race. It was a twin engine, biplane flying boat, built by Société Latham.
The Caproni Ca.61 was an Italian heavy day bomber aircraft of 1922. It was the final development of the Caproni three engine, twin boom biplane types developed during World War I, but it was not put into production.
The Potez 24 A.2 was a mid-1920s French biplane intended to replace the Potez 15 as an army observation aircraft. The further improved and larger Potez 25 was preferred for production.
The CAMS 54 was a strengthened and more powerful version of the French CAMS 51 civil transport and naval reconnaissance flying boat, developed for transatlantic flights. It is sometimes referred to as the 54 GR.
The Cañete Pirata, also known as Hidro Antonio Cañete de Reconocimiento (HACR), was a Spanish military parasol wing, single-engined flying boat flown in the late 1920s. Only one was built.
The LFG V 8 Bärbel (Barbel) in English) was a small, single-engined, biplane flying boat which carried two passengers. The sole example was built in Germany shortly after World War I but was exported and used for Baltic flights.
The Zeppelin-Lindau Gs.I, often known post-WWI as the Dornier Gs.I after its designer Claude Dornier, was a civil flying boat developed immediate post-war from a military prototype. Its passenger cabin seated six. Only one was completed, and that was eventually scuttled to keep it out of Allied hands. Another of the military prototypes was intended to have a bigger, nine seat cabin and other refinements but the Gs.II was incomplete when discovered by Allied inspectors.