The J40 design was a parallel developement to the Junkers G38 passenger airliner. Since 1926 several designs for a giant seaplane were under research at Junkers Flugzeugwerke as an alternate approach to the Junkers G38 landplane studies.
An early design of 1926 is known as Postflugboot Design Nr. 15, which was a flying boat approach with two swimmers. When the G38 became more concrete, an intermediate idea of Junkers was to take the standard G38 fuselage and put it on swimmers. This swimmer design was actually called J40. However, the Junkers design office had doubt, that such a large aircraft could be put on swimmers. Therefore in 1928 the seaplane design returned to boat layout again, picking up the Junkerissime double fuselage layout.
At this stage of design a decision was made, that Junkers should be supported by the German government for his giant landplane design G38, while Dornier was selected for the giant seaplane developement of the Do X. The German Navy still showed interest in the J40 flying boat design. Experiences from the Do X and Rohrbach Romar showed, that large scale seaplanes at the end of the twenties had not sufficent ranges to cross the Atlantic Ocean due to their heavy weight. Therefore the Reichsverkehrsministerium and Lufthansa decided to stop any activities upon large scale flying boats and turned over to smaller swimmer boats as the later BV139. The further developements of the J40 flying boat therefore also came to an end in 1930.
Type Flying boat project J 40 Crew 5 + ? passengers Flying boat project 15 Crew ? + 14 passengers Flying boat project, Double fuselage
Engine 2 Junkers L8 + 2 2 Junkers  L88/55 3 Junkers Fo 3 2 Junkers L88
Dimensions Length 21,40 m , height  ,  span 44,0 m , wing area 280 m2  , Length 22,0  m , height  , span 40,0 m , wing area 190 m2 
Weights Empty , loaded  13000 kg, max. take off weight   payload 7000 kg Empty , loaded   kg, max. take off weight   payload kg Empty , loaded 12000  kg, max. take off weight   payload kg
Performance Max.. speed  210 km/h, cruising speed  , range 2300 km, endurance  , service ceiling   , climb