Junkers 38 G
The Junkers G.38 was a large German four-engined transport aircraft which first flew in 1929. Two prototypes were constructed in Germany. Both aircraft flew as a commercial transport within Europe in the years leading up to World War II.
Structurally the G38 conformed to standard Junkers’ practice, with a multi-tubular spar cantilever wing covered, like the rest of the aircraft in stressed, corrugated duraluminium. The biplane tail, found in other large aircraft of the time was intended to reduce rudder forces; initially there were three rudders with only a central fixed fin. The undercarriage was fixed, with double tandem main wheels that were initially enclosed in very large spats. The wing had the usual Junkers "double wing" form, the name referring to the full span movable flaps which served also as ailerons in the outer part.
The first Junkers prototype—3301 and marked as D-2000—first flew on 6 November 1929 with four diesel engines: two L55 12-cylinder V-motors and two 294 kW L8 6-cylinder inline motors with combined power rating of 1470 kW (1971 hp). The Reich Air Ministry purchased the D-2000 for demonstration flights, and took delivery on 27 March 1930. In flight tests, the G.38 set four world records including speed, distance and duration for airplanes lifting a 5000 kg payload. On 2 May 1930 Lufthansa put the D-2000 into commercial service for both scheduled and chartered flights.
( Wikipedia: https://en.wikipedia.org/wiki/Junkers_G.38 )
Beware of the loe Climbrate!
Passanger: 9 (for TPF)
Power: 2×600 + 2×400 PS PS
Speed: 174 MPH
Construction year: 1929 – 1945
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