The Inspector wrote:
It is a DOUGLA A-20G unless the picture you are seeing is different from the color left side profile picture I see of U.S. ARMY A-20G-40-DO s/n 4321475 mfr l/n 21122 built in Santa Monica CA.
The 'balance weight' you think you see is the antenna wire lead tube in for the antenna wire running from the mid fuselage mast antenna up to the fixed vertical fin NOT the rudder. All control surfaces on the A-20 were frieze type where the balance counter weights were built into the leading edge of the control surface ahead of the hinge point of that control surface. The mass balance weight on the Il-4 is simular to the ones seen on Ju-87's, Bf-109's. Lancaster Bombers. and GRUMMAN G-21/G-44 elevators.
Since I've pinned this down to a specific s/n and a specific mfr. line number (21122) and the fact that you all seem to be overlooking the NOSE WHEEL on the A-20 VERSUS the TAIL WHEEL on the Il-4, the general shape of the fuselages (A-20 slabsided vs completely round) the size and shape of the vertical fins on each.
If you are going by the upper aft turret then using that criteria, a LANCASTER, STIRLING, or HUDSON, could be mistaken as an Il-4. Have you looked @ GOOGLE IMAGES yet to see the differences between an Il-4 and an A20?
OH, Yeah, one other fairly minor point of interest, the picture is of 'Little Joe' which is in the NMUSAF @ Wright Patterson AFB.
Pass that ceegar over here-
Look how the Horizontal Stabs are attached or let's say the location. The A20 is higher up isn't it?
Look at the A20 slots_hinge) in the rudder. None in crash photo.
In the crash photo the fuselage going forward of the turret towards the cockpit is different than the A-20 photo