I'm curious if anybody has performance figures for the A-26D/E which seemed to differ in the fact that it had a more powerful engine, a redesigned cowling, and wide-chord blades. Does anybody have figures for maximum speed, what altitude this applies at, and so on?
Based on the data I have from a PDF "USAF~USN engine designations 9th ED (50-01-01)", the R-2800-83 was rated for 17500', but these figures are w/o ram compression.
C CORSNING GregP S Shortround6 W wuzak
Based on the data I have from a PDF "USAF~USN engine designations 9th ED (50-01-01)", the R-2800-83 was rated for 17500', but these figures are w/o ram compression.
C CORSNING GregP S Shortround6 W wuzak