The movement of this straight edge over an aluminium plate fastened to the cable of the bars free end was noted. ... (b) Fore and aft wires from upper rear spars to lower front spars slack at all stations. ... FINAL EX AMI .\a#39;.\ TION An examination was made by a representative, John M. Rogers, of the Heat Treating Department ... (d) Hinge pins at (6) lower wing bent. ... From this stress strain diagram and the elongation of the cables during the test on the H-12 machine, the tensions in themanbsp;...
|Title||:||Aviation and Aeronautical Engineering|