weight of wing structure, equivalenl fuselage and equivalent fail aall, in lbs., i.e., \ Vw + \V, + \V, , , :2-2999 Ca#39; + 5-9257 C2 for allbelowC = 6-2 2-1684 ... Wx includes flying and engine controls (including starting mag., switches, - and wiring, and doping system), instruments, pilota#39;s seating, ... Stress Load, W8: 7-1 Aw = 7-1 x 13 -36 Ca#39; = 94-85 Ca#39;. in lbs. ... Ton-Miles Per Gallon aquot; One other curve is run on this diagram, the curve to obtain which all the foregoing has been necessitated, namely aanbsp;...
|Title||:||Flight No.1 Vol.XIII|