— BESDLIS @ - 363 “ Therpa)! The temperature rise wes insignificant due to the limiting side loads position and very emall thermal inpute that vere received. Qeat: At tine of shook arrival the gust load vas 48% of limit wing bending at station 497,0, 45% at station 615.0 and 42% at station 144.C, Since the fuselage bending, shear end torsion gages were adied only recertly, they have not been calibreted, and results from recorded inputs cannot be oompared to limiting criteria at thie time. However, it ie believed that the recorded fuselage inpote for thie event vere small, yp vat Qverpressure: Peak overpressure measured at N+ 44.06 seconde, DISCUSSION . The calibration of the side loads gages in the fuselage vil) net be accomplished until return to the 27]. Therefore the percent bending in the fuselage will sot be know until the calibration is complete! an? the data reduced , -%-