VingTipe: The paint was blistered ani peeled on the tep and dbetten of both wing tips. Again, in this conse, it is diffieult to seperate thermal frow rain damage. The plastic itself did net appear Gemaged but only the aluminum paint, Plastie Tips: About the same as the wing tips but to a lesser degree. Stebileter: The aluminum peint on the underside was bilstered and peeled in some cases. Oompartpent: The vhite silicone rubber seal on the bottom edge of the door was cracked diagonally acroes and two lock tabs were breken off, ‘This demage can be attributed to veer ani tear fron overheat enused by use of afterburzers and normal usage of opening ant elosing the door, Wing Surface: The blue insignia paint on the upper left wing was wildly blistered near the aileron hinge atteciment. Zastrupeptation: There ves ne apparent damage to the instrumentation. Of the 50 cscillegreph receded parameters, 47 preduced weable data. One calorimeter malfunctioned. Tvo thermocouples failed te produce usable Gata; ome beeame wapeened and the other geve upreliable readings. 26 paremeters recoried on the photopane), 24 produced weable data. Of the The ambient air temperature probe malfunctioned ant the 4/B fuel flew produced ‘eareliable data, Date: Ho gust data was received since the aircraft out ran the shock , ThermalDat : 4 41 ef about 160° wae experienced on the unpainted heavyeund of the ving, BEST The stabilater honeroomb experienced « AT of py AVAIL ABLE co - 43 COpENooe gAND &