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 &