What was found
FUSELAGE SKIN, STA 325 BT STR21L-22L: TWO EXISTING BLENDOUTS FOUND ON EXTERNAL FUSELAGE SKIN. NOMINAL THICKNESS: 0.130". (-0.002" THICKNESS BLENDED). ONLY ONE BLENDOUT IS DOCUMENTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN, STA 325 BT STR21L-22L: TWO EXISTING BLENDOUTS FOUND ON EXTERNAL FUSELAGE SKIN. NOMINAL THICKNESS: 0.130". (-0.002" THICKNESS BLENDED). ONLY ONE BLENDOUT IS DOCUMENTED.