What was found
UPPER FUSELAGE SKIN HAS "BLEND OUT" AT BS 444.5 & STR 4LT. REPAIRED FUSELAGE SKIN AT BS 444.5 & STR 4LT PER SRM 53-00-01 FIGURE 201 SECTION I & II.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE SKIN HAS "BLEND OUT" AT BS 444.5 & STR 4LT. REPAIRED FUSELAGE SKIN AT BS 444.5 & STR 4LT PER SRM 53-00-01 FIGURE 201 SECTION I & II.