What was found
DURING CHECK-C MAINT FOUND FUSELAGE SKIN BULGED AT STA 350 BETWEEN LONGERON 22L AND 23L. ACCOMP HFEC PER NDT MANUAL PART 6, 51-00-03, AND NO CRACK FOUND. REPAIRED PER SRM 53-04, PAGE 35, FIG 12B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT FOUND FUSELAGE SKIN BULGED AT STA 350 BETWEEN LONGERON 22L AND 23L. ACCOMP HFEC PER NDT MANUAL PART 6, 51-00-03, AND NO CRACK FOUND. REPAIRED PER SRM 53-04, PAGE 35, FIG 12B.