What was found
EXTERNAL FUSELAGE SKIN BS 1600-1620 BETWEEN S25-26R HAS TWO DENTS. . BS 1613 BETWEEN S26-25R A=0.6 Y=.045 A/Y= 13.33 OUT OF LIMITS. REPAIRED IAW SRM-53-00-01, FIG 201, REPAIR NR 7. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERNAL FUSELAGE SKIN BS 1600-1620 BETWEEN S25-26R HAS TWO DENTS. . BS 1613 BETWEEN S26-25R A=0.6 Y=.045 A/Y= 13.33 OUT OF LIMITS. REPAIRED IAW SRM-53-00-01, FIG 201, REPAIR NR 7. MAJOR REPAIR.