What was found
NICK IN LOWER FUSELAGE SKIN AT STA 525 BETWEEN S-27L AND S-28L, DEEPER THAN .006 INCH, CHEMILLED AT THAT POINT IS .040 INCH. DOUBLER AND FILLER INSTALLED AT STA 525 BETWWEN S-27L AND S-28L IAW SRM 53-00-01, REPAIR 7, FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NICK IN LOWER FUSELAGE SKIN AT STA 525 BETWEEN S-27L AND S-28L, DEEPER THAN .006 INCH, CHEMILLED AT THAT POINT IS .040 INCH. DOUBLER AND FILLER INSTALLED AT STA 525 BETWWEN S-27L AND S-28L IAW SRM 53-00-01, REPAIR 7, FIG 201.