What was found
AT C CHECK, AFT LOWER FUSELAGE HAS CORROSION AT FS 1680 BETWEEN L- 306 AND L-30R. CUT OUT DAMAGED SKIN, FABRICATED REPAIR PARTS, DRILLED, TREATED AND INSTALLED PARTS PER SRM 53-2-1 AND 51-1-21. INSTALLED FLOORS PER SRM 51-3-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, AFT LOWER FUSELAGE HAS CORROSION AT FS 1680 BETWEEN L- 306 AND L-30R. CUT OUT DAMAGED SKIN, FABRICATED REPAIR PARTS, DRILLED, TREATED AND INSTALLED PARTS PER SRM 53-2-1 AND 51-1-21. INSTALLED FLOORS PER SRM 51-3-0.