What was found
FOUND DISTORTION ON PANEL AT FUS SKIN RT BETWEEN STA 540 AND 560 AND BETWEEN STRINGERS 35 TO 36. STRAIGHTENED AND SMOOTHED PANEL IAW SRM 51-40-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND DISTORTION ON PANEL AT FUS SKIN RT BETWEEN STA 540 AND 560 AND BETWEEN STRINGERS 35 TO 36. STRAIGHTENED AND SMOOTHED PANEL IAW SRM 51-40-01.