What was found
ACCESS PANEL LT WING 516ET FOUND 2 CRACK ON ANGLE INTERNAL SKIN. REMOVED EXISTING REPAIR AND REPAIR STIFFENERS IAW SRM 51-35-01 PAG 1-13 AND 51-33- 01 PAGE 34-47 AND SRM 57-10-00 FIG 23 VOL I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ACCESS PANEL LT WING 516ET FOUND 2 CRACK ON ANGLE INTERNAL SKIN. REMOVED EXISTING REPAIR AND REPAIR STIFFENERS IAW SRM 51-35-01 PAG 1-13 AND 51-33- 01 PAGE 34-47 AND SRM 57-10-00 FIG 23 VOL I.