What was found
L/H WING UPPER I/B ACCESS PANEL 551 DT CRACK AT T/E<[01] APPLIED REPAIR AT PANEL#551DT PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4.N MATERIAL USED RESIN EY 3804 PO#20400614 FIBERGLASS PO#1690463.;[02] VERIFIED STEP 1
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
L/H WING UPPER I/B ACCESS PANEL 551 DT CRACK AT T/E<[01] APPLIED REPAIR AT PANEL#551DT PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4.N MATERIAL USED RESIN EY 3804 PO#20400614 FIBERGLASS PO#1690463.;[02] VERIFIED STEP 1