What was found
2(EA) CRACK INDICATIONS FOUND: L/H UPPER WING SKIN & DRAG FITTIN G FASTENER HOLE #2, IN UPPER LAYER(SKIN) AT 3 & 9 ''OCLOCK POSITI ONS. FLIGHT CYCLES THEREAFTER." REPAIRED #2 HOLE AT L/H WING SKIN & I/B DRAG FITTING PER REO-G24 "ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2B OF ECRA- 432 AND REPLACED I/B DRAG FITTING P/N 653N0002-13, PO: 1057274.1 01053 LATEST REVISION ON OR BEFORE THE AIRCRAFT THRESHOLD 21,400 PER BAC DWG 112N7001, REV D, B757-200 SRM 57-20-01, REPAIR 8. TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS PER PART 2A O F ECRA-01053 LATEST REVISION AT INTERVALS NOT TO EXCEED 1,050