What was found
DURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND BETWEEN STA 840-859, STR 39-42, RT, 3 EA FLUSH PATCH WITH INTERNAL DOUBLER. NO ACTION REQUIRED. REPAIR IS CONFORM TO SRM 53-20-00 FIG 13 SH 8/9. PERFORMED EA 8-5330-94668 PART 1 INSPECTION. NO DEFECT FOUND.