What was found
DURING CHECK-C MAINT FOUND HOLE IN MEMBRANE UNDER LAV TIE DOWN, STA 200 AND LBL 44 INCHES. REMOVED TORN EDGE OF PUNCTURE TO 1/2 IN DIAMETER HOLE. INSTALLED REPAIR DOUBLER AROUND HOLE PER SRM 53-01, FIG 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT FOUND HOLE IN MEMBRANE UNDER LAV TIE DOWN, STA 200 AND LBL 44 INCHES. REMOVED TORN EDGE OF PUNCTURE TO 1/2 IN DIAMETER HOLE. INSTALLED REPAIR DOUBLER AROUND HOLE PER SRM 53-01, FIG 4.