What was found
DURING CHECK-C MAINT, THE MID CARGO DOOR SKIN AFT EDGE WAS CRACKED. CRACK WAS BLENDED OUT TO 9/36 INCH DEEP BY 1.25 INCH WIDE. EDGE DISTANCE TO FASTENER WAS 0.5. REPAIRED PER SRM 52-05 FIG H PAGE 5. ENGR TASK 004 (H005180A).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, THE MID CARGO DOOR SKIN AFT EDGE WAS CRACKED. CRACK WAS BLENDED OUT TO 9/36 INCH DEEP BY 1.25 INCH WIDE. EDGE DISTANCE TO FASTENER WAS 0.5. REPAIRED PER SRM 52-05 FIG H PAGE 5. ENGR TASK 004 (H005180A).