What was found
PIT - DURING Q1 CHECK, FOUND .5 INCH CRACK AFT CARGO DOOR PAN AT PAN AFT EDGE BELOW LATCH CAM ARM. INSTALLED DOUBLER PER SRM 52-05 FIG 35A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q1 CHECK, FOUND .5 INCH CRACK AFT CARGO DOOR PAN AT PAN AFT EDGE BELOW LATCH CAM ARM. INSTALLED DOUBLER PER SRM 52-05 FIG 35A. (M)