What was found
CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT LWR TERMINUS OF DOOR SURROUND FRAME BS 300 STRINGER 17R WL 209. INSTALLED FRAME REQUIRE PER SRM 51-70-11 FIG 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT LWR TERMINUS OF DOOR SURROUND FRAME BS 300 STRINGER 17R WL 209. INSTALLED FRAME REQUIRE PER SRM 51-70-11 FIG 1. (M)