What was found
CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 540, STRINGER 22R SUPPORT ANGLE RAM AIR INLET SUPPORT. FABRICATED AND INSTALLED REPLACEMENT REPAIR ANGLE PER 53-50-03. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 540, STRINGER 22R SUPPORT ANGLE RAM AIR INLET SUPPORT. FABRICATED AND INSTALLED REPLACEMENT REPAIR ANGLE PER 53-50-03. (M)