What was found
ON INSPECTION, NR 1 ENGINE TRUSS INBOARD SIDE UPPER HAS CRACK. WELDED CRACK IAW MANUFACTURERS REPAIR INSTRUCTIONS CONTAINED IN KIT NR 114-9033-1, PARAGRAPH 16. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON INSPECTION, NR 1 ENGINE TRUSS INBOARD SIDE UPPER HAS CRACK. WELDED CRACK IAW MANUFACTURERS REPAIR INSTRUCTIONS CONTAINED IN KIT NR 114-9033-1, PARAGRAPH 16. (M)