What was found
CORROSION ON SEAT TRACK HARD POINT AREA Y254, FRAME 16. ORIGINAL THICKNESS .080", CURRENT THICKNESS .060" & MATERIAL LOSS 20%. REPLACED SEAT TRACK IAW SRM 51-42-11 PAR 7. MATERIAL LOSS BEYOND LIMITS IAW SRM 53-11-14 PB 101.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON SEAT TRACK HARD POINT AREA Y254, FRAME 16. ORIGINAL THICKNESS .080", CURRENT THICKNESS .060" & MATERIAL LOSS 20%. REPLACED SEAT TRACK IAW SRM 51-42-11 PAR 7. MATERIAL LOSS BEYOND LIMITS IAW SRM 53-11-14 PB 101.