What was found
LH CONTINUITY FITTING CRACKED. (APPROX .150") JUST OUTBOARD OF B END AS METAL THICKNESS BEGINS TO DECREASE. CRACK RUNS VERTICALLY THROUGH THE ENTIRE THICKNESS. GEN BY V909079 ON HAECO LCQ NR 92 90338/30338 ECRA5310-08187 ON OR BEFORE AIRCRAFT REACHES 35574 FLT CYCLES. CYCLES, THEREAFTER. PERFORM REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 4700 FLT ACCOMPLISH INITIAL INSPECTION OF FRONT WINDSHIELD FRAME LOWER NODE REPAIRED HOLES PER PART 2 OF THE LATEST REVISION OF RII. REMOVED AND REPLACED CONTINUITY FITTING IAW ECRA5310-08187 DIP 53-DIP REJECTED BACK FOR SIGNOFF REMOVED AND REPLACED CONTINUITY FITTING IAW ECRA5310-08187. NO FURTHER ACTION REQUIRED.