What was found
RAM AIR SCOOP CRACKED VERT. LT. SIDE. TRANSFERRED STEP 1 FROM PRI 517410-14, REMOVED DAMAGED AREA WITH A 4" X 8.5" X 2" CUTOUT. STEP 2, HFEC COMPLETED. ALL INFO TRANSFERED FROM PRI NR 552071. ACCOMPLISED BNEC IAW SPM06-10-01.003, NO CRACKS QC 2021. TRANSFERED STEP 4 FROM PRI 517410-14 FORM FILLER FROM 6 061-0, .050". HEAT TREAT IAW PS 900-4-1, NR 1 CONDUCTIVITY TEST PERFORMED ON REPAIR FILLER IAW PS 900-4-NR 1 FOUND TO BE 45 PERCENT IACS. REF.PRI 517410-14, REV ORIGINAL. TRANSFERED FROM PRI 517410-14. WELDED REPAIR IAW SRM 55-05, ACCOMPLISHED FPI IAW PSM-900-6-1, 2, NO CRACKS-QC. REDEFERRED LOG TO QC, ESTABILISHED MONITOR INSPECTION 10-0553-8-7369, SN 971, REP SEC I. REPAIR LIMIT TO 4000 FH OR 547 DAYS, RESTRICTION REVISED ACCORDINGLY ASSOCIATED ER/A 00-420329 ADDED FOR AC 0971. DVI WAS PERFORMED AND CRACK WAS FOUND. REPAIR WAS ACCOMPLISHED IAW ER/A 420329-14MA REVISION "C" TIME LIMITED INSTRUCTIONS SRM 55-05, PAR 4. PERFORM REPETITIVE VISUAL INSPECTION WITHIN EVERY "C" CHECK LIMIT, 4000 FLIGHT HOURS OR 547 DAYS IAW ER/A NR 420329-14MA, REV "C" SECTION 1.