What was found
IN REF AMDS 5720-01100-04A STEP 18 , SCRATCH ON FASTENER HOLE NO.7 ON SKIN AND FITTING AT 5 O'CLOCK POSITION AT LT WING. REASON FOR RE-WRITE: AFTER FINAL INSTALLATION OF INBD DRAG FITTING WITH FRONT SPAR AND UPPER/ LOWER WING SKINS, UPPER LINK PIN MISSALIGNED WAS NOTED. SCRATCH ON FASTENER HOLE NO.7 ON SKIN AND FITTING AT 5 O'CLOCK POSITION AT LT WING WAS REPAIRED IAW PRI 592324-14 REV 0 TO PRI REV 6 AND ER/A 592324-14 REV.D, SECTION VIII: PERMANENT REPAIR. (1409674)