What was found
LT BETWEEN FR35 & 36 HAS 60 HOLES. HOLE NUMBER 16 IS CRACKED IN THE 7 ''CLOCK POSITION. ALL OTHER HOLES I/B OF CUT OUT HAVE NO REJECTABLE INDICATIONS. HOLES O/B & ALL HOLES IN CROSSBEAM ATTACHMENT HAVE OUT OF ROUND/REJECTABLE DAMAGE. REPAIR REQUIRED PRIOR TO NEXT FLIGHT CYCLE ON REF 9296967 AD RELATED (2018-06 -04). WHILE ACCOMPLISHING EA5330-05216 INSPECTION SEVERAL HOLES WERE FOUND TO BE CRACKED. ACCOMPLISHED REPAIR PER PART 1 OF ECRA5331-0 2380. DTA, ACCOMPLISH PERMANENT REPAIR AT FUSELAGE FR35-36R PRESSURE PANEL HOLES PER PART 3 OF ECRA5331-02380 ON OR BEFORE 2 5OCT2019. PLANNING TO CONTACT ENGINEERING AFTER 25AUG2019, BUT BEFORE 25SEP2019 FOR PERMANENT REPAIR.