What was found
CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R. SUMMARY OF NRC 00057: CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R WAS REPAIRED PER ETI-17-22-001 REV. 3 AND ER/A 596558-14AD SECTION I. PERMANENT REPAIR REPAIR APPROVAL IS LIMITED TO 60,000 FLIGHT CYCLES. DAMAGE TOLERANCE ANALYSIS (DTA) IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA AC 120-93 ON REF 2094374 ACCOMPLISH THE SECTION II: REPETITIVE INSPECTIONS EVERY 24 MONTHS AFTER 21JAN2022. ON REF LOG 2094384 SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING ASSOCIATED ER/A 14-596558 ADDED FOR AC 9556. (LP #2094621)