What was found
DURING L-CHECK, FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 LBL 14. TEMPORARY REPAIRED ACCOMPLISHED IAW EA99-214503, SEC I. SECTION II FURTHER TEMPORARY REPAIR TO BE DONE WITHIN 4000 FLIGHT HOURS AFTER SECTION I ACCOMPLISHMENT. SECTION III REQUIRES INSPECTION WITHIN 20,000 CYCLES AFTER SECTION II AND EVERY 6,000 CYCLES THEREAFTER. SECTION IV PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 40,000 CYCLES AFTER SECTION II. (K)