What was found
DURING OVERNIGHT CHECK FOUND CRACK IN AFT LT FUSELAGE SKIN AT BS 1059 ABOVE L18. REPAIRED PER EA 99-214064 SECT I. SECTION II REQUIRES A BOEING DAMAGE TOLERANCE ANALYSIS AND INSPECTION NO LATER THAN 10/11/10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OVERNIGHT CHECK FOUND CRACK IN AFT LT FUSELAGE SKIN AT BS 1059 ABOVE L18. REPAIRED PER EA 99-214064 SECT I. SECTION II REQUIRES A BOEING DAMAGE TOLERANCE ANALYSIS AND INSPECTION NO LATER THAN 10/11/10.