What was found
FUSELAGE SKIN HAS CORROSION BS 916, STR 24L. GROUNDED - YES. REMOVED CORROSION ORIGINAL SKIN THICKNESS 0.063, IAW B737-800 SRM 53-80-01-O1, REMAINING SKIN THICKNESS 0.061. REMOVED 0.002 BLENDED AREA WITHIN ALLOWABLE LIMITS, IAW B737-800 SRM 53-00-01-1A-1 PARA 4B(2)(B). ALODINED IAW B737-800 SRM 51-20-01. PRIMED IAW BOEING SOPM 20-44-04 PAINTED TOP COAT, IAW B737-800 AMM 51-21-99.