What was found
D: Fuselage skin bulged between sta 1450-1465 stringer 28 L/HC: Bulging caused by corroded stringer, out of limits, removed damaged area fabricated repair parts and installed per 737 SRM 51-40-02, 53-00-03 fig 201 DWG 14683820, and SRM 51-20-01, 53-60-03 fig 1