What was found
FUSELAGE SKIN CRACKED AT EMERGENCY LIGHT S22L, CRACK APPROXIMATELY 1 INCH LONG. INSTALLED REPAIR PER SRM 53-00-01, REPAIR 31, FIG 201, PROCEDURE V. ISSUED DIP PER EC/RA 5331-01399 TO READ, BEFORE THE ACCUMULATION OF 60,000 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH PERMANENT REPAIR OR CONTACT ENGINEERING TO PERFORM A REPAIR ASSESSMENT.