What was found
FUSELAGE FRAME, FR 54 LATERAL PANEL THREE HOLES CRACKED AT STRINGER 36L, 44L - 44R. COMPLIED WITH EA 6-5330-T0388383 P1 REPAIRED THE FUSELAGE FRAME FR54 LATERAL PANEL 3EA CRACKED HOLES AT S36L S44L S44R. EA TITLE: FUSELAGE - PLATES & SKINS - CRACK HOLES ON SKIN LAP JOINT AT FR54 S36L,S44L AND S44R - ALI 531582-01-1. THIS REPAIR IS CONSIDERED AS CAT B REPAIR DUE TO AWAITING FURTHER DAMAGE TOLERANCE (DT) APPROVAL. THIS REQUIREMENT WILL BE TRACKED BY ENMDS TO OBTAIN STAGE 2 AND/OR STAGE 3 APPROVAL WITHIN 6-MONTHS. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 53300244 FOR WORK DETAILS.