What was found
PER EC/RA 5360-01873 PART 1, STEP 2. INITIATE A NEW DIP LOGPAGE FOR THE INTERIM REPAIR. AT FUSELAGE STRINGER 25L, STA 807 AND 847. 847 ON AIRCRAFT N37408 IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA 5360-01873. AFTER AUGUST 30, 2026, BUT BEFORE SEPTEMBER 30, 2026, PERFORM AN INSPECTION OF THE FUSELAGE STRINGER 25L REPAIR BETWEEN STA 807 & AFTER AUGUST 30, 2026, BUT BEFORE SEPTEMBER 30, 2026, PERFORM AN TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION OF THE FUSELAGE STRINGER 25L REPAIR BETWEEN STA 807 & 847 ON AIRCRAFT N37408 IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA 5360-01873.