What was found
MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE FRAME STA 89 WITH CRACK IN OUTBOARD RADIUS BETWEEN LONGERONS 18 AND 19. STOP DRILLED CRACK PER SRM 51-10 AND REPAIRED PER SRM 53-01, PAGE 10, FIGURE 2. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE FRAME STA 89 WITH CRACK IN OUTBOARD RADIUS BETWEEN LONGERONS 18 AND 19. STOP DRILLED CRACK PER SRM 51-10 AND REPAIRED PER SRM 53-01, PAGE 10, FIGURE 2. (X)