What was found
IAH - INSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF RT VERTICAL FIN ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 19. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IAH - INSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF RT VERTICAL FIN ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 19. (X)