What was found
DURING INSPECTION, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 0.25 INCH CRACK AT STA 285. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED IN ACCORDANCE WITH S/B 727-53-145.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 0.25 INCH CRACK AT STA 285. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED IN ACCORDANCE WITH S/B 727-53-145.