What was found
TAIL INTERIOR, LT CANTED FRAME WEB HAS .5" LONG CRACK AT FASTENER, BS 1485, 10 O`CLOCK POSITION, 1" BELOW HORIZONTAL STIFFENER.INSTALLED LT VENT BOX ASSY. ALL WORK PERFORMED AND COMPLETED IAW SRM 53-03, FIG. 48.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR, LT CANTED FRAME WEB HAS .5" LONG CRACK AT FASTENER, BS 1485, 10 O`CLOCK POSITION, 1" BELOW HORIZONTAL STIFFENER.INSTALLED LT VENT BOX ASSY. ALL WORK PERFORMED AND COMPLETED IAW SRM 53-03, FIG. 48.