What was found
ANGLE, 1.5 INCH LONG CRACK, RT WING ROOT, BS 540 AT S22R, AFT END. INSTALLED REPAIR ANGLE DOUBLER IAW T/R 53-50-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ANGLE, 1.5 INCH LONG CRACK, RT WING ROOT, BS 540 AT S22R, AFT END. INSTALLED REPAIR ANGLE DOUBLER IAW T/R 53-50-03.