What was found
INSPECTION FOUND A 1 INCH CRACK AT FORWARD FASTENER HOLE OF STRINGER 23L AND FAIL SAFE CHORD WAS BULGED AT BS 727. A STRINGER CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK AT FORWARD FASTENER HOLE OF STRINGER 23L AND FAIL SAFE CHORD WAS BULGED AT BS 727. A STRINGER CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.