What was found
TWO CRACKS AT FORWARD BS 400 BULKHEAD STRINGER S44L AND S44R, AT CORNER AFT O WHEEL WELL AND CRACK AT BS 400 AROUND FASTENER. REPAIRED PER BOEING SB 53-23-05 AND SRM 53-30-03 FIG 35.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TWO CRACKS AT FORWARD BS 400 BULKHEAD STRINGER S44L AND S44R, AT CORNER AFT O WHEEL WELL AND CRACK AT BS 400 AROUND FASTENER. REPAIRED PER BOEING SB 53-23-05 AND SRM 53-30-03 FIG 35.