What was found
DURING INSPECTION FOUND CRACK IN FUSELAGE SKIN AT BS 540, 2ND FROM TOP AFT, OPENED FASTENER HOLE BETWEEN STRINGER 22R AND STRINGER 23R. MAINTENANCE REPAIRED IAW AND WORK ACCOMPLISHED ON WORK CARD 5331-01257-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION FOUND CRACK IN FUSELAGE SKIN AT BS 540, 2ND FROM TOP AFT, OPENED FASTENER HOLE BETWEEN STRINGER 22R AND STRINGER 23R. MAINTENANCE REPAIRED IAW AND WORK ACCOMPLISHED ON WORK CARD 5331-01257-10.