As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION (MID-FEC) FOUND CRACK INDICATION AT FRAME BS 727D R, BETWEEN STRINGERS 8 & 9 AT AIR CONDITIONING OUTLET EXTRUSION SUPPORT ATTACHMENT TO FUSELAGE FRAME, MARKED. PER EA5310-04716 REV.E OPT 1. COMPLIED WITH STEPS 1-13 OF EA5310-04716 REV. E TO REPAIR CRACKED FRAME AT BS.727D RT SIDE AT STRINGER 8 & 9. SEE ABOVE LISTED WIPS FOR ALL WORK ACCOMPLISHED.