What was found
AT HMV-1, INSP FOUND CHORD ANGLE CRACKED AT 48 SECTION LT SIDE STA 1342. THE HORIZONTAL CHORD ANGLE IS CRACKED JUST I/B OF FIN TERMINAL FITTING. FITTING IS PREVIOUSLY STOP DRILLED. REPAIRED CRACK PER M/M 53-11-0 PG 808.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT HMV-1, INSP FOUND CHORD ANGLE CRACKED AT 48 SECTION LT SIDE STA 1342. THE HORIZONTAL CHORD ANGLE IS CRACKED JUST I/B OF FIN TERMINAL FITTING. FITTING IS PREVIOUSLY STOP DRILLED. REPAIRED CRACK PER M/M 53-11-0 PG 808.