What was found
WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED LOWER SKIN STIFFENER ON RT ELEVATOR AT ELEV STA 17.2 INSIDE ACCESS PANEL 9406 APPROX 5.25 INCHES AFT OF FRONT SPAR CHORD. REPAIRED IAW SRM 51-20-2, 51-30-2, 51-20-1, 55-20-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED LOWER SKIN STIFFENER ON RT ELEVATOR AT ELEV STA 17.2 INSIDE ACCESS PANEL 9406 APPROX 5.25 INCHES AFT OF FRONT SPAR CHORD. REPAIRED IAW SRM 51-20-2, 51-30-2, 51-20-1, 55-20-2.