What was found
CRACK IN FUSELAGE SKIN AT STA 727E, STRINGER 18, 2.5 IN. REPAIRED CRACK PER SRM 53-00-01, FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE SKIN AT STA 727E, STRINGER 18, 2.5 IN. REPAIRED CRACK PER SRM 53-00-01, FIG 201.