What was found
FUSELAGE, CRACKED FORMER STA Y=907 AND X=-60 AT RT FILLET PANEL. FORMER WAS REPAIRED PER SRM 53-01 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE, CRACKED FORMER STA Y=907 AND X=-60 AT RT FILLET PANEL. FORMER WAS REPAIRED PER SRM 53-01 FIG 2.