What was found
ANGLE FOUND CRACKED ON TOP OF FUSELAGE , UNDER CENTER PANEL 261 FT. R & R WITH NEW PART IAW SRM 51-42-05 AND SRM 51-40-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ANGLE FOUND CRACKED ON TOP OF FUSELAGE , UNDER CENTER PANEL 261 FT. R & R WITH NEW PART IAW SRM 51-42-05 AND SRM 51-40-10.