What was found
A CRACK WAS FOUND AT NLG ROOF PANEL AT STIFFENER C-5 IN AREA OF FRAME 14. REPAIR PERFORMED BY BLENDING OUT THE CRACKED STIFFENER AND INSTALLING REINFORCED ANGLES AND SHIMS IAW EA 6-5312-103289 AND RAS/AS/139/2006 ISS A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A CRACK WAS FOUND AT NLG ROOF PANEL AT STIFFENER C-5 IN AREA OF FRAME 14. REPAIR PERFORMED BY BLENDING OUT THE CRACKED STIFFENER AND INSTALLING REINFORCED ANGLES AND SHIMS IAW EA 6-5312-103289 AND RAS/AS/139/2006 ISS A.