What was found
CHAFING DAMAGE TO LEFT AFT AREA OF NOSE WHEELWELL. TUNNEL AT FRAME 5, FS 160.77 CAUSED BY STRUT BOLT INSTALLED IN WRONG DIRECTION.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CHAFING DAMAGE TO LEFT AFT AREA OF NOSE WHEELWELL. TUNNEL AT FRAME 5, FS 160.77 CAUSED BY STRUT BOLT INSTALLED IN WRONG DIRECTION.