What was found
ATTACH ANGLE CRACKED AT FS 409.00+128, BL 0.00. REMOVED ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 & SRM 51-25-16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ATTACH ANGLE CRACKED AT FS 409.00+128, BL 0.00. REMOVED ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 & SRM 51-25-16.