What was found
CORROSION ON CUSP ANGLE STA Y=200 X=-54 AT W1. REPLACED CUSP ANGLE STA Y=167-200 X=-54 IAW MD88 SRM 53-05 FIG 55.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON CUSP ANGLE STA Y=200 X=-54 AT W1. REPLACED CUSP ANGLE STA Y=167-200 X=-54 IAW MD88 SRM 53-05 FIG 55.