What was found
UNDER PANEL 212HP WEB AND ANGLE AT -Y953/FR10 CRACKED. DOT: 101-11 TG-101. INSTALLED NEW ANGLE UNDER PANEL 212HP AT Y-953/FR 10 I.A.W. A300-600 S.R.M. 51-40-21. REVIEWED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UNDER PANEL 212HP WEB AND ANGLE AT -Y953/FR10 CRACKED. DOT: 101-11 TG-101. INSTALLED NEW ANGLE UNDER PANEL 212HP AT Y-953/FR 10 I.A.W. A300-600 S.R.M. 51-40-21. REVIEWED.