What was found
LT WING VERTICAL CONNECTION ANGLE ON FORWARD SPAR AT NACELLE HAS TWO CRACKS IN RADIUS AT UPPER AND LOWER ENDS. REPAIRED IAW DHC-8 SRM 51-40-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING VERTICAL CONNECTION ANGLE ON FORWARD SPAR AT NACELLE HAS TWO CRACKS IN RADIUS AT UPPER AND LOWER ENDS. REPAIRED IAW DHC-8 SRM 51-40-11.