What was found
CRACK DAMAGE ON LT ENGINE HORSECOLLAR AFT WEB PN 85410012-001. REMOVED DAMAGE AND APPLIED DOUBLERS IAW ECO 008.54-15.02
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK DAMAGE ON LT ENGINE HORSECOLLAR AFT WEB PN 85410012-001. REMOVED DAMAGE AND APPLIED DOUBLERS IAW ECO 008.54-15.02