What was found
FAULT- #2 ENGINE PYLON OUTBD ACCESS HOLE INNER SKIN HAS A CRACK GOING THRU HILOK AT THE 3 0CLOCK POSITION. REMOVED 2EA FASTENERS IAW SRM 51-40-02-0G AND CRACK EVALUATED IAW SRM 54-51-01-1A-1 ALLOWABLE DAMAGE
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FAULT- #2 ENGINE PYLON OUTBD ACCESS HOLE INNER SKIN HAS A CRACK GOING THRU HILOK AT THE 3 0CLOCK POSITION. REMOVED 2EA FASTENERS IAW SRM 51-40-02-0G AND CRACK EVALUATED IAW SRM 54-51-01-1A-1 ALLOWABLE DAMAGE