What was found
DURING SERV CHK, FOUND 1 INCH CRACK IN FWD END LT PYLON FUSE ATTACH ANGLE. MAINT REPAIRED IAW SRM 54-04 FIG 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SERV CHK, FOUND 1 INCH CRACK IN FWD END LT PYLON FUSE ATTACH ANGLE. MAINT REPAIRED IAW SRM 54-04 FIG 10.