What was found
FOUND DURING D-1 LETTER CHECK - .25 INCH CRACK IN RT UPPER ENG PYLON TO FUSELAGE ANGLE 12 INCHES FROM AFTM EDGE. REPAIRED PER SRM 54-04A PG17 FIG 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND DURING D-1 LETTER CHECK - .25 INCH CRACK IN RT UPPER ENG PYLON TO FUSELAGE ANGLE 12 INCHES FROM AFTM EDGE. REPAIRED PER SRM 54-04A PG17 FIG 4.