What was found
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SKIN CRACK APPROXIMATELY 2 INCHES IN LENGTH IN MED UPPER FORWARD JAMB CORNER STATION 160 FUSELAGE EXTERIOR SKIN. INSTALLED DOUBLER AND FILLER REPAIR PER SRM 53-05 FIG 25A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SKIN CRACK APPROXIMATELY 2 INCHES IN LENGTH IN MED UPPER FORWARD JAMB CORNER STATION 160 FUSELAGE EXTERIOR SKIN. INSTALLED DOUBLER AND FILLER REPAIR PER SRM 53-05 FIG 25A. (M)