What was found
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN LEFT FUSELAGE SKIN BETWEEN LONGERON 3L AND 4L STATION 1095. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN LEFT FUSELAGE SKIN BETWEEN LONGERON 3L AND 4L STATION 1095. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27. (M)