What was found
DURING INSPECTION, FOUND 5 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1240. REPAIRED DAMAGED SKIN TO STA 1240 BY TEMPORARY REPAIR IAW ENGINEER DRAWING B87-R01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND 5 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1240. REPAIRED DAMAGED SKIN TO STA 1240 BY TEMPORARY REPAIR IAW ENGINEER DRAWING B87-R01.