What was found
During "L" check found crack in fuselage bulkhead upper attach angle at BS 2122.8. Repaired per EA 12-194259.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
During "L" check found crack in fuselage bulkhead upper attach angle at BS 2122.8. Repaired per EA 12-194259.