What was found
LT UPPER WING TO FUSELAGE SUPPORT ANGLE. HAS 1" CRACK BETWEEN FRAMES 48-49. WILL BE REPAIRED DURING COMPLIANCE OF FRAME 50 CRACK NRTC E680918.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT UPPER WING TO FUSELAGE SUPPORT ANGLE. HAS 1" CRACK BETWEEN FRAMES 48-49. WILL BE REPAIRED DURING COMPLIANCE OF FRAME 50 CRACK NRTC E680918.