What was found
RIGHT WING TO FUSELAGE UPPER SUPPORT ANGLE IS CRACKED 2 1/2 ICHES LONG AT FRAME 49. REPAIRED IAW SRM 53-23-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING TO FUSELAGE UPPER SUPPORT ANGLE IS CRACKED 2 1/2 ICHES LONG AT FRAME 49. REPAIRED IAW SRM 53-23-12.