As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H FUSELAGE SKIN AT STA. 1156 HAS A .400 IN. CRACK AT THE AFT FASTENER HOLE COMMON TO THE TEE CAP (2 FASTENERS ABOVE LONGERON 39R) PROPAGATING AFT TO THE EDGE OF SKIN PANEL. (MARKED) WORKED I.A.W E.A # 8-5310-T0343606 (FUSELAGE-MAINFRAME-FUSELAGE SKIN AND FRAME AT STATION 1156, L-37 AND JUST ABOVE L-39, R/H/S-REPAIR)