What was found
WHILE ACCOMPLISHING REPETITIVE INSPECTION OF FUSELAGE SKIN REPAIR AT BS 1475 BETWEEN LONGERONS 1 AND 3R, FOUND REPAIR TO HAVE 2" CRACK IN RADIUS, STA 1475 BETWEEN LONGERON 1 AND L2R AT INBD DAMAGE CUTOUT. R & R ANGLE IAW SRM 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE ACCOMPLISHING REPETITIVE INSPECTION OF FUSELAGE SKIN REPAIR AT BS 1475 BETWEEN LONGERONS 1 AND 3R, FOUND REPAIR TO HAVE 2" CRACK IN RADIUS, STA 1475 BETWEEN LONGERON 1 AND L2R AT INBD DAMAGE CUTOUT. R & R ANGLE IAW SRM 51-30-05.