What was found
AT C-CK, RADOME- 2 (EA) .25 INCH CRACKS ON RADOME LOWER LIP (INNER PART). PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CK, RADOME- 2 (EA) .25 INCH CRACKS ON RADOME LOWER LIP (INNER PART). PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B.