What was found
AT C-CHECK, FUSELAGE EXTERIOR PNEUMATIC GROUND FRAME SHOWS CRACK .25 AT STA 160.00. STOP DRILLED CRACK IAW SRM 53-2-0, PG 2B, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8, PG 17 & 18. N/R 4260.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, FUSELAGE EXTERIOR PNEUMATIC GROUND FRAME SHOWS CRACK .25 AT STA 160.00. STOP DRILLED CRACK IAW SRM 53-2-0, PG 2B, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8, PG 17 & 18. N/R 4260.