What was found
PANEL 192DL HAS SEVERAL FASTENER HOLES WORN AND ELONGATED IN THE COMPOSITE MATERIAL BETWEEN WHEEL WELL CUT OUTS, AFT EDGE. REPAIRED DAMAGED FASTENER HOLES IAW SRM II 51-72-06, 51-40-02 & 51-40-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 192DL HAS SEVERAL FASTENER HOLES WORN AND ELONGATED IN THE COMPOSITE MATERIAL BETWEEN WHEEL WELL CUT OUTS, AFT EDGE. REPAIRED DAMAGED FASTENER HOLES IAW SRM II 51-72-06, 51-40-02 & 51-40-04.