What was found
PIT - Q6 - RIVET HOLES, .1250 INCH TO .2500 INCH - 7 RIVET HOLES, CRACKED; LWR SKIN AFT FASTENER ROW CENTERED ON SLAT ACT. AREA. INSTALLED DOUBLER IAW SRM 57-43-01.(K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - Q6 - RIVET HOLES, .1250 INCH TO .2500 INCH - 7 RIVET HOLES, CRACKED; LWR SKIN AFT FASTENER ROW CENTERED ON SLAT ACT. AREA. INSTALLED DOUBLER IAW SRM 57-43-01.(K)