What was found
INSPECTION FOUND TWO 0.1 INCH CRACKS AT RIVET HOLES IN AFT PRESSURE BULKHEAD BETWEEN S6L AND S7L AT BS 1016. REPAIRED IAW SRM 53-80-08, FIGURE 202 AND 207.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO 0.1 INCH CRACKS AT RIVET HOLES IN AFT PRESSURE BULKHEAD BETWEEN S6L AND S7L AT BS 1016. REPAIRED IAW SRM 53-80-08, FIGURE 202 AND 207.