What was found
PIT - DURING Q4-C6 CHECK, FOUND .25 INCH CRACK IN LONGERON AT BELT FRAME 24 RIGHT BETWEEN STA 446 - STA 465. REMOVED CRECKED SECTION, INSTALLED NEW LONGERON AND SPLICES PER TYPICAL REPAIR 53-10-07, FIGURE NR 2. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q4-C6 CHECK, FOUND .25 INCH CRACK IN LONGERON AT BELT FRAME 24 RIGHT BETWEEN STA 446 - STA 465. REMOVED CRECKED SECTION, INSTALLED NEW LONGERON AND SPLICES PER TYPICAL REPAIR 53-10-07, FIGURE NR 2. (X)