What was found
DURING LINE CHECK, FOUND A 3 INCH CRACK IN THE SLANTED PRESSURE PANEL TO FUSELAGE ATTACH ANGLE APPROXIMATELY LBL 24 ABOVE THE REAR SPAR. REPAIRED ANGLE (P/N 9923419-9) PER EA 97-111746.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING LINE CHECK, FOUND A 3 INCH CRACK IN THE SLANTED PRESSURE PANEL TO FUSELAGE ATTACH ANGLE APPROXIMATELY LBL 24 ABOVE THE REAR SPAR. REPAIRED ANGLE (P/N 9923419-9) PER EA 97-111746.