What was found
CRACK INDICATION FOUND ON FR.68 LH WEB HORIZONTAL FLANGE INNER CAP STR .22L. CRACK LENGTH IS 1.181 INCH APPROX. (REQUESTING REPAIR DISPOSITIO N. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED, AND REPAIR MUST B E ACCOMPLISHED PRIOR TO FURTHER FLIGHT. REFER TO EM 5311-01244, WORK S ECTION 01A, SB A320- 53-1491 REV 01, AND FAA AD 2022-15-05, EASA AD 202 2-0030. (LP: 031684)