What was found
CRACK ON CUSP MEMBRANE (WEB) X=56 AND STA 611 AT CPAX. CRACK WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5 FIG 204. (LP #2795916)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON CUSP MEMBRANE (WEB) X=56 AND STA 611 AT CPAX. CRACK WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5 FIG 204. (LP #2795916)