What was found
CRACK WAS FOUND AT CUSP WEB ON FUSELAGE STA 218, X= 56. SUMMARY OF NRC 00609: LH CUSP WEB ON FUSELAGE STA 218, X=56 WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 PAR 4 FIG 201. (LP #0071687)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK WAS FOUND AT CUSP WEB ON FUSELAGE STA 218, X= 56. SUMMARY OF NRC 00609: LH CUSP WEB ON FUSELAGE STA 218, X=56 WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 PAR 4 FIG 201. (LP #0071687)