What was found
IAW TASK 310-01436-01 STEP 5 AFTER REMOVAL CUSP MEMBRENE CRACK WAS FOUND AT CUSP WEB. FUSELAGE STA 674 LH SIDE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1606106) (AIRCRAFT GROUNDED)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IAW TASK 310-01436-01 STEP 5 AFTER REMOVAL CUSP MEMBRENE CRACK WAS FOUND AT CUSP WEB. FUSELAGE STA 674 LH SIDE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1606106) (AIRCRAFT GROUNDED)