awing 2553-0037 Rev C as approved on FAA form 8110.3 per Stephen Formes DERT-230238-CE dated Dec 20, 2013. INSTRUCTIONS FOR CONTINUEDAIRWORTHINESS. THE REMOVAL OF THE INTERIOR IS ON THE CONDITION OF FAILURE. THERE ARE NO ADDITIONAL INSPECTIONS REQUIRED. CONTINUE TO INSPECT JAW MANUFACTURERS MBA, SRIL OR CMM AS APPLICABLE