Advanced wing integration and ground test completed

Before closure of the wing structure all relevant systems test equipment wiring sensors and actuators need to integrated and tested A detail description of the final wing buildup and internal layout will be documented as well as results from the initial testing of the integrated equipment Due to the fuselage rebuilt several additional tests are necessary to prove the flight worthiness of the aircraft what are also described in this deliverableThe DD actuator acceptance taxi tests and the GVT for the improved demonstrator under construction are described in this deliverable