The Flight Phase Adaptive Aero-Servo-Elastic Aircraft Design Methods (FliPASED) project opens a completely new dimension for the integrated aircraft design, since coupling between aeroelasticity, gust response, flight control methods, instrumentation and certification aspects is not exploited in current aircraft designs. A common set of models, coupled with joint requirements enable a multidisciplinary-optimized design for the entire aircraft, leading to more optimized overall performance. The demonstrator T-FLEX built within the FLEXOP project is carried over to FLiPASED and flights FT7-FT23 were flown with it, generating useful data for the aeroelasticity community. After an in-flight incident on 30/08/2022 the demonstrator was re-built as P-FLEX and flights FT24-FT37 were flown with the new demonstrator. Including active flutter control tests. The flight test data and corresponding documentation are published in the present repository.