I. Introduction
Huge volumes of data must be collected as part of testing activities related to large platforms. The flight test instrumentation (FTI) system is a vital system to acquire data during the flight test campaign. To be able to collect all required data, some components such as data acquisition units, network switches, recorders, digital buses, different analogue, and digital sensors, are needed to be integrated [1]. After that, hundreds of flight tests are performed during the development of aircraft systems. The main aim is to implement flight test activities, validating, verifying, and certifying the design after analysing the flight test data [2]. Instrumentation design engineers collect requests from systems engineers for platform sub-systems to determine data acquisition methods. Then, they evaluate these flight test instrumentation requests (FTIR) and provide their design with the corresponding requirement documents.