Premixed piloted jet flames are an ideal generic configuration to examine the impact of turbulence on thermo-chemical states for staged-combustion systems, like rich-quench-lean technologies, which have been proposed for ammonia combustion to minimize emissions. The current study aims to gain fundamental insights on the internal scalar structure of such premixed and rich-lean stratified ammonia-hydrogen flames. Turbulent premixed NH3/H2/N2-air jet flames, stabilized by a large, lean pilot flame (ϕ = 0.57), were investigated over a range of lean to rich global equivalence ratios (ϕglobal = 0.8, 1.2, and 1.6), employing simultaneous 1D Raman/Rayleigh spectroscopy with a novel calibration approach for NH3. The quantitative scalar data of instantaneous flame structures and thermo-chemical states are analyzed with emphasis on the NH3–H2 interaction and its effects on differential diffusion. In the transition from lean to rich jet flames, the spatial flame structures reveal the presence of residual H2 in the products, while a significant minimization of the NH3 slip is observed. The remaining H2 undergoes turbulent mixing with the hot exhaust gas causing additional heat release and elevated temperatures compared to 1D adiabatic flame simulations. The local oxygen concentration is found to be a determining factor in the interaction between thermal cracking and oxidation of NH3. Due to the formation of H2 as a result of NH3 cracking on the one hand and the oxidation reactions and diffusion of H2 on the other hand, a relatively high H2 concentration is still observed at relatively high temperatures despite the presence of O2. This interplay between in situ cracking, diffusion, turbulent mixing, and oxidation reactions leads to a zone of stratified combustion, so that overall a two-stage combustion characteristic is observed, showing premixed combustion primarily within the jet flow and stratified combustion in the mixing zone with the pilot exhaust gas.