Fan case with thrust reverser cascade section, corresponding fan section and gas turbine engine

A fan case (72) of a gas turbine engine (20) includes a fan blade containment section (78) defined about an engine axis (A), a thrust reverser cascade section (80) downstream of the blade containment section (78) and a Fan Exit Guide Vane section (82) downstream of the thrust reverser cascade section (80). A corresponding fan section (22) and a gas turbine engine (20) are also provided.