38 deg C temp limit is for composite airframes? What a load of ....... so, what happens to the 787, 747,767,737, Airbus A330,A320,A340,A380 aircraft, all the gliders, Grob aircraft, and countless other airframes that sit parked in hangars and operate in environs far hotter than 38 deg C? what about all those composite engine cowls wrapped around countless Lycoming, continental, rotax, Rolls Royce GE and Pratt and whitney turbine engines? dont forgedt the internal core cowls that sit at temps well above 100 deg for trips across the pacific every day? all those composite F18s sitting and flying around the deserts of the middle east?
by they way, my specialty is Composite airframe structures..... that limit is just a Jabiru excuse. their airframes can handle well over 38 deg C, if they used the cheapest lowest rated epoxy resins, then the maximum will be 70 deg C.
unless of course, Jabiru dont use Milspec or aviation grade epoxy? hmmmmm