To add to what Franzkait has said, answer the question," How will the fuel be transferred out of the axle wing?" If you use a common method of the period (air pressure) just imagine what might happen if you take a sudden swerve and take out a runway light. Suppose the light tears a hole in the bottom of your pressurized axle fuel tank. Where does the fuel go? Are there any ignition sources?
Run the same scenario with an electric fuel pump. suppose the pump is energized at the time of the runway excursion and the wiring is damaged....
OK, I recognize that proper systems operation will mitigate some of these hazards, but why place fuel tanks in harms way?
For Franzkait, GFK is not a common term on the US side of the pond. The references I have found refer to a glass (or carbon) fiber reinforced plastic that is injection moldable. Is that what you are referring to?