Disclosed is an aircraft that comprises a fuselage, a left wing and a right wing opposite one another with respect to said fuselage and each enclosing at least one fuel tank. According to certain transparency aspects, the encryption and decryption functionality of the invention do not require any changes to the software layers such as file systems, device drivers, operating systems, or applications. The inside needle may be adapted to electrically contact one or more electrical semiconductor circuit components located below the semiconductor layer. A subsequent heating cycle raises the assembly to the reflow temperature of the solder balls, thereby attaching the solder balls to the underlying solder bump pads, and at least partially curing the polymer material to form a support collar at the base region of each attached solder ball. The motion detection mechanism is magnetically coupled to a pointer rotation mechanism configured to indicate the position of the diaphragm and the corresponding pressure sensed by the diaphragm.