Abstract: An aircraft electronic device retention mechanism and method of removeably supporting an aircraft electronic device having first electrical contacts within a cockpit having compatible second electrical contacts includes a base that is generally configured to the size and shape of a surface of the electronic device and at least one lever that is mounted by a pivot to the base. The lever(s) has an engaging portion that is adapted to engage an engaged portion of the electronic device and an actuation portion. The actuation portion is adapted to rotate the lever(s) about said pivot between a first orientation in which the engaging portion retains the engaged portion and a second orientation in which the engaging portion does not retain said engaged portion. A manual actuator is connected with the actuation portion of the pivot.