Abstract: A mounting bracket for holding a heat insulating mat in an aircraft cabin has a lower and an upper section configured to conform to a trough-shaped flange of a stringer secured to the fuselage. A holding pin forms part of the lower section and can be connected to the insulating mat. The two sections are onto the stringer (2) as a clip. For this purpose the lower section (4) fits with a trough (10) around the stringer (2) and the upper section (5) formed with a snap-in locking device including an expander pin (9) is arranged with a barrel portion in the trough of the stringer. The upper section (5) has a plate (14) tangentially merging into the barrel portion and extending outside the stringer (2) for the snap-in action.

Abstract: A connecting device is provided in aircraft for attaching of built-in elements such as galley and lavatory walls, storage cabinets and the like to structural parts of the airframe. The connecting device meets the special requirements of aircraft construction, reliably prevents corrosion at the structure and at the same time allows for an adjustment for balancing tolerances. The connecting device is constructed such that the individual elements of the connecting device can be combined to each other, that the built-in elements can be adjusted in their position regarding the x-, y-, and z-directions, that as desired space can be provided above the floor level and that the connection bores of the structure are provided with sealing rings.