FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to frame element to be used in assembly of aircraft components, in particular, inner component or insulation pack. Frame element 10, 10' to be used in assembly system 46 may be jointed to aircraft structure 36 and comprises tie-down fitting to secure inner element 34 or insulation pack 52 to frame element 10, 10'. Said frame element 10, 10' comprises two tie-beams 12; 14; 12'; 14' arranged in parallel and connection tie-beam 16; 18; 16' extending between the latter. Connection tie-beam 16, 18 has recess 26, 28, 30, 32 to receive frame 42, 44 in jointing frame element 10 to structure 46. Assembly system 46 comprises several frame element 10, 10'. Said frame element with component 34, 53 jointed thereto is jointed to aircraft structure 36.
EFFECT: simple and fast mounting.
16 cl, 10 dwg
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