FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Ceiling panel 1 consists of plastic composite element 3 with elements 5 arranged at lateral edges 4 extending in direction of aircraft flight path X to be jointed to aircraft airframe or at parts jointed therewith. Holder 6 is located at transverse edge 8 extending across aircraft flight path X while mating part 7 is arranged at opposite transverse edge 8. Holder 6 makes a complementary element for mating part 7. Every said holder 6 can interact with appropriate mating part 7 without using the tool for making plug-in joint of ceiling panels 1 with geometrical closure in vertical direction Z.
EFFECT: reduced vertical shift from one ceiling panel to adjacent panel, fast and simple mounting/dismantling.
19 cl, 13 dwg
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