FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Aircraft tail 1 consists of bearing structure 14 to support the engines extending through fuselage 6 via two openings 18, 18 at both sides of aircraft center plane axis P. Said bearing structure 14 consists of first and second semi-structures 22, 22 that pass through said first and second openings 18, 18. Said semi-structures are interconnected to allow their disassembly inside fuselage 8. Proposed method comprises displacing first semi-structure so that its inner end in passing through first opening is directed forward to pass through second opening with inner end directed forward so that inner end of first semi-structure is jointed with that of second inner semi-structure.
EFFECT: ease of assembly/disassembly.
10 cl, 14 dwg
