FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft module and method of its production. Module comprises frame component 2 and functional element 4. Lateral section serves to fasten functional element 4 and features configuration mating that of fuselage 6 or that of aircraft floor element 5. Note here that frame component surrounds functional element center of gravity and may be attached to aircraft floor element 5 in first position 7 and to elements of fastening to aircraft fuselage 6 in second position 7'. Functional element 4 may make seat elements 14, things storage pockets 11, info boards, galleys, W.C.s, passenger service blocks, lamps, air conditioners, loud speakers, TV sets, computers and oxygen masks. Besides, aircraft may use system made up of multiple modules that may transfer driven by electrical drive. Proposed method comprises the following jobs, i.e. mounting functional element 4 of frame component 2, attaching frame component 2 to aircraft floor element 5 in first position on the floor and attaching frame component 2 to fuselage 6 in second position 7'.
EFFECT: higher reliability of attachment.
24 cl, 29 dwg
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