FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft door hinge. Proposed hinge assembly comprises door support assembly attached to door, and hinge lever assembly. The latter comprises first toothed assembly attached to aircraft, second toothed assembly attached to door support assembly, and jointing assembly connected to first and second toothed assemblies. Said first and second toothed assemblies interact to displace door support assembly and hinge lever assembly relative to each other to retain the door, in fact, parallel with aircraft on opening the door.
EFFECT: easier entry and exit for passengers.
20 cl, 21 dwg
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