SYSTEM AND METHOD FOR ASSEMBLING AN AFT FUSELAGE SECTION OF AN AIRCRAFT

A system and method for forming an aft fuselage section of an aircraft include a forward section having a stabilizer channel. The forward section includes an upper sill beam and a lower sill beam. One or more pivot fittings are securely fastened between the upper sill beam and the lower sill beam. T...

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Bibliographische Detailangaben
Hauptverfasser: BREEDLOVE, Max Tyler, JOSEPH, Joel, ROSMAN, Richard R, DIEP, Paul B
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A system and method for forming an aft fuselage section of an aircraft include a forward section having a stabilizer channel. The forward section includes an upper sill beam and a lower sill beam. One or more pivot fittings are securely fastened between the upper sill beam and the lower sill beam. The one or more pivot fittings are configured to pivotally couple to a horizontal stabilizer within the stabilizer channel.