DECOMPRESSION PANEL FOR USE IN AN AIRCRAFT

A method of installing and replacing a plurality of decompression panels into a sidewall assembly of an aircraft includes coupling a first decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly. The method also includes inserting a tab of the first decompression...

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Bibliographic Details
Main Authors Olliges Michael J, Glaze Tatum Jeremy Ryan, Arm Hannah Rebecca, Loken Allan A, Perkins Thomas
Format Patent
LanguageEnglish
Published 16.02.2017
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT
HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:A method of installing and replacing a plurality of decompression panels into a sidewall assembly of an aircraft includes coupling a first decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly. The method also includes inserting a tab of the first decompression panel into a slot of a second decompression panel. The slot is defined by a flange extending along a surface of the second decompression panel. The method further includes coupling the second decompression panel to at least one of a sidewall and a floor panel of the sidewall assembly.
Bibliography:Application Number: US201615336397