Modular trim paneling and outfitting system for an aircraft passenger cabin interior

An aircraft passenger cabin outfitting system comprising:

• a first aircraft fuselage having a first cross-sectional dimension, and having a first passenger cabin therein adapted to said first cross-sectional dimension;
• a second aircraft fuselage having a second cross-sectional dimension different from said first cross-sectional dimension, and having a second passenger cabin therein adapted to said second cross-sectional dimension;
• a plurality of cabin interior sidewall panels that all respectively have the same dimensions and the same configuration as each other, wherein a first one of said sidewall panels is installed in said first passenger cabin in said first aircraft fuselage and a second one of said sidewall panels is installed in said second passenger cabin in said second aircraft fuselage;
• a plurality of stowage bins that all respectively have the same dimensions and the same configuration as each other, wherein a first one of said stowage bins is installed in said first passenger cabin in said first aircraft fuselage, a second one of said stowage bins is installed in said second passenger cabin in said second aircraft fuselage, respective gaps are formed between said sidewall panels and said stowage bins, and said gaps in said first passenger cabin have a different size than said gaps in said second passenger cabin;
• and
• a plurality of first light covers, and a plurality of second light covers that respectively have different dimensions relative to said first light covers, wherein said first light covers are installed to cover said gaps in said first passenger cabin, and said second light covers are installed to cover said gaps in said second passenger cabin.

An aircraft passenger cabin outfitting system comprising:

• a first aircraft fuselage having a first cross-sectional dimension, and having a first passenger cabin therein adapted to said first cross-sectional dimension;
• a second aircraft fuselage having a second cross-sectional dimension different from said first cross-sectional dimension, and having a second passenger cabin therein adapted to said second cross-sectional dimension;
• and
• a plurality of cabin interior components selected from among cabin trim components and cabin stowage bin components;
• wherein:
• said cabin trim components are one of:
• entire sidewall panels, main sidewall panels, upper sidewall panels, dado panels, ceiling panels, and cabin general illumination light covers;
• said cabin interior components all respectively have the same dimensions and the same configuration as each other;
• and
• a first one of said cabin interior components is installed in said first passenger cabin in said first aircraft fuselage while maintaining said same dimensions and said same configuration, and a second one of said cabin interior components is installed in said second passenger cabin in said second aircraft fuselage while maintaining said same dimensions and said same configuration.

An aircraft passenger cabin outfitting system comprising:

• a first aircraft fuselage having a first cross-sectional dimension, and having a first passenger cabin therein adapted to said first cross-sectional dimension;
• a second aircraft fuselage having a second cross-sectional dimension different from said first cross-sectional dimension, and having a second passenger cabin therein adapted to said second cross-sectional dimension;
• plurality of first cabin interior components selected from among cabin trim components and cabin stowage bins, that all respectively have the same first dimensions and the same first form-stable configuration as each other;
• and
• a plurality of second cabin interior components selected from among cabin trim components and cabin stowage bins, that all respectively have the same second dimensions and the same second form-stable configuration as each other;
• wherein one of said first cabin interior components and one of said second cabin interior components are installed in said first passenger cabin in said first aircraft fuselage while respectively maintaining said first form-stable configuration and said second form-stable configuration, and while overlapping each other in a first overlapping range in a circumferential direction in said first aircraft fuselage;
• and
• wherein another of said first cabin interior components and another of said second cabin interior components are installed in said second passenger cabin in said second aircraft fuselage while respectively maintaining said first form-stable configuration and said second form-stable configuration, and while overlapping each other in a second overlapping range in a circumferential direction in said second aircraft fuselage, wherein said second overlapping range has a different size than said first overlapping range.

An aircraft passenger cabin outfitting system comprising:

• a first aircraft fuselage having a first cross-sectional dimension, and having a first passenger cabin therein adapted to said first cross-sectional dimension;
• a second aircraft fuselage having a second cross-sectional dimension different from said first cross-sectional dimension, and having a second passenger cabin therein adapted to said second cross-sectional dimension;
• and
• plural first cabin interior components and plural second cabin interior components, that are each selected from among cabin trim components and cabin stowage bins;
• wherein said first cabin interior components all respectively have the same first dimensions and the same first form-stable configuration as each other, and said second cabin interior components all respectively have the same second dimensions and the same second form-stable configuration as each other;
• and
• wherein a first selected number of said first and second cabin interior components are installed in a first modular arrangement in said first passenger cabin in said first aircraft fuselage while maintaining said respective form-stable configurations of said respective cabin interior components, and a second selected number of said first and second cabin interior components are installed in a second modular arrangement in said second passenger cabin in said second aircraft fuselage while maintaining said respective form-stable configurations of said respective cabin interior components, and wherein said second selected number differs from said first selected number and/or said second modular arrangement differs from said first modular arrangement.