AIRCRAFT STRUCTURAL PARTS

Brand Owner (click to sort) Address Description
717 BOEING MANAGEMENT COMPANY M/C 110-SB36 2201 Seal Beach Blvd. Seal Beach CA 907401515 Aircraft and structural parts and manuals therefor;
CARBON CUB CUB MARKS 1819 S. 16th Ave. Yakima WA 98903 Aircraft and structural parts for aircraft made in significant part of carbon or carbon fiber;CARBON;
CUB CUB MARKS 1819 S. 16th Ave. Yakima WA 98903 Aircraft and structural parts for aircraft;
CUB Cub Crafters, Inc. 1918 South 16th Avenue Yakima WA 98902 Aircraft and structural parts for aircraft;
FSI Flight Structures, Inc. 11404 Commando Road Everett WA 98204 Aircraft structural parts, namely, crew rest areas and bunks, [ doors, ] floor beams, frames, ducting, deep ceiling tubs, closets and seating class dividers;Designing and engineering aircraft and accessories; testing, analysis and evaluation of the goods, namely, aircraft components and accessories, of others for the purpose of certification;
FSI FLIGHT STRUCTURES INC. Flight Structures, Inc. 11404 Commando Road Everett WA 98204 Aircraft structural parts, namely, crew rest areas and bunks,[ doors, ] floor beams, frames, ducting, deep ceiling tubs, closets and seating class dividers;FLIGHT STRUCTURES INC.;Designing and engineering aircraft and accessories; testing, analysis and evaluation of the goods, namely, aircraft components and accessories, of others for the purpose of certification;
PERMAFLEX TWIN COMMANDER AIRCRAFT 1176 Telecom Dr. Creedmoor NC 27522 aircraft structural parts, namely, deicing boots;
SECURITECT PPG INDUSTRIES OHIO, INC. 3800 West 143rd Street Cleveland OH 44111 Aircraft structural parts, namely, doors, partitions, panels, bulkheads, and floors; structural parts for land, sea, and air vehicles, namely, transparencies for use as windshields and windows;
 

Where the owner name is not linked, that owner no longer owns the brand

    
Technical Examples
  1. A process and device for detecting on an aircraft an overshoot of design loads at the level of a structural part of the aircraft. The detection device includes a speed measuring device for measuring an effective speed of the aircraft. A first comparator compares the measured effective speed with a maximum speed relating to the current flight configuration of the aircraft. A vertical load measuring device measures a vertical load factor of the aircraft, and a second comparator compares the measured vertical load factor with a limit value of the vertical load factor. An inspection determining device determines whether a structural inspection needs to be performed at the level of the structural part, based of the results of the first and second comparisons.