Spirit Aero Systems 787 8, 787 9 Wing Fixed / Movable Leading Edge Structures Work Values

Daily Duties at Spirit Aero Systems 787 8, 787 9 Wing Fixed / Movable Leading Edge Structures:

Design 787-9 Wing Movable Leading Edge Ribs: Worked on site at Boeing to optimize and integrate 787-9 Wing Movable Leading Edge Ribs for the new derivative. Coordinated closely with Design Lead Engineers and affected stakeholders including Stress, Materials and Processes, Weights, Manufacturing to optimize 787-9 Wing Movable Leading Edge Ribs. Completed release of all 787-9 Slat 1 and 6 MLE Rib MBDs, ARMs IRMs and RLMs. Burn down Manufacturing Change Requests: Coordinated with Boeing Design Lead Engineers to burn down Manufacturing Change Requests. Completed several CRs, releasing 787-8 Fixed Leading Edge MBDs, ARMs and IRMs to resolve problems encountered in the assembly of the 787-8. Design Slat 7 and 10 Static and Fatigue Test Fixtures: Designed a Static and Fatigue Test Fixture to simulate the 787-8 Fixed Leading Edge Main Track and Aux Track Rib Roller interface in the Retracted Preloaded and Take Off Preloaded positions for Slats 7 and 10. Coordinated Static and Fatigue Test Fixture interfaces directly with Tooling Engineers on site in Wichita, Kansas, while meeting loading requirements provided by Stress Analysts in Everett, Washington to insure first time quality and seamless interfaces between production hardware and Test Fixture parts. Developed and released hundreds of 787-8 Component Level Test parts. Design Flight Test parts to support wiring required for four Flight Test aircraft: Designed Flight Test Brackets required to support additional wiring for four Flight Test aircraft. Coordinated wiring to 787-8 Fixed Leading Edge structure interfaces with Design Lead Engineers and Flight Test Engineers when developing Brackets. Completed development and release of hundreds of 787-8 Flight Test parts supporting wiring required for Flight test of four 787-8 airplanes. Design Slat 9 Fatigue Test Fixture: Designed a Fatigue Test Fixture to simulate loads on a typical Slat. Coordinated Fatigue Test Fixture interfaces directly with Tooling Engineers on site in Wichita, Kansas, while meeting loading requirements provided by Stress Analysts in Everett, Washington to insure first time quality and seamless interfaces between production hardware and Test Fixture parts. Developed and released Component Level Test parts to interface with 787-8 Slat 9 six inch test specimens for Fatigue Tests.

What they like about Spirit Aero Systems 787 8, 787 9 Wing Fixed / Movable Leading Edge Structures:

Working in an organization that is technologically advanced, creative, and innovative is critical in your assessment of hiring companies. Less important to you are stability of the organization, the length of time an organization has been in business, and the business' plans for the future. You prefer a fast-moving company that will take risks to achieve its goals and objectives. The length of time the company has been in business is irrelevant. Maintaining status quo is unnecessary. You thrive on change, uncertainty and the upside of potential business risks, especially those associated with innovation. Stability for the long haul is not nearly as important as is working in an atmosphere that is charged with a sense of urgency and constant change.

Tags

CATIA V5, Relational Design, Structures Design, Static Test Fixture, Fatigue Test Fixture, Inlet, Fan Cowl, Optistruct, Enovia V5, TRAS Actuators, PDOS Actuators, Aircraft Interiors, F-35 Joint Strike Fighter, Outbd Wingbox, Major Fittings

Skills

These are some of the questions we asked our climbers about their experiences with Spirit Aero Systems 787 8, 787 9 Wing Fixed / Movable Leading Edge Structures: