Case Study On Boeing

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PROJECT COST MANAGEMENT PROBLEM IN BOEING 787 DREAMLINER
1. Introduction
1.1. Boeing is one of the largest and most powerful American multinational corporations which mostly designs, manufactures and sells airplanes along with rotorcrafts, rockets and satellites. The corporation lost its market share to Airbus in the late 1990s, so it was in need of a new aircraft that would generate revenues by creating value for customers.
1.2. In 2003, Boeing started a four years project to develop the 787 Dreamliner aimed at improving efficiency of the airplanes by using a composite material (carbon fiber, aluminum and titanium) in airplane manufacturing against the traditional material (aluminum) and an electrical system using lithium-ion batteries and …show more content…

This approach in the project was taken to reduce the manufacturing and assembly costs and development time but in reality this same decision from the management pushed the project more than three years behind schedule incurring billions of dollars expenses which was more than twice the allocated budget. It was challenging for Boeing to complete the project within allocated budget and time frame. The situation would be different if the corporation had kept the key technologies within the organization rather than outsourcing them as even with good technology, outsourcing possesses major risks in assembling the airplane because the components might not fit together. But these decisions were taken against the advice of a Boeing aerospace engineer Dr. L. J. Hart-Smith who knew these potential problems and presented them in a brilliant paper at a conference back in …show more content…

Boeing designed the 787 Dreamliner for long-haul transportation for 250 passengers for about a 20% lower fuel cost which was possible only if the aircraft's body were made using lightweight composite materials (but not the traditionally used aluminum) and with electrical system using lithium-ion batteries. But such composite materials were never before used to that extent in a large civilian aircraft. So it was challenging for the corporation to design such a big fuselage (a multi-sectional cylindrical barrel) covering the entire seating area of the aircraft and with more sections compared to that of aluminum-based fuselages which tend to fatigue. Thus these composite materials’ fuselages would reduce maintenance and replacement costs of the

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