Boeing Case Study Example | Topics and Well Written Essays - 2000 words

Boeing - Case Study Example in that location were a lot of apprehensions among the directors as the caller had not enough experience of developing a weather sheet of their own.Project Uncertainty and Risk Management, the project management was not effective in Boeing 767 program, is the first impuissance. Since the company did not have any past experience of cockpit design for cardinal soulfulnesss, it resulted in many difficulties in the successful execution of the final product. There should have been a through analysis of design forrader getting the final approval. Another weakness was that the geographic locations of production were also not considered. This hence became a major weakness as the transportation of parts was important on time. Time also became life-sustaining also due to the change in the design of cockpit.The strength was that the conversion of conversion from two-person to three person cockpit, which a very big risk was handled very intelligently. First stre ngth was that the delivery of the planes was just champion month jibeed. This conversion also raised project disbelief concern. As the parts were designed for two person cockpit and payments were al bushel made. The strength of project management was that it was decided that passing experts will fix this chore once parts are installed. This resulted in minimization of the risk of production disruption. Hence the project uncertainty arising from risk was avoided. This made the design of new cockpit more adaptable to changes.In terms of smell managements some other weakness aroused due to this conversion for space. This risk seemed to disrupt the modification of the thirty planes which were almost ready and were also ready to be flown. However, many managers opposed this approach as it violated the fire run across systems and may result in working environment without fire system for some time work the new system gets installed again (Shaw, 1999).Another weakness in terms of q uality was about the modification in production. Until all drawing and parts were available, cockpit work was delayed for two-crew models, and also demanded the alteration in the rill procedure. Testing of each system sequentially when it became operational was not possible then. Furthermore another weakness which reinforced this weakness was that functional testing was d unmatchable after complete installation of two-person cockpit. Hence the delay in problem detection and correction became another big weakness in terms of quality assurance. This gave chances for some errors and problem to be overlooked from one stage of installation to other.However, the strength of this program with postulate to the quality management was that parts installation was done only once and there were no subsequent removal hence the configuration was secured. This reduces the effort cost that might have incurred if parts were removed one after the