Considerations on EN 9100: 2016 / AS 9100D standard new changes
Journal Title: INCAS BULLETIN - Year 2018, Vol 10, Issue 1
Abstract
This article aims to highlight the main changes brought by the new edition of standard EN 9100: 2016 / AS 9100D. This standard is an effective tool for organizations working in the aerospace industry, providing the framework for achieving the ultimate goal of on-quality and on-time delivery of products and services. Using the SR EN ISO 9001: 2015 model for quality management system requirements and validation of compliance by third party assessment, EN 9100: 2016 / AS 9100D has been developed to include additional requirements that are of particular interest to the aerospace industry. Aspects of safety and performance of aerospace products are critical to stakeholders, appearing to be an uncompromising standard for guidance.
Authors and Affiliations
Ilinca SOARE, Emil MILITARU
BOOK REVIEWS: Problems of Quantitative Methods. Algebra, Trigonometry, Analytical Geometry and Mathematical Analysis (Part I) - Probleme de metode cantitative. Algebra, trigonometrie, geometrie analitica si analiza matematica (Partea I), Sorin BERBENTE, Corneliu BERBENTE Published by Editura Universitatii Romano-Britanice, Seria “Business”, Bucuresti, 2006, ISBN (10) 973-87669-1-5/ ISBN (13) 978-
On Lean Turbulent Combustion Modeling
This paper investigates a lean methane-air flame with different chemical reaction mechanisms, for laminar and turbulent combustion, approached as one and bi-dimensional problem. The numerical results obtained with Canter...
Book Review: English-Romanian Dictionary for Mechanical Engineering, Lorena DELEANU, Gabriela DIMA, Daniela SORCARU Editura Didactica si Pedagogica, Bucuresti, 2009 Vol. 1: A-M, Vol. 2: N-Z, ISBN 978-973-30-2595-5
Global Optimized Shapes of Flying Configurations Compared with Those of Gliding Birds
The determination of global optimized (GO) shape of a flying configuration (FC) (namely, the simultaneous optimization of its camber, twist and thickness distributions and also of the similarity parameters of its planfor...
Attitude Control Synthesis for Small Satellites Using Gradient Method. Part II Linear Equations, Synthesis
In order to continue paper [5] which presented the nonlinear equations of the movement for small satellite, this paper presents some aspects regarding the synthesis of the attitude control. After the movement equation li...