Browse Topic: Regulations
This specification establishes the requirements for brush plating of cadmium by electrodeposition.
In the last years, new rotorcraft configurations have increased the attention among industries, through which the tiltrotor one due to its capability of combining both rotorcraft and aircraft advantages. However, there are situations where the vertical take-off mode could be enhanced in hard environmental and flight conditions. Therefore, to address this challenge, this work aims to develop a methodology to characterize a roll take-off model for a general tiltrotor configuration in such situations. By combining the integration of the equation of motion and geometrical assumptions, the runway distance is determined for an acceptable range of nacelle tilting angles. The process is developed by meeting the requirements defined by the regulations, combining the aircraft certification standards (CS23 and CS25) with the available tiltrotor certification basis from the FAA project #TC3419RC-R. Following the Nominal application, a sensitivity analysis is carried out, which studies the main
Aircraft development efforts are rapidly shifting toward the use of distributed electric propulsion. As the industry moves along a path to full electrification, hybrid propulsion systems will be increasingly employed where battery technology does not support a fully electric design. The fuel systems in new aircraft designs can be challenging, and the existing regulatory framework may not be capable of dealing with unique aircraft designs that do not neatly fit within existing categories. This presents a challenge to aircraft designers. Fuel remains essential to the propulsion system, and an optimal, yet simple fuel system will be necessary to leave room in the design trade space for more challenging and risky functions. Understanding the certification requirements and having a basic knowledge of the tradeoffs in fuel measurement accuracy are the key elements necessary to support a systems approach to optimizing a fuel measurement subsystem.
U.S. Army Aviation has extensively managed critical aircraft components based on the technical requirements and methods outlined in AMCOM Regulation 702-7 Flight Safety Parts/New Source Testing Program Management. This paper provides an overview of the newly revised AMCOM Regulation 702-7, previously published in October 2000. This update was necessary to keep up with the updated requirements of high tier documents, such Public Law 108-136, DA Pam 95-9, and other related regulations. This effort has produced a new AMCOM Regulation 702-7 Critical Safety Items (CSI), Critical Application Items (CAI), and New Source Testing (NST) Program Management, officially released in June 2017. The revised document addresses the complete quality oversight controls for CSIs and includes newly defined oversight and control requirements for CAIs. Furthermore, the new revision has been clarified by incorporating lessons learned while eliminating confusion and ambiguity from the previous document. The
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