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Continuing Airworthiness Challenges
SAE Technical Paper Series, 1994Structural safety is an evolutionary accomplishment, and attention to detail design features is key to its achievement. A multitude of design considerations is involved in ensuring the structural integrity of Boeing jet transports that have common design concepts validated by extensive analyses, tests, and three decades of service.
Ulf G. Goranson, Jack F. Mcguire
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Cybersecurity as Airworthiness
SSRN Electronic Journal, 2017The foundational Act in United States aviation regulation directed the Secretary of Commerce to “foster air commerce” and develop safety regulations in the process. The Federal Aviation Administration (“FAA”)’s modern duties include “assigning and maintaining safety as the highest priority in air commerce” and “encouraging and developing civil ...
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2010
Publisher Summary The airworthiness of an aircraft is concerned with the standards of safety incorporated in all aspects of its construction. These range from structural strength to the provision of certain safeguards in the event of crash landings and include design requirements relating to aerodynamics, performance, and electrical and hydraulic ...
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Publisher Summary The airworthiness of an aircraft is concerned with the standards of safety incorporated in all aspects of its construction. These range from structural strength to the provision of certain safeguards in the event of crash landings and include design requirements relating to aerodynamics, performance, and electrical and hydraulic ...
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2014
This book is aimed at advanced students and professionals, who are expected to have to make decisions regarding the fitness for service of new aviation products, whether whole aircraft or subsystems. This chapter compares initial and continued airworthiness and what goes into determining airworthiness, focusing primarily on civilian aeroplanes, with a ...
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This book is aimed at advanced students and professionals, who are expected to have to make decisions regarding the fitness for service of new aviation products, whether whole aircraft or subsystems. This chapter compares initial and continued airworthiness and what goes into determining airworthiness, focusing primarily on civilian aeroplanes, with a ...
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The Journal of the Royal Aeronautical Society, 1930
The object of the present paper is to place before the Society certain general considerations regarding the effect of airworthiness regulations on the design of civil aircraft.I should like first to thank the Air Ministry Authorities for permitting me to read this paper, and to explain that any opinions expressed are entirely my own.The Air Navigation ...
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The object of the present paper is to place before the Society certain general considerations regarding the effect of airworthiness regulations on the design of civil aircraft.I should like first to thank the Air Ministry Authorities for permitting me to read this paper, and to explain that any opinions expressed are entirely my own.The Air Navigation ...
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The Arithmetic of Airworthiness
The Journal of the Royal Aeronautical Society, 1954One of the many problems facing the aeronautical engineer is to make a vehicle, the reliability of which is tolerable, from an assembly of bits and pieces which, individually, are more or less unreliable. The practical answer has been to duplicate, triplicate, and generally to multiply the items about which doubt is felt.This approach to reliability ...
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Facilitating Continued Airworthiness [PDF]
, 2014 Initial airworthiness determines whether an aircraft or new part is fit for entry into use. However, for an aircraft to provide continued, safe, effective operation continued airworthiness is key. The way in which a part or aircraft deemed airworthy initially maintains its airworthiness is by regular inspection, maintenance, replacement when required ...
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Aircraft Engineering and Aerospace Technology, 1980
J.R.D. Kenward was with British Airways from 1950–1977: as Manager, Performance Engineering from 1967: from 1947–50, he was with BOAC in various technical branch posts. After graduation he entered the design office of De Havilland 1946–7. Since 1977 he has been a Consultant in aviation.
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J.R.D. Kenward was with British Airways from 1950–1977: as Manager, Performance Engineering from 1967: from 1947–50, he was with BOAC in various technical branch posts. After graduation he entered the design office of De Havilland 1946–7. Since 1977 he has been a Consultant in aviation.
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The Aeronautical Journal, 1978
In considering the necessity for requirements to establish the airworthiness of helicopters it is essential to take into account the capabilities of the vehicle itself, the environment in which the vehicle is likely to be used and the abilities of the people most likely to be involved with the vehicle.As envisaged by the inventors the helicopter is a ...
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In considering the necessity for requirements to establish the airworthiness of helicopters it is essential to take into account the capabilities of the vehicle itself, the environment in which the vehicle is likely to be used and the abilities of the people most likely to be involved with the vehicle.As envisaged by the inventors the helicopter is a ...
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2011
Publisher Summary This chapter discusses the airworthiness. For an aircraft, or aircraft part (airworthiness), is the possession of the necessary requirements for flying in safe conditions, within allowable limits. In this definition, three key elements deserve special consideration: safe conditions, possession of the necessary requirements, and ...
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Publisher Summary This chapter discusses the airworthiness. For an aircraft, or aircraft part (airworthiness), is the possession of the necessary requirements for flying in safe conditions, within allowable limits. In this definition, three key elements deserve special consideration: safe conditions, possession of the necessary requirements, and ...
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