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    <copyright>Copyright © 2026. National Academy of Sciences. All rights reserved.</copyright>
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    <managingEditor>tris-trb@nas.edu (Bill McLeod)</managingEditor>
    <webMaster>tris-trb@nas.edu (Bill McLeod)</webMaster>
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      <title>Large passenger/cargo UAS market to reach $150 billion : sensor-carrying large UAS will lead the way; short-haul regional cargo flights to follow</title>
      <link>https://trid.trb.org/View/1507352</link>
      <description><![CDATA[]]></description>
      <pubDate>Mon, 02 Apr 2018 11:34:10 GMT</pubDate>
      <guid>https://trid.trb.org/View/1507352</guid>
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      <title>Researchers assess mid-air refuelling : is it viable for airlines--or just a flight of fancy?</title>
      <link>https://trid.trb.org/View/1355199</link>
      <description><![CDATA[]]></description>
      <pubDate>Tue, 26 May 2015 10:57:40 GMT</pubDate>
      <guid>https://trid.trb.org/View/1355199</guid>
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      <title>Bombardier's annual bizjet forecast released</title>
      <link>https://trid.trb.org/View/1213441</link>
      <description><![CDATA[]]></description>
      <pubDate>Tue, 11 Sep 2012 10:00:59 GMT</pubDate>
      <guid>https://trid.trb.org/View/1213441</guid>
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    <item>
      <title>The quest for STOL airliners</title>
      <link>https://trid.trb.org/View/1123834</link>
      <description><![CDATA[]]></description>
      <pubDate>Thu, 01 Dec 2011 11:13:34 GMT</pubDate>
      <guid>https://trid.trb.org/View/1123834</guid>
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      <title>Antonov blacklist</title>
      <link>https://trid.trb.org/View/807646</link>
      <description><![CDATA[Subtitle: Hundreds of the aircraft have been targeted for grounding until their airworthiness is assured.]]></description>
      <pubDate>Mon, 07 May 2007 13:55:02 GMT</pubDate>
      <guid>https://trid.trb.org/View/807646</guid>
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      <title>POSSIBILITY OF HEARING LOSS FROM EXPOSURE TO INTERIOR AIRCRAFT NOISE</title>
      <link>https://trid.trb.org/View/177469</link>
      <description><![CDATA[This report reviews criteria for hearing damage developed by the Committee on Hearing, Bioacoustics and Biomechanics (CHABA) of the National Academy of Science. It presents noise levels occurring in narrow and wide body commercial aircraft, business jet aircraft and short takeoff and landing (STOL) aircraft. It presents estimates of time exposure for pilots and crews based on FAA permitted flight times. It also provides estimations of possible hearing damage resulting from different exposures to interior noise of various aircraft types. (Author)]]></description>
      <pubDate>Tue, 30 Sep 2003 00:00:00 GMT</pubDate>
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    <item>
      <title>IMPROVING THE CONTINUED AIRWORTHINESS OF CIVIL AIRCRAFT</title>
      <link>https://trid.trb.org/View/496107</link>
      <description><![CDATA[This report focuses on the committee's primary task: defining the key elements of an improved aircraft certification safety management process for large transport airplanes and recommending how potential barriers to implementing the recommended process could be overcome. Chapter 2 provides background information on the role of AIR (Aircraft Certification Service), on how that role has evolved, and on specific regulatory actions that are part of the current safety management process. Chapter 3 provides background information on the causes of incidents and accidents. Chapter 4 describes the recommended safety management process, which includes a mechanism for monitoring its own effectiveness. Chapter 5 describes the relationships between human factors, environmental factors, and aircraft systems in accidents and incidents, followed by comments on several current initiatives to reduce accidents and incidents associated with human error. Chapter 6 recommends approaches for overcoming five key barriers to the implementation of the recommended safety management plan. Chapter 7 describes special characteristics of the small aircraft and rotorcraft communities and the special concerns that these characteristics raise with respect to the recommended safety management plan.]]></description>
      <pubDate>Wed, 24 Feb 1999 00:00:00 GMT</pubDate>
      <guid>https://trid.trb.org/View/496107</guid>
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    <item>
      <title>NASA AVIATION SAFETY REPORTING SYSTEM</title>
      <link>https://trid.trb.org/View/77614</link>
      <description><![CDATA[A decline in reports concerning small aircraft was noted; more reports involved transport aircraft, professional pilots, instrument meteorological conditions, and weather problems. A study of 136 reports of operational problems in terminal radar service areas was made. Pilot, controller, and system factors were found to be associated with these occurrences. Information transfer difficulties were prominent. Misunderstandings by pilots, and in some cases by controllers, of the policies and limitations of terminal radar programs were observed.]]></description>
      <pubDate>Sat, 29 Dec 1979 00:00:00 GMT</pubDate>
      <guid>https://trid.trb.org/View/77614</guid>
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    <item>
      <title>AIRFRAME TECHNOLOGY FOR ENERGY EFFICIENT TRANSPORT AIRCRAFT</title>
      <link>https://trid.trb.org/View/55537</link>
      <description><![CDATA[Fuel costs comprise a major portion of air transport operating costs.  Thus, energy efficiency is an essential design goal for future transport aircraft.  Advanced composite structures, advanced wing geometries, and active control systems all promise substantial benefits in fuel efficiency and direct operating cost for derivative and new aircraft introduced by 1985.  Technology for maintenance of a laminar boundary layer in cruise offers great benefits in fuel efficiency and direct operating cost and may be ready for application to transports introduced in the 1990's. NASA and the air transport industry are cooperating in a comprehensive Aircraft Energy Efficiency Program to expedite the introduction of these advanced technologies into production aircraft.]]></description>
      <pubDate>Wed, 09 Nov 1977 00:00:00 GMT</pubDate>
      <guid>https://trid.trb.org/View/55537</guid>
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    <item>
      <title>FLIGHT DISPLAYS FOR THE NEXT GENERATION AIRCRAFT</title>
      <link>https://trid.trb.org/View/55543</link>
      <description><![CDATA[The increasing complexity of the operational environment will dictate the requirement, and the advanced technology will provide improved information transfer warranting the conclusion.  The next generation of commercial transports will no longer be designed principally for manual controls with electromechanical instruments.  The cockpit designs of new aircraft will incorporate instruments and displays with digital interfaces and effective monitoring to exploit the inherent advantages of automatic controls.  Modern systems engineering will be applied to the design of caution and warning systems and the designs of advanced sytems, such as multifunction switching, to reduce crew workload and stress.]]></description>
      <pubDate>Wed, 09 Nov 1977 00:00:00 GMT</pubDate>
      <guid>https://trid.trb.org/View/55543</guid>
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    <item>
      <title>SIMULATION'S POTENTIAL ROLE IN ADVANCED AIRCRAFT CERTIFICATION</title>
      <link>https://trid.trb.org/View/55542</link>
      <description><![CDATA[It is the opinion of the FAA that future developments in air transportation will introduce significantly greater complexity into the aircraft and the operating system than now exists.  Past experience with simulation techniques indicate they contain the potential of contributing significantly to the safe and rapid introduction of these new technologies.  It is the intent of the FAA to explore this potential in detail to ensure that maximum values can be gained thru its exploitation.]]></description>
      <pubDate>Wed, 09 Nov 1977 00:00:00 GMT</pubDate>
      <guid>https://trid.trb.org/View/55542</guid>
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    <item>
      <title>SUMMARY AND ANALYSIS OF FEASIBILITY-STUDY DESIGNS OF V/STOL TRANSPORT AIRCRAFT</title>
      <link>https://trid.trb.org/View/27024</link>
      <description><![CDATA[Studies of the technical feasibility of V/STOL concepts for commercial short haul transport aircraft emphasizing the technical aspects of aircraft design have been completed. Various VTOL and STOL short haul transport concepts are compared in terms of design gross weight, direct operating cost, gust sensitivity, and perceived noise levels; the impact on this comparison of design range requirements, austere design philosophy, advanced technology, nonproductive time, and other considerations is included.]]></description>
      <pubDate>Thu, 05 Sep 1974 00:00:00 GMT</pubDate>
      <guid>https://trid.trb.org/View/27024</guid>
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