Evaluation of Two Unique Side Stick Controllers in a Fixed-Base Flight Simulator
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Cockpit Image Recorders: a Picture Is Worth a Thousand Words
Cockpit Image Recorders 1051 t1152111 2005, CCH INCORPORATED. All Rights Reserved. Reprinted with permission from "Issues in Aviation Law and Policy." Cockpit Image Recorders: A Picture Is Worth a Thousand Words by David E. Rapoport and Paul D. Richter May 2005 Everywhere we go our moves are randomly recorded, but sug- gest a video camera be placed in the cockpit of an aircraft, a pilot's workplace, and watch out! The pilot unions immediately switch off the auto-pilot and begin complaining how this would be a clear and abominable violation of their members' privacy rights. Do bankers, gas station attendants, convenience store clerks, jailers, blackjack dealers and doormen colnplain about cameras in their workplaces? Would we listen if they did? For the last four years, the U.S. National Transportation Safety Board's (NTSB) goal of putting video cameras in the cockpits of large commercial jets has been frustrated, in large part, by the efforts of the major pilot unions. This article will review the efforts by the NTSB and others to require video cameras in the cockpits of large transport category aircraft, discuss the arguments for and against this proposal, and conclude the time has coine for the Federal Aviation Administration (FAA) to put safety first and follow the NTSB's five-year-old recommendation that it mandate video cameras in the cockpit. Cockpit Video Image Recorders Are Now on the NTSB's "Most Wanted" List The NTSB, an independent Federal agency, is charged by Congress with investigating every civil aviation accident in the United States.' The NTSB's primary function is to promote safety Issues in Aviation Law and Policy 1052 Aviation Safety/Security it1 tran~portation.~Since inception, the NTSB has investigated more than 124,000 aviation accidents. -
How a Cockpit Remembers Its Speeds
COGNITIVE SCIENCE 19, 265-288 (1995) How a Cockpit Remembers Its Speeds EDWIN HUTCHINS University of California, San Diego Cognitive science normally takes the individual agent as its unit of analysis. In many human endeavors, however, the outcomes of interest are not determined entirely by the information processing properties of individuals. Nor can they be inferred from the properties of the individual agents, alone, no matter how detailed the knowledge of the properties of those individuals may be. In com- mercial aviation, for example, the successful completion of a flight is produced by a system that typically includes two or more pilots interacting with each other and with a suite of technological devices. This article presents a theoretical framework that tokes a distributed, socio-technical system rather than an indi- vidual mind as its primary unit of analysis. This framework is explicitly cognitive in that it is concerned with how information is represented and how representa- tions are transformed and propagated in the performance of tasks. An analysis of a memory task in the cockpit of a commercial airliner shows how the cognitive properties of such distributed systems can differ radically from the cognitive properties of the individuals who inhabit them. Thirty years of research in cognitive psychology and other areas of cognitive science have given us powerful models of the information processing prop- erties of individual human agents. The cognitive science approach provides a very useful frame for thinking about thinking. When this frame is applied to the individual human agent, one asks a set of questions about the mental An initial analysis of speed bugs as cognitive artifacts was completed in November of 1988. -
Faa Ac 20-186
U.S. Department Advisory of Transportation Federal Aviation Administration Circular Subject: Airworthiness and Operational Date: 7/22/16 AC No: 20-186 Approval of Cockpit Voice Recorder Initiated by: AFS-300 Change: Systems 1 GENERAL INFORMATION. 1.1 Purpose. This advisory circular (AC) provides guidance for compliance with applicable regulations for the airworthiness and operational approval for required cockpit voice recorder (CVR) systems. Non-required installations may use this guidance when installing a CVR system as a voluntary safety enhancement. This AC is not mandatory and is not a regulation. This AC describes an acceptable means, but not the only means, to comply with Title 14 of the Code of Federal Regulations (14 CFR). However, if you use the means described in this AC, you must conform to it in totality for required installations. 1.2 Audience. We, the Federal Aviation Administration (FAA), wrote this AC for you, the aircraft manufacturers, CVR system manufacturers, aircraft operators, Maintenance Repair and Overhaul (MRO) Organizations and Supplemental Type Certificate (STC) applicants. 1.3 Cancellation. This AC cancels AC 25.1457-1A, Cockpit Voice Recorder Installations, dated November 3, 1969. 1.4 Related 14 CFR Parts. Sections of 14 CFR parts 23, 25, 27, 29, 91, 121, 125, 129, and 135 detail design substantiation and operational approval requirements directly applicable to the CVR system. See Appendix A, Flowcharts, to determine the applicable regulations for your aircraft and type of operation. Listed below are the specific 14 CFR sections applicable to this AC: • Part 23, § 23.1457, Cockpit Voice Recorders. • Part 23, § 23.1529, Instructions for Continued Airworthiness. -
A “Short Course” on Ice and the TBM
A “Short Course” on Ice and the TBM. Icing is topical at the present time as a result of a recent accident in a TBM. I have had a number of conversations with pilots who I would consider knowledgeable and it is apparent that there is a lot of confusion surrounding this subject. Also noting on line posts this confusion is not limited to owner pilots. I have had occasion to be a victim of my own stupidity in a serious icing condition years ago and I can vouch that icing is a deadly serious situation in more ways than one. Before going on with the subject we want to stipulate that the data we are about to provide is a summary of information that is to be found on line, along with narrative and data provided from knowledgeable instructors, if any of the data provided conflicts with anything you have been taught we urge you to satisfy yourself as to which data is correct. TBM operators fly in the same airspace where we find Part 25 aircraft (Commercial Category) aircraft. There is a big difference in how these two categories of aircraft are affected by icing conditions. A 767 will often be climbing at over 300 kts and 4000+ ft/min at typical icing altitudes. This creates two very distinct advantages for the 767: first, their icing exposure time may be less than 1/3 of ours. Second, icing conditions are a function of TAT (Total Air Temperature), not SAT (static air temp). TAT is warmer than SAT because of the effects of compressibility as the airplane operates at faster and faster speeds. -
Cessna Owner Magazine Article, October 2017
The following article appeared in the October 2017 edition of CESSNA OWNER magazine, the official publication of the Cessna Owner Organization. Whether for business or pleasure, the Official Publication of the Cessna Owner Organization Since 1975 Cessna Owner Organization is dedicated to assisting CESSNA>> October 2017 aircraft owners in OWNER MAGAZINE their continual pursuit to become better, TKS smarter and safer ROTECTION owners and pilots. ICE P Since 1975, the Liquid Armor for the collective knowledge War on Icing and experience of its members has saved owners countless hours of downtime and thousands of dollars in operational expenses. www.cessnaowner.org www.facebook.com/ CessnaOwnerOrganization Est. 1975 Not a member? Learn more at www.CessnaOwner.org TKS Ice Protection Liquid Armor for the War on Icing By Scott Sherer here are many people out accumulation before launching. I wind is strong and the wind chill there who really like snow also have a heavy-duty tug for get- is very low. The winter cloud in Tsports; things like skiing, ting my bird in and out of the han- Wisconsin is dark and grey. (I say snowboarding, ice skating, hockey, gar quickly, and the Janitrol fur- “cloud” and not “clouds” because we snowmobiling and all of those other nace, along with an assortment of seem to have only one cloud here sports that you typically see during other engine and interior warming and it covers the entire state from the winter Olympics. I’m sure that contraptions, helps to get my plane November well into January!) many aviators enjoy some of these warm and ready fast. -
Leading the Charge We Put TBM 940 Speedster Through Its Paces for NBAA
15-21 October 2019 I flightglobal.com FLIGHT TEST Leading the charge We put TBM 940 speedster through its paces for NBAA £3.90 Wow, how? ACES high 42 Questions remain over defunct US Air Force boosts Collins Icelandic carrier’s comeback 13 with ejection seat deal 20 9 770015 371310 FLIGHT TEST Power of one Turboprop-single family has been a market success since launch in 1988, amassing sales of more than 900 units across three variants Daher has delivered a compelling offer for owner-flyers, with a range of enhancements on the TBM 940 providing an edge over the piston-twin segment. We put it through its paces MICHAEL GERZANICS POMPANO BEACH have allowed single-engined designs to make to be efficient. Airspace congestion, however, inroads into the twin-turbine segment. can make reaching optimum altitudes for jets he single-engined turboprop market The growth of the single-engined turbo- problematic, so their real-world range can be is populated by numerous aircraft of prop segment is based on the near-bulletproof shorter. Jets also have higher direct operating varying configurations. In broad reliability and scalability of the PT6 family. costs, however. T strokes, it can be broken down into This paradigm shift from piston-twins to tur- Runway performance and training require- two segments: fast, low-winged aircraft and bine-singles is conceptually on par with ex- ments are also two factors that fuel the single- slower, more spacious high-winged designs. tended twin-engine operations authorisations engined turboprop segment, because runway In the West, these diverse offerings share a all but killing off three- and four-engined civil length for turboprops is shorter than that single critical component – their engine. -
LORD Flight Control Equipment
LORD Flight Control Equipment ELECTROMECHANICAL SOLUTIONS LORD provides customers innovative offerings globally with best-in-class cockpit controls • Inceptors to convert pilot inputs into flight control system commands • Force feedback optimized for pilot effectiveness • Electromechanical actuators for deployment of doors, landing gear, vents and control surfaces • Worldwide distribution, repair and overhaul network with AOG stock, servicing OEMs and end users Typical Applications: Benefits: • Cockpit Controls/ • Enable safer flights Inceptors Flight Controls for Business and Commercial Aircraft • Reduce pilot workload • Actuators • Reduce aircraft weight • Sensors • Optimize drag of wings • Dampers Side Stick • Enhance pilot comfort Throttle Control Flaps and Spoiler Levers Electric Pedals Actuator Systems for Aircraft and Helicopters • Door Systems • Flight Control Systems • Force Feel Systems • Locking Systems Our extensive experience in commercial fixed wing flight control systems and our innovative active vibration control systems in helicopters combine to make us a great partner for providing advanced flight control interfaces for aerospace applications. Cockpit Control Solutions LORD inceptors provide functional and ergonomic interfaces between pilots and various aircraft systems. Our Cockpit Control solutions are compact and lightweight and can be seamlessly integrated into cockpit designs. LORD flight control inceptors can be tailored to sidestick or yoke based cockpit layouts. Pilot Interface with: Modular Inceptor Components: • Flight Control Systems • Force Feel Dampers • Engine Control Systems • RVDT Transducer Units • Landing Gear Systems • Force Transducer Units Integrated Inceptors: • Auto Throttle Control Unit • Speed Brake Control Unit • Flap and Slat Control Unit • Nose Wheel Steering Hand Wheel • Side Stick (or Yoke) • Rudder and Brake Pedals Electromechanical Actuators Current aircraft primarily use hydraulic actuators to move surfaces and manage the landing gear operations. -
Cockpit Human Factors Research Requirements
© U.S. Department of Transportation Federal Aviation Administration COCKPIT HUMAN FACTORS RESEARCH REQUIREMENTS COCKPIT HUMAN FACTORS RESEARCH REQUIREMENTS prepared by: U.S. Department of Transportation Research and Special Programs Administration Transportation Systems Center Cambridge, MA02142 for U.S. Department of Transportation Federal Aviation Administration Washington, DC 20591 APRIL, 1989 Table Of Contents SECTION _ PAGE EXECUTIVE SUMMARY 1 1.0 INTRODUCTION 4 1.1 HISTORY 4 1.2 BACKGROUND 5 1.3 CIVIL AVIATION HUMAN FACTORS ACTIVITIES OUTSIDE THE FAA 5 1.4 SPECIFIC APPLICATION AREAS 6 1.4.1 Aircraft Automation 6 1.4.2 Right Deck Certification 7 1.4.3 Warning and Alerting Systems 7 1.4.4 Operator Errors andAccident Analysis 8 1.4.5 Displays 9 1.4.6 Controls 10 1.4.7 Right Crew Training 10 2.0 OVERVIEW 13 2.1 PROGRAM RATIONALE 13 2.2 OBJECTIVES OF THIS DOCUMENT 14 2.3 PROGRAM OPERATIONS 14 2.4 PROGRAM DESCRIPTION 15 3.0 RESEARCH REQUIREMENTS 17 3.1 COCKPIT AUTOMATION 19 3.1.1 Pilot Intervention andControl (Manual Reversion) 20 3.1.2 Pilot Proficiency and Automated Systems 21 SECTION PAGE 3.2 DISPLAYS AND CONTROLS 23 3.2.1 Information Transfer (Right Deck Information Requirements) 24 3.2.2 InformationTransfer (DisplayDesign) 26 3.2.3 Standardization of Right Deck Displays, Controls, and Procedures 28 3.2.4 Human Performance Criteria for Terminal Procedures 29 3.2.5 Human Performance Criteria for Instrument Procedure Charts 30 3.2.6 Weather Information Collection and Dissemination 32 3.2.7 RotorcraftDisplay and Control-IFR Requirements -
F-117A Accident During Air Show Flyover Caused by Omission of Fasteners in Wing-Support Structure
FLIGHT SAFETY FOUNDATION Aviation Mechanics Bulletin SEPTEMBER–OCTOBER 1998 F-117A Accident during Air Show Flyover Caused by Omission of Fasteners in Wing-support Structure FLIGHT SAFETY FOUNDATION Aviation Mechanics Bulletin Dedicated to the aviation mechanic whose knowledge, craftsmanship and integrity form the core of air safety. Robert A. Feeler, editorial coordinator September–October 1998 Vol. 46 No. 5 F-117A Accident during Air Show Flyover Caused by Omission of Fasteners in Wing-support Structure.......................................................... 1 Maintenance Alert ...................................................................................... 9 News & Tips ............................................................................................... 13 AVIATION MECHANICS BULLETIN Copyright © 1998 FLIGHT SAFETY FOUNDATION INC. ISSN 0005-2140 Suggestions and opinions expressed in FSF publications belong to the author(s) and are not necessarily endorsed by Flight Safety Foundation. Content is not intended to take the place of information in company policy handbooks and equipment manuals, or to supersede government regulations. Staff: Roger Rozelle, director of publications; Wayne Rosenkrans, senior editor; Mark Lacagnina, senior editor; John D. Green, copyeditor; Rick Darby, editorial consultant; Karen K. Ehrlich, production coordinator; Ann L. Mullikin, assistant production coordinator; and David Grzelecki, librarian, Jerry Lederer Aviation Safety Library. Subscriptions: US$35 (U.S.-Canada-Mexico), US$40 Air Mail (all other countries), six issues yearly. • Include old and new addresses when requesting address change. • Flight Safety Foundation, Suite 300, 601 Madison Street, Alexandria, VA 22314 U.S. • Telephone: (703) 739-6700 • Fax: (703) 739-6708 We Encourage Reprints Articles in this publication, in the interest of aviation safety, may be reprinted, in whole or in part, in all media, but may not be offered for sale or used commercially without the express written permission of Flight Safety Foundation’s director of publications. -
Digital Fly-By-Wire
TF-2001-02 DFRC Digital Fly-By-Wire "The All-Electric Airplane" Skies around the world are being filled with a new generation of military and commercial aircraft, and the majority of them are beneficiaries of one of the most significant and successful research programs conducted by NASA's Dryden Flight Research Center -- the Digital Fly-By-Wire flight control system. The Dryden DFBW program has changed the way commercial and military aircraft are designed and flown. Aircraft with fly-by- wire systems are safer, more reliable, easier to fly, more NASA F-8 modified to test a digital fly-by-wire flight control system. maneuverable and fuel NASA Photo ECN 3276 efficient, and maintenance costs are reduced. Flight control systems link pilots in their cockpits with moveable control surfaces out on the wings and tails. These control surfaces give aircraft directional movement to climb, bank, turn, and descend. Since the beginning of controlled flight in the early 1900s, wires, cables, bellcranks, and pushrods were the traditional means of connecting the control surfaces to the control sticks and rudder pedals in the cockpits. As aircraft grew in weight and size, hydraulic mechanisms were added as boosters because more power was needed to move the controls. The Digital Fly-By-Wire (DFBW) program, flown from 1972 to 1985, proved that an electronic flight control system, teamed with a digital computer, could successfully replace mechanical control systems. 1 Electric wires are the linkage between the cockpit automatically compensates -- as many as 40 and control surfaces on a DFBW aircraft. Command commands a second -- to keep the aircraft in a stable signals from the cockpit are processed by the digital environment. -
Kc-10A, T/N 83-0080 9Th Air Refueling Squadron 60Th Air Mobility Wing Travis Air Force Base, California
UNITED STATES AIR FORCE AIRCRAFT ACCIDENT INVESTIGATION BOARD REPORT KC-10A, T/N 83-0080 9TH AIR REFUELING SQUADRON 60TH AIR MOBILITY WING TRAVIS AIR FORCE BASE, CALIFORNIA LOCATION: NEAR MOUNTAIN HOME AFB, IDAHO DATE OF ACCIDENT: 1 NOVEMBER 2016 BOARD PRESIDENT: COL PERRY M. LONG III Conducted IAW Air Force Instruction 51-503 ACTION OF THE CONVENING AUTHORITY 1 0 JUL 2117 The report of the accident investigation board, conducted under the provisions of AFI 51-503, that investigated the 1 November 2016 mishap that occurred near Mountain Home Air Force Base, Idaho, involving KC-10A, T/N 83-0080, assigned to the 60th Air Mobility Wing, Travis Air Force Base, California, complies with applicable regulatory and statutory guidance and on that basis is approved. \\signed\\ fHOMA^J; Major General, U| Vice Commander United States Air Force Accident Investigation Board Report Class A Mishap, Near Mountain Home AFB, ID EXECUTIVE SUMMARY UNITED STATES AIR FORCE AIRCRAFT ACCIDENT INVESTIGATION KC-10A, T/N 83-0080 NEAR MOUNTAIN HOME AFB, IDAHO 1 NOVEMBER 2016 On 1 November 2016, at 1546 hours Zulu time (Z), a United States Air Force KC-10A Extender, tail number 83-0080, the mishap aircraft, assigned to the 60th Air Mobility Wing, departed from its home station of Travis Air Force Base (AFB), California, on a training mission in support of two flights of F-15s and a C-17. The scheduled flight profile was a formation departure from Travis AFB, refueling for approximately one hour with the F-15s, refueling training for approximately 1 hour 15 minutes with the C-17, and approximately one half hour of approach training before landing at Travis AFB. -
Influence of Coupled Sidesticks on the Pilot Monitoring's Awareness
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Institute of Transport Research:Publications Influence of Coupled Sidesticks on the Pilot Monitoring's Awareness During Flare Alan F. Uehara∗ and Dominik Niedermeiery DLR (German Aerospace Center), Braunschweig, Germany, 38108 Passive sidesticks have been used in modern fly-by-wire commercial airplanes since the late 1980s. These passive sidesticks typically do not feature a mechanical coupling between them, so the pilot's and copilot's sidesticks move independently. This characteristic disabled the pilot monitoring (PM) to perceive the control inputs of the pilot flying (PF). This can lead to problems of awareness in abnormal situations. The development of active inceptor technology made it possible to electronically couple two sidesticks emulating a mechanical coupling. This research focuses on the benefits of coupled sidesticks to the situation awareness of the PM. The final approach and landing scenario was considered for this study. Twelve pilots participated in the simulator experiment. Results suggest that the coupling between sidesticks, allowing the PM to perceive the PF's inputs, can improve the PM's situation awareness. Nomenclature ADI Attitude Director Indicator PF Pilot Flying AGL Above Ground Level PFD Primary Flight Display ATC Air Traffic Control PM Pilot Monitoring DLR German Aerospace Center PNF Pilot Not Flying FAA Federal Aviation Administration SA Situation Awareness FBW Fly-By-Wire SOP Standard Operating Procedure FCS Flight Control System TOGA Takeoff/Go-Around KCAS Knots Calibrated Airspeed VMC Visual Meteorological Conditions IMC Instrument Meteorological Conditions I. Introduction he control inceptors and the actuators of the control surfaces are mechanically decoupled in fly-by-wire T(FBW) airplanes.