The History Of

Total Page:16

File Type:pdf, Size:1020Kb

The History Of * cover (Final) 2/18/04 2:27 PM Page 1 The History of The XV-15 Tilt Rotor Research Aircraft From Concept to Flight The History of the XV-15 Tilt Rotor Research Aircraft:FromConcepttoFlight Research Rotor Tilt The HistoryoftheXV-15 Monograph 17NASASP-2000-4517 National Aeronautics and Space Administration Martin D. Maisel • Demo J. Giulianetti • Daniel C. Dugan NASA SP-2000-4517 The History of the XV-15 Tilt Rotor Research Aircraft: From Concept to Flight Martin D. Maisel Demo J. Giulianetti and Daniel C. Dugan Monographs in Aerospace History #17 The NASA History Series National Aeronautics and Space Administration Office of Policy and Plans NASA History Division Washington, D.C. 2000 Contents Prologue . iii Dedication . v Acknowledgments . vii Forewords . ix List of Figures . xiii List of Acronyms . xix Introduction . 1 Early Efforts. 4 XV-3 Program . 12 NASA-Army Cooperation . 19 Building the Technology Base. 20 Tilt Rotor Research Aircraft Project Office. 28 Aircraft Development . 42 Navy Participation . 59 Flight Envelope Expansion . 61 Flight Research . 65 Incidents. 83 Paris Air Show . 88 Evaluations and Demonstrations . 91 Crash . 98 The End of an Era . 100 XV-15 Project Summary . 103 Epilogue . 105 Appendix A Aircraft Descriptions . 115 Appendix B Key Personnel . 133 Appendix C Chronology . 140 Appendix D Awards and Records . 154 Appendix E Photo Gallery. 157 Appendix F Bibliography of Tilt Rotor Related Publications. 164 About the Authors . 185 Index . 187 i Prologue This monograph is a testament to the efforts of many people overcoming multi- ple technical challenges encountered while developing the XV-15 tilt rotor research aircraft. The Ames involvement with the tilt rotor aircraft began in 1957 with investiga- tions of the performance and dynamic behavior of the Bell XV-3 tilt rotor air- craft. At that time, Ames Research Center was known as the Ames Aeronautical Laboratory of the National Advisory Committee for Aeronautics (NACA). As we approach the new millennium, and after more than 40 years of effort and the successful completion of our initial goals, it is appropriate to reflect on the technical accomplishments and consider the future applications of this unique aircraft class, the tilt rotor. The talented engineers, technicians, managers, and leaders at Ames have worked hard with their counterparts in the U.S. rotorcraft industry to overcome technolo- gy barriers and to make the military and civil tilt rotor aircraft safer, environmen- tally acceptable, and more efficient. The tilt rotor aircraft combines the advantages of vertical takeoff and landing capabilities, inherent to the helicopter, with the forward speed and range of a fixed wing turboprop airplane. Our studies have shown that this new vehicle type can provide the aviation transportation industry with the flexibility for high- speed, long-range flight, coupled with runway-independent operations, thus hav- ing a significant potential to relieve airport congestion. We see the tilt rotor air- craft as an element of the solution to this growing air transport problem. I am proud of our past accomplishments and ongoing efforts in the development of tilt rotor technology. Much remains to be done to continue to develop and fur- ther enable quiet, ultra-safe, cost-efficient flight for this class of vehicles. I am convinced that Ames Research Center will continue to provide the leadership necessary to be in the forefront of new developments leading to the introduction of tilt rotor aircraft into the aviation transportation system of the 21st century. Enjoy the aviation historical journey that unfolds on the following pages. Harry McDonald Director, NASA Ames Research Center iii Dedication The story of the successful development of the tilt rotor aircraft is not just about technology, but also about the efforts of many capable people who dedicated themselves to what they believed would be an important advancement in avia- tion. The tasks proved to be technically challenging and involved both high financial and safety risks. This history, therefore, is dedicated to all of the people who held on to the dream and made it possible, and especially to those who, unfortunately, have passed on and are not able to witness the remarkable product of their work. A partial list of these people includes: Bob Lichten and Lovette Coulter of Bell Helicopter Textron Inc.; Pip Gilmore of the Boeing Helicopter Company; Laurel (Shorty) Schroers and Gary Churchill of the U.S. Army; and Jim Weiberg, Dr. Leonard Roberts, and Jerry Bree of the NASA Ames Research Center. Their efforts have advanced aeronautical technology significantly and made their mark on aviation history. v Acknowledgments The authors wish to acknowledge Frank J. Aguilera, manager of the Ames Advanced Tilt Rotor Technology Office, who requested the writing of this histo- ry and who sponsored the work. This account of the history of the development of tilt rotor technology is the product of valuable contributions from many peo- ple, each of whom played a key role in the long chain of events that led to the successful accomplishment of the tilt rotor research aircraft program goals. Firsthand recollections and comments were provided by Bell Helicopter personnel, both active and retired, including Dick Stansbury, Jerry Pickard, Jose Caero, Claude Liebensberger, Jack DeTore, John Williams, Sam Ferguson, and Hank Smyth. We are especially indebted for assistance provided by Ron Reber of Bell Helicopter Textron Inc., who provided the link to other Bell per- sonnel and who generously made available Bell’s large resource of XV-3 and XV-15 still photographs. Former and current Government employees who pro- vided important information included Paul Yaggy and Dave Sharpe of the Army laboratory at Ames; Woody Cook, Dave Few, Mike Bondi, Don Reynolds, and John Wilson of NASA Ames; John Ward of NASA Headquarters; and Hal Andrews of NAVAIR. The authors also thank John Schneider (retired), Ken Bartie and Hal Rosenstein of the Boeing Helicopter Company for photographs and information, and Jay Hendrickson for background about the Platt-LePage Aircraft Company. In addition, the authors wish to thank tilt rotor pioneer Mario Guerrieri for his input regarding the Transcendental Aircraft Corporation. Finally, the authors wish to acknowledge Roger W. Ashbaugh of the Documentation and Technology Branch and Lynn L. Albaugh, Capitol Resource Management, both at Ames, for their assistance in preparing this publication. The authors have made every effort to ensure that the historical accounts in this document are reported accurately and that the people associated with these events are correctly identified. However, due to limitations of the available docu- mentation, the names of some individuals may have been inadvertently omitted. Also, the reader should be aware that some information is not presented chrono- logically because events that are important in telling this story often occurred separately but during the same time period. There are also a number of people at NASA Headquarters who helped in various ways. In the NASA History Office, M. Louise Alstork edited, proofread, and pre- pared the index while Stephen J. Garber and Nadine J. Andreassen also assisted with editing and production. Roger D. Launius, the NASA Senior Historian, pro- vided much useful overall guidance. The Printing and Design Office developed the layout and handled the printing. Geoff Hartman and Joel Vendette handled the editing and design, respectively, while Jeffery Thompson and Stanley Artis saw this work through the publication process. Thanks are due them all. vii Foreword The development of tilt rotor aircraft technology involved some of the same fac- tors that led to other important aeronautical accomplishments of this century. The vision of a few individuals in search of a practical and efficient new aircraft design, commitment to their goals, and their willingness to continue to pursue their objective while encountering major technical problems and programmatic challenges were critical ingredients in this tale. However, the unique aspect of the tilt rotor story was the combined Government and industry focused effort that was sustained for over four decades to explore, comprehend, develop, and refine this technology. The remarkable product of the investment of public and private funds, and the efforts of the people dedicated to the concept, is an aircraft type that will have an impact on civil and military aviation that will rival the introduc- tion of the practical helicopter more than 60 years ago. As this book is being written, the first production V-22 Osprey tilt rotor aircraft is being prepared for delivery to the U.S. Marine Corps and the Bell-Augusta BA609 six- to nine-passenger civil tilt rotor aircraft is well into the development phase. When these new vehicles enter service, I am confident that other visionar- ies will find new uses for this capability, both in the civil transport and military arenas. The tilt rotor aircraft has come of age. I have had the good fortune to have been closely associated with a significant element of this activity, the XV-15 tilt rotor research aircraft project, for several decades. It is fitting that this adventure in aeronautical technology development be recorded. I know firsthand that the success of the tilt rotor can be credited to the capable industry and Government individuals whose story is told in the fol- lowing pages. Hans Mark Director of Defense Research and Engineering Office of the Secretary of Defense Director, NASA Ames Research Center, 1969-1977 ix Foreword The XV-15 tilt rotor research aircraft program resulted in part from earlier inves- tigations by the U.S. military seeking new and more efficient concepts for air support of field operations. The XV-3 tilt rotor emerged from the Army/Air Force convertiplane program of the 50s as a strong contender. However, it faced significant stability problems that discouraged many supporters and threatened to swamp the program.
Recommended publications
  • Silicon Valley Chapter Military Officers Association of America
    Silicon Valley Chapter Military Officers Association of America Volume XII Issue 11The Bulletin Dec 2015 OFFICERS, BOARD, AND CHAIRS PRESIDENT: Lt. Col. Mike Sampognaro USAF merry christmas to all 408-779-7389 1st VP: Lt. Col. Jay Craddock USAF 650-968-0446 2nd VP: CWO5 Robert Landgraf USMC 408-323-8838 Secretary: COL Warren Enos AUS Luncheon Program 408-245-2217 Treasurer: CAPT Lloyd McBeth USN 408-241-3514 17 Dec 2015 Past President: CAPT Paul Barrish USN 408-356-7531 Touring Morocco DIRECTORS & COMMITTEE CHAIRS Auxiliary Liaison vacant Chaplain Chaplain Fred Tittle USMC 609-802-3492 Commissary/Exchange Advisory CDR Ralph Hunt USN 650-967-8467 Friends-in-Need (FIN) Program CDR Al Mouns USN 408-257-5629 Programs Lt. Col. Jesse Craddock USAF 650-968-0446 ROTC CWO4 Patrick Clark USA 831-402-8548 Membership/Recruitment CWO5 Robert Landgraf USMC 408-323-8838 Scholarship CAPT Paul Barrish USN 408-356-7531 Travel (Space-A Advisory) CDR V.A. Eagye USN 408-733-3177 Web Master Lt Col Mike Sampognaro USAF 408-779-7389 Veteran Affairs Col Keith Giles,USAF(ret) Lt Col Neil Miles USAF 408-929-1142 Development Officer CAPT Gil Borgardt USN 650-342-1270 Sargeant-at-Arms Social Hour: 11:00 AM CDR Ralph Hunt USN 650-967-8467 Chapter Outreach CWO5 Robert Landgraf USMC 408-323-8838 Luncheon: 11:45 AM CALMOAA, Legislation & Navy League Liaison LCDR Tom Winant USN 650-678-7120 Luncheon is $26.00 Personal Affairs CAPT Robert French USN 650-363-1188 See Back Page for Reservations Form and Directions The Chapter Board meets at the Moffett Air Traffic Control Tower, Moffett Federal Airfield Bulletin Editor It is time to renew your Lt.
    [Show full text]
  • NSIAD-95-133 Military Bases: Analysis of DOD's 1995 Process
    United States General Accounting Office Report to the Congress and the GAO Chairman, Defense Base Closure and Realignment Commission April 1995 MILITARY BASES Analysis of DOD’s 1995 Process and Recommendations for Closure md Realignment GAO/NSIAD-95-133 National Security and International Affairs Division B-26 1024 April 14,1995 To the President of the Senate and the Speaker of the House of Representatives The Honorable Alan J. Dixon Chairman, Defense Base Closure and Realignment Commission The Secretary of Defense announced his 1995 recommendations for base closures and realignments to the Defense Base Closure and Realignment Commission on February 28,1995. This report responds to the Defense Base Closure and Realignment Act of 1990 (P.L. 101~510), as amended, which requires that we provide the Congress and the Commission, by no later than April 15,1995, a report on the recommendations and selection process. We have identified issues for consideration by the Commission as it completes its review of the Secretary of Defense’s recommendations. Given that this is the last of three biennial reviews authorized under the 1990 act, we are also including matters for consideration by the Congress regarding the potential need for continuing Iegislation to authorize further commission reviews and authorize changes, as needed, to prior decisions We are sending copies of this report to the Chairmen, Senate Committee on Appropriations, Subcommittee on Defense; Senate Committee on Armed Services; House Committee on Appropriations, Subcommittee on National Security; House Committee on National Security; the Secretaries of Defense, the Army, the Navy, and the Air Force; and the Directors of the Defense Logistics Agency and the Defense Investigative Service.
    [Show full text]
  • The Luftwaffe Wasn't Alone
    PIONEER JETS OF WORLD WAR II THE LUFTWAFFE WASN’T ALONE BY BARRETT TILLMAN he history of technology is replete with Heinkel, which absorbed some Junkers engineers. Each fac tory a concept called “multiple independent opted for axial compressors. Ohain and Whittle, however, discovery.” Examples are the incandes- independently pursued centrifugal designs, and both encoun- cent lightbulb by the American inventor tered problems, even though both were ultimately successful. Thomas Edison and the British inventor Ohain's design powered the Heinkel He 178, the world's first Joseph Swan in 1879, and the computer by jet airplane, flown in August 1939. Whittle, less successful in Briton Alan Turing and Polish-American finding industrial support, did not fly his own engine until Emil Post in 1936. May 1941, when it powered Britain's first jet airplane: the TDuring the 1930s, on opposite sides of the English Chan- Gloster E.28/39. Even so, he could not manufacture his sub- nel, two gifted aviation designers worked toward the same sequent designs, which the Air Ministry handed off to Rover, goal. Royal Air Force (RAF) Pilot Officer Frank Whittle, a a car company, and subsequently to another auto and piston 23-year-old prodigy, envisioned a gas-turbine engine that aero-engine manufacturer: Rolls-Royce. might surpass the most powerful piston designs, and patented Ohain’s work detoured in 1942 with a dead-end diagonal his idea in 1930. centrifugal compressor. As Dr. Hallion notes, however, “Whit- Slightly later, after flying gliders and tle’s designs greatly influenced American savoring their smooth, vibration-free “Axial-flow engines turbojet development—a General Electric– flight, German physicist Hans von Ohain— were more difficult built derivative of a Whittle design powered who had earned a doctorate in 1935— to perfect but America's first jet airplane, the Bell XP-59A became intrigued with a propeller-less gas- produced more Airacomet, in October 1942.
    [Show full text]
  • Shelf List 05/31/2011 Matches 4631
    Shelf List 05/31/2011 Matches 4631 Call# Title Author Subject 000.1 WARBIRD MUSEUMS OF THE WORLD EDITORS OF AIR COMBAT MAG WAR MUSEUMS OF THE WORLD IN MAGAZINE FORM 000.10 FLEET AIR ARM MUSEUM, THE THE FLEET AIR ARM MUSEUM YEOVIL, ENGLAND 000.11 GUIDE TO OVER 900 AIRCRAFT MUSEUMS USA & BLAUGHER, MICHAEL A. EDITOR GUIDE TO AIRCRAFT MUSEUMS CANADA 24TH EDITION 000.2 Museum and Display Aircraft of the World Muth, Stephen Museums 000.3 AIRCRAFT ENGINES IN MUSEUMS AROUND THE US SMITHSONIAN INSTITUTION LIST OF MUSEUMS THROUGH OUT THE WORLD WORLD AND PLANES IN THEIR COLLECTION OUT OF DATE 000.4 GREAT AIRCRAFT COLLECTIONS OF THE WORLD OGDEN, BOB MUSEUMS 000.5 VETERAN AND VINTAGE AIRCRAFT HUNT, LESLIE LIST OF COLLECTIONS LOCATION AND AIRPLANES IN THE COLLECTIONS SOMEWHAT DATED 000.6 VETERAN AND VINTAGE AIRCRAFT HUNT, LESLIE AVIATION MUSEUMS WORLD WIDE 000.7 NORTH AMERICAN AIRCRAFT MUSEUM GUIDE STONE, RONALD B. LIST AND INFORMATION FOR AVIATION MUSEUMS 000.8 AVIATION AND SPACE MUSEUMS OF AMERICA ALLEN, JON L. LISTS AVATION MUSEUMS IN THE US OUT OF DATE 000.9 MUSEUM AND DISPLAY AIRCRAFT OF THE UNITED ORRISS, BRUCE WM. GUIDE TO US AVIATION MUSEUM SOME STATES GOOD PHOTOS MUSEUMS 001.1L MILESTONES OF AVIATION GREENWOOD, JOHN T. EDITOR SMITHSONIAN AIRCRAFT 001.2.1 NATIONAL AIR AND SPACE MUSEUM, THE BRYAN, C.D.B. NATIONAL AIR AND SPACE MUSEUM COLLECTION 001.2.2 NATIONAL AIR AND SPACE MUSEUM, THE, SECOND BRYAN,C.D.B. MUSEUM AVIATION HISTORY REFERENCE EDITION Page 1 Call# Title Author Subject 001.3 ON MINIATURE WINGS MODEL AIRCRAFT OF THE DIETZ, THOMAS J.
    [Show full text]
  • Wake Turbulence and Separation Standards
    Tel: +267 3 6882 00 /3913236 Aeronautical Information Services Fax: +267 3913121 P O Box 250 AIC Email: [email protected] Gaborone AFS: FBHQYAYX BOTSWANA 06/11 01 MAR WAKE TURBULENCE AND SEPARATION STANDARDS INTRODUCTION The hazards associated with wake turbulance have long been demonstrated by a number of accidents and incidents. There is at the present time insufficient understanding of the correlation between turbulant wake theory and operational experience to state with an acceptable degree of certainty what weight classifications should be denoted and what separation should be applied between them. In the meantime ICAO has issued guidance material and this forms the basics of procedures being introduced in Botswana with immediate effect. CHARACTERISTICS Wake turbulence vortices are present behind every aircraft, but are particularly severe when generated by large and wide-bodied jet aircraft. These vortices are two counter- rotating cylindrical air masses trailing aft from the aircraft. The vortices are most dangerous to following aircraft during the take-off, initial climb, final approach and landing phases of flight. They tend to drift down, and when close to the ground move sideways from the track of the generating aircraft occasionally rebounding upwards. The characteristics of the wake vortex generated by an aircraft in flight are established initially by factors related to the aircraft gross weight, airspeed, configuration and wingspan. Subsequently, the vortices characteristics are altered and eventually dominated by interactions between the vortices and the ambient atmosphere. The wind,wind shear, turbulence and atmospheric stability affect the motion and decay of a vortex system. Vortex wake generation begins on rotation when the nose wheel lifts off the runway and ends when the nose wheel touches down on landing.
    [Show full text]
  • FAA Order 8130.2H, February 4, 2015
    U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADM INISTRATION ORDER 8130.2H 02/04/2015 National Policy SUBJ: Airworthiness Certification of Products and Articles This order establishes procedures for accomplishing original and recurrent airworthiness certification ofaircraft and related products and articles. The procedures contained in this order apply to Federal Aviation Administration (FAA) manufacturing aviation safety inspectors (ASI), to FAA airworthiness AS Is, and to private persons or organizations delegated authority to issue airworthiness certificates and related approvals. Suggestions for improvement of this order may be submitted using the FAA Office of Aviation Safety (AVS) directive feedback system at http://avsdfs.avs.faa.gov/default.aspx, or FAA Form 1320-19, Directive Feedback Information, found in appendix I to this order. D G!JD Cf1 · ~ David Hempe Manager, Design, Manufacturing, & Airworthiness Division Aircraft Certification Service Distribution: Electronic Initiated By: AIR-1 00 02/04/2015 8130.2H Table of Contents Paragraph Page Chapter 1. Introduction 100. Purpose of This Order .............................................................................. 1-1 101. Audience .................................................................................................. 1-1 102. Where Can I Find This Order .................................................................. 1-1 103. Explanation of Policy Changes ................................................................ 1-1 104. Cancellation ............................................................................................
    [Show full text]
  • Bell 429 Product Specifications
    BELL 429 SPECIFICATIONS BELL 429 SPECIFICATIONS Publisher’s Notice The information herein is general in nature and may vary with conditions. Individuals using this information must exercise their independent judgment in evaluating product selection and determining product appropriateness for their particular purpose and requirements. For performance data and operating limitations for any specific mission, reference must be made to the approved flight manual. Bell Helicopter Textron Inc. makes no representations or warranties, either expressed or implied, including without limitation any warranties of merchantability or fitness for a particular purpose with respect to the information set forth herein or the product(s) and service(s) to which the information refers. Accordingly, Bell Helicopter Textron Inc. will not be responsible for damages (of any kind or nature, including incidental, direct, indirect, or consequential damages) resulting from the use of or reliance on this information. Bell Helicopter Textron Inc. reserves the right to change product designs and specifications without notice. © 2019 Bell Helicopter Textron Inc. All registered trademarks are the property of their respective owners. FEBRUARY 2019 © 2019 Bell Helicopter Textron Inc. Specifications subject to change without notice. i BELL 429 SPECIFICATIONS Table of Contents Bell 429 ..................................................................................................................................1 Bell 429 Specification Summary (U.S. Units) ........................................................................4
    [Show full text]
  • Archaeological Resources Study, February 2017
    NASA Ames Research Center Archaeological Resources Study Prepared for: Prepared by: February 2017 NASA Ames Research Center Archaeological Resources Study Table of Contents 1. INTRODUCTION............................................................................................................. 1 1.1 Project Description...................................................................................................1 1.2 Preparers ..................................................................................................................1 2. CULTURAL SETTING ................................................................................................... 4 2.1 Prehistoric and Ethnohistoric Context .....................................................................4 2.2 Historic Context .......................................................................................................5 2.2.1 Spanish Period ..............................................................................................5 2.2.2 Mexican Period ............................................................................................6 2.2.3 American Period ...........................................................................................6 2.2.4 Moffett Field ..............................................................................................13 2.2.5 Ames Research Center ...............................................................................17 3. ARCHIVAL RESEARCH.............................................................................................
    [Show full text]
  • National Transportation Safety Board Aviation Accident Final Report
    National Transportation Safety Board Aviation Accident Final Report Location: IRVINE, CA Accident Number: LAX97FA059 Date & Time: 11/30/1996, 1307 PST Registration: N2TE Aircraft: Morane-Saulnier MS760 II Aircraft Damage: Destroyed Defining Event: Injuries: 3 Fatal Flight Conducted Under: Part 91: General Aviation - Personal Analysis Shortly after takeoff, the pilot radioed the air traffic control tower declaring an emergency and stating his intent to return for landing. He stated that he had taken off with an external boarding ladder attached to the aircraft. Several witnesses reported that the aircraft's downwind leg was too close to the airport causing the aircraft to overshoot the turn to the final approach course, and that the pilot increased the aircraft's bank angle as he tried to align the aircraft with the landing runway. As the aircraft was intercepting the final approach course, it abruptly rolled inverted, the nose dropped, and the aircraft spiraled onto the roof of an industrial building. A Boeing 757 aircraft, landing on the same runway, had passed over the accident site 2 minutes and 17 seconds earlier. The B-757 was cleared to land before the accident aircraft received a takeoff clearance and was on the runway when the pilot declared the emergency and turned downwind. The local controller did not issue a wake turbulence advisory. Experienced MS760 pilots reported that the aircraft will exhibit no adverse performance or safety affects with the boarding ladder attached. Probable Cause and Findings The National Transportation Safety Board determines the probable cause(s) of this accident to be: The pilot's failure to maintain an adequate airspeed margin while maneuvering in a steep banked turn to the landing runway, which resulted in an inadvertent stall/spin.
    [Show full text]
  • Easy Access Rules for Standardised European Rules of the Air (SERA)
    Easy Access Rules for Standardised European Rules of the Air (SERA) EASA eRules: aviation rules for the 21st century Rules and regulations are the core of the European Union civil aviation system. The aim of the EASA eRules project is to make them accessible in an efficient and reliable way to stakeholders. EASA eRules will be a comprehensive, single system for the drafting, sharing and storing of rules. It will be the single source for all aviation safety rules applicable to European airspace users. It will offer easy (online) access to all rules and regulations as well as new and innovative applications such as rulemaking process automation, stakeholder consultation, cross-referencing, and comparison with ICAO and third countries’ standards. To achieve these ambitious objectives, the EASA eRules project is structured in ten modules to cover all aviation rules and innovative functionalities. The EASA eRules system is developed and implemented in close cooperation with Member States and aviation industry to ensure that all its capabilities are relevant and effective. Published December 20201 1 The published date represents the date when the consolidated version of the document was generated. Powered by EASA eRules Page 2 of 213| Dec 2020 Easy Access Rules for Standardised European Rules Disclaimer of the Air (SERA) DISCLAIMER This version is issued by the European Aviation Safety Agency (EASA) in order to provide its stakeholders with an updated and easy-to-read publication. It has been prepared by putting together the officially published regulations with the related acceptable means of compliance and guidance material (including the amendments) adopted so far.
    [Show full text]
  • Air Traffic Management for Tiltrotors Questions and Answers
    ASS. NAZ. ASSISTENTI E CONTROLLORI DELLA NAVIGAZIONE AEREA ITALIAN AIR TRAFFIC CONTROLLERS’ ASSOCIATION MEMBER OF IFATCA INTERNATIONAL FEDERATION OF AIR TRAFFIC CONTROLLERS’ ASSOCIATIONS AIR TRAFFIC MANAGEMENT FOR TILTROTORS QUESTIONS AND ANSWERS Issue 2 Introduction The history of aviation has seen many technologies developed and matured by the military prior to their introduction into commercial service such as jet propulsion, fly-by-wire flight controls and composite primary structures. Today tiltrotor technology follows a similar path, having been successfully demonstrated by the military for over 10 years in the Bell Boeing V-22, the Leonardo Helicopters AW609 is on the verge of civil certification for commercial use. As the speed, range, and VTOL capability of the V-22 tiltrotor has revolutionized military missions like combat search and rescue, medical evacuation, and long-range ship to shore transportation, so too will the AW609 in commercial SAR, EMS, and offshore oil and gas transportation. The AW609’s use in civil operations will enable true point to point travel and help reduce congestion at busy airports. As the technology and operational regulations are on the horizon1, some questions, remarks or concerns may arise within the Air Traffic Management (ATM) community on how to integrate tiltrotor activities into usual aircraft management and on how to interact with tiltrotor flights. This joint document between Leonardo Helicopters and the Italian Air Traffic Controllers Association ANACNA aims to provide answers to these points. From a Gate-to-Gate perspective this Q&A sheet is divided into the different flight phases: 1. Departure 2. In flight 3. Arrival 4.
    [Show full text]
  • Bell Uh-1 Iroquois
    BELL UH-1 IROQUOIS UH-1 SERVICE Manufacturer: Bell Helicopter Corp. of Bell Aircraft Corp., Fort Worth, Texas, USA (In 1960, became Bell Helicopter Co., Textron Corp.) (In 1976, became Bell Helicopter Textron, Textron Inc.) Models: Model 204, 205, 208, 210, 211, 212, 214, 412, 450, 533, 577 Designations: H-1 (UH-1); H-40, H-48, HU-1, CH-118 / CH-135 / CH-146 (CAF) Names: Iroquois; Huey (unofficial), Venom & Super Huey (UH-1Y) First official flight: XH-40 22/10/1956 Factory production period: 1955 – 1987 (military) 1963 – present (civil) Primary service period: 1959 – 1980’s Last official flight: - - UH-1 VARIANTS 1956 Model 204 XH-40 3 1956 Model 204 YH-40 6 Total: 00009 1959 Model 204 HU-1A (UH-1A) 182 1960 Model 204 YHU-1B (YUH-1B) 4 1961 Model 204 HU-1B (UH-1B) 1030 1965 Model 204 UH-1C 755 Total: 01971 1961 Model 205 YHU-1D (YUH-1D) 7 1963 Model 205 UH-1D 2010 Total: 02017 1963 Model 204 UH-1E 209 1964 Model 204 UH-1F 120 1967 Model 204 TH-1F 26 Total: 00355 1967 Model 205 UH-1H 5648 1968 Model 205 CUH-1H 10 1971 Model 205 HH-1H 30 Total: 05688 1969 Model 204 HH-1K 27 1969 Model 204 TH-1L 90 1968 Model 204 UH-1L 8 Total: 00125 1969 Model 212 UH-1N 288 1971 Model 212 CUH-1N 50 1974 Model 212 VH-1N 6 Total: 00344 2006 Model 450 UH-1Y 135 Total: 00135 1962 Model 204 Model 204 80 1968 Model 205 Model 205 332 1969 Model 212 Model 212 917 1970 Model 214 Model 214 509 1981 Model 412 Model 412 1026 Total: 02864 Total: 13508 Foreign built – Indonesia: 1986 Model 412 NBell 412 30 Total: 00030 Foreign built – Italy: 1961 Model 204 Model AB.204
    [Show full text]