MD HELICOPTERS DELIVERS NEW MD 600N with ADVANCED, FAA-CERTIFIED ALL-GLASS COCKPIT Authorized Sales Representative Sapura Aero Accepts New, Multi-Mission MD 600N

Total Page:16

File Type:pdf, Size:1020Kb

MD HELICOPTERS DELIVERS NEW MD 600N with ADVANCED, FAA-CERTIFIED ALL-GLASS COCKPIT Authorized Sales Representative Sapura Aero Accepts New, Multi-Mission MD 600N FOR IMMEDIATE RELEASE MD HELICOPTERS DELIVERS NEW MD 600N WITH ADVANCED, FAA-CERTIFIED ALL-GLASS COCKPIT Authorized Sales Representative Sapura Aero accepts new, multi-mission MD 600N The new MD 600N features an integrated all-glass cockpit; utility/personnel transport & single-patient EMS capability Mesa, Ariz., October 17, 2017 – MD Helicopters, Inc. (MDHI) announces the delivery of a new MD 600N to its Subang, Malaysia- based sales agent, Sapura Aero. Configured with the company’s upgraded FAA type-certified all- glass cockpit, this MD 600N also features single-patient EMS interior from Air Ambulance Technology (AAT). “I am proud to deliver this exquisite aircraft to our partners at Sapura Aero, and am excited about the growth that this delivery will inspire in the region,” said Lynn Tilton, Chief Executive Officer for MD Helicopters. “We have an excellent relationship with the Sapura team built on a shared commitment to operational and organizational excellence. With this delivery complete, I am confident we will move forward with a focus on rapid expansion and excellence in customer experiences.” Type-Certified Glass Cockpit At the 2017 HAI Heli-Expo in Dallas, Texas, MD Helicopters announced their commitment to deliver FAA- certified all-glass cockpits to the company’s full range of single- and twin-engine aircraft. In June of this year the company announced it had completed all FAA certification requirements for the MD 600N cockpit upgrade. On July 26, 2017, the type certification was granted. MDHI’s single-engine all-glass cockpit features: Howell Instruments Electronic Flight Instrument System Garmin G500 (GDU620) PFD/MFD Garmin GTN 650 Touchscreen NAV/COM/GPS L-3 ESI 500 Electronic Standby Instrument Flexible, Multi-Function Cabin Design Renowned for its ergonomic, modular interior design, the MD 600N has the flexibility to support up to six (6) different cabin configurations. This aircraft was delivered with the ability to effortlessly transition 4555 E. MCDOWELL ROAD, MESA, AZ 85215 MDHELICOPTERS.COM between three (3) of these options in order to meet its anticipated mission requirements for utility/personnel transport and Emergency Medical/Air Ambulance Services. Utility/Transport In its utility/personnel transport configuration, the MD 600N cabin features seating for up to five (5) via a 3- passenger front bench and two (2) aft-mounted club seats. The front bench can be installed either forward or aft-facing to ensure optimal passenger comfort. EMS/Air Ambulance When configured for EMS/air ambulance operation, the MD 600N features a single-patient transport Air Ambulance Technologies interior equipped with a state-of-the-art monitor/defibrillator, ventilator, suction unit, and 2x 5L 200 bar Oxygen cylinder, to treat and monitor the patient. Sapura Aero has been an authorized MDHI sales & service representative since 2015. As an authorized sales representative serving the South East Asian countries (ASEAN) of Malaysia, Brunei, Cambodia, East Timor, Indonesia, Laos, Myanmar, Singapore, Thailand, and Vietnam, Sapura Aero offers the full range of MDHI’s commercial helicopter products as well as the optional equipment and accessories to support them. MEDIA ASSETS: A short (0:58) video of the new MD 600N is available here. A selection of high resolution images of this aircraft can be found here. ### About MD Helicopters, Inc. MD Helicopters, Inc. (MDHI), a woman-owned, small business, is a leading manufacturer of commercial, military, law enforcement and air-rescue helicopters. The MDHI family of rotorcraft is world renowned for its value, versatility and performance, and includes the twin-engine MD 902 Explorer, the MD 530F Cayuse Warrior Light Scout Attack Helicopter, the new MD530G Attack helicopter, and a single-engine commercial fleet that includes the MD 600N, MD 520N, MD 500E and MD 530F. The innovative NOTAR® system for anti-torque control with no tail rotor – a key feature of the MD 902, MD 600N and MD 520N – is used exclusively by MD Helicopters to provide safer, quieter performance and confined-area access capability. For more information about MDHI, follow us on Facebook, Twitter, Instagram and LinkedIn, or visit www.mdhelicopters.com. About Sapura Aero SDN BHD Sapura Aero, an Integrated Private Aviation Services Provider, operates out of our home base of Subang (WMSA) and Senai (WMKJ), we operate licensed unscheduled charter, offer aircraft management, ground handling and provide significant number of aircraft parking. We endeavor to deliver an end-to-end private aviation experience by managing the whole business aviation lifecycle. For more information about Sapura Aero, visit http://www.sapura-aero.com. Contact: Amy Romano Director, Marketing & Communications MD Helicopters, Inc. E: [email protected] M: 480.244.3027 D: 480.346.6344 .
Recommended publications
  • Helicopter Noise Reduction Technology, Status Report
    Helicopter Noise Reduction Technology Status Report 21 April 2015 Contributors: ICCAIA: Snecma, Airbus Helicopters, Sikorsky Aircraft, Bell Helicopter, AgustaWestland, Turbomeca, Marenco Swisshelicopter Research Centers: NASA, DLR, ONERA, JAXA 1 Contents 1 Introduction .................................................................................................................................................. 3 2 Helicopter noise sources and related noise generation mechanisms ............................................................ 4 2.1 Rotor noise ........................................................................................................................................... 4 2.2 Anti-torque noise .................................................................................................................................. 4 2.3 Engine noise ......................................................................................................................................... 5 2.3.1 Turboshaft Engines.......................................................................................................................... 5 2.3.2 Piston Engines ................................................................................................................................. 5 2.4 Contribution of noise sources depending on flight condition .............................................................. 5 3 State-of-the-Art Helicopters ........................................................................................................................
    [Show full text]
  • Md 520N Helicopter
    TTEECCHHNNIICCAALL DDEESSCCRRIIPPTTIIOONN MMDD 552200NN HHEELLIICCOOPPTTEERR MD Helicopters, Inc. Marketing and Sales 4555 E. McDowell Rd. Mesa, AZ 85215 480-346-6130 www.mdhelicopters.com [email protected] MISSION PROVEN, CHALLENGE READY THIS PAGE INTENTIONALLY LEFT BLANK TECHNICAL DESCRIPTION MD 520N HELICOPTER MD Helicopters, Inc. 4555 E. McDowell Rd Mesa, Arizona CAGE: 1KVX4 DUNS: 054313767 www.mdhelicopters.com This Technical Description includes information and intellectual property that is the property of MD Helicopters, Inc. (MDHI). It provides general information for evaluation of the design, equipment, and performance of the MD 520N helicopter. The information presented in this Technical Description does not constitute an offer and is subject to change without notice. This proprietary information, in its entirety, shall not be duplicated, used, or disclosed—directly or indirectly, in whole or in part—for any purpose other than for evaluation. MD Helicopters, Inc. reserves the right to revise this Technical Description at any time MD 520N Technical Description REPORT NO.: MD14030410-520NTD NO. OF PAGES: 52 Use or disclosure of data in this Technical Description is subject to the restriction on the cover page of this document. ATTACHMENTS: None Revision By Approved Date Pages and/or Paragraphs Affected New BAH 04-Mar-14 All (Initial Issue) MD 520N Technical Description Contents 1. FOREWORD ........................................................................................................ 1 2. KEY ADVANTAGES AND FEATURES
    [Show full text]
  • Applications
    An invitation to AHS Award Nomination Form Nominations are due by February 26 honor Please nominate online at www.vtol.org/awards-and contests/awards-nomination. innovation and If you are not able to register online, please contact Liz Malleck at (703) 684-6777 x107 excellence for a paper form. in vertical flight technology and its applications The AHS International Awards Program AHS International has a tradition for honoring the vertical flight industry’s most outstanding achievements. Established in 1944, the Society’s Awards Program provides an international showcase for the finest work and research in the industry. Whether it be for a single outstanding contribution or achievement, a major technical innovation, an act of heroism, long and valued service or work that further advances the frontiers of vertical flight technology and its applications, the Society’s awards attract worldwide recognition. Who is eligible for an award? The Society’s Awards recognize achievement at all levels and in all disciplines. Anyone working in the vertical flight industry, anywhere in the world, whether in academia, airframes, engines, systems, the military services, government, research, manufacturing, or in civil and commercial operations or in any other discipline involved in vertical flight is eligible. The Awards Program is structured to recognize individuals at various stages of their careers. Who makes the nominations? he simple answer is you do. You have an important and responsible role to play in identifying those of your colleagues deserving of special T recognition. If there is someone, or a group of persons, you feel is making an outstanding contribution to the world of vertical flight, please read through this brochure, select the appropriate award and make your recommendation.
    [Show full text]
  • Technical Description
    TTEECCHHNNIICCAALL DDEESSCCRRIIPPTTIIOONN MMDD 990022 EEXXPPLLOORREERR MD Helicopters, Inc. Sales and Marketing 4555 E. McDowell Rd. Mesa, AZ 85215 PH: 480.346.6474 FAX: 480.346.6339 www.mdhelicopters.com [email protected] MISSION PROVEN, CHALLENGE READY THIS PAGE INTENTIONALLY LEFT BLANK TECHNICAL DESCRIPTION MD 902 EXPLORER MD Helicopters, Inc. 4555 E. McDowell Rd Mesa, Arizona CAGE: 1KVX4 DUNS: 054313767 www.mdhelicopters.com This Technical Description includes information and intellectual property that is the property of MD Helicopters, Inc. (MDHI). It provides general information for evaluation of the design, equipment, and performance of the MD 902 helicopter. The information presented in this Technical Description does not constitute an offer and is subject to change without notice. This proprietary information, in its entirety, shall not be duplicated, used, or disclosed—directly or indirectly, in whole or in part—for any purpose other than for evaluation. MD Helicopters, Inc. reserves the right to revise this Technical Description at any time MD 902 Explorer Technical Description REPORT NO.: MD14021407-902TD NO. OF PAGES: 74 Use or disclosure of data in this Technical Description is subject to the restriction on the cover page of this document. ATTACHMENTS: None Revision By Approved Date Pages and/or Paragraphs Affected New RCP 14-Feb-14 All (Initial Issue) MD 902 Explorer Technical Description Contents 1. FOREWORD ........................................................................................................ 1
    [Show full text]
  • Military Helicopter Modernization: Background and Issues for Congress
    Order Code RL32447 CRS Report for Congress Received through the CRS Web Military Helicopter Modernization: Background and Issues for Congress June 24, 2004 Christian F. M. Liles Research Associate Foreign Affairs, Defense and Trade Division Christopher Bolkcom Specialist in National Defense Foreign Affairs, Defense and Trade Division Congressional Research Service ˜ The Library of Congress Military Helicopter Modernization: Background and Issues for Congress Summary Recent military operations, particularly those in Afghanistan and Iraq, have brought to the fore a number of outstanding questions concerning helicopters in the U.S. armed forces, including deployability, safety, survivability, affordability, and operational effectiveness. These concerns are especially relevant, and made more complicated, in an age of “military transformation,” the “global war on terrorism,” and increasing pressure to rein in funding for the military, all of which provide contradictory pressures with regard to DOD’s large, and often complicated, military helicopter modernization efforts. Despite these questions, the military use of helicopters is likely to hold even, if not grow. This report includes a discussion of the evolving role of helicopters in military transformation. The Department of Defense (DOD) fields 10 different types of helicopters, which are largely of 1960s and 1970s design. This inventory numbers approximately 5,500 rotary-wing aircraft, not including an additional 144 belonging to the Coast Guard, and ranges from simple “utility” platforms such as the ubiquitous UH-1 “Huey” to highly-advanced, “multi-mission” platforms such as the Air Force’s MH- 53J “Pave Low” special operations helicopter and the still-developmental MV-22B “Osprey” tilt-rotor aircraft. Three general approaches can be taken to modernize DOD’s helicopter forces: upgrading current platforms, rebuilding current helicopter models (often called recapitalization), or procuring new models.
    [Show full text]
  • MD HELICOPTERS SECURES $34 MILLION ARMY CONTRACT Deal
    MD HELICOPTERS SECURES $34 MILLION ARMY CONTRACT Deal provides logistical support for the Afghanistan Air Force MD 530F aircraft fleet Mesa, Ariz., December 3, 2020 – MD Helicopters, Inc. (MDHI) announces an agreement with the U.S. Army worth about $34 million to provide logistics support for the Afghanistan Air Force MD 530F Cayuse Warrior light attack and reconnaissance helicopter fleet. The deal is a continuation of MDHI’s contractor logistics support (CLS) with the U.S. Army and Multi-National Aviation Special Project Office (MASPO) for the fleet. Under the terms of the contract, MDHI will provide maintenance, repairs, updates, and overhauls of the aircraft in Mesa, Arizona, and Kabul, Afghanistan. The estimated completion date for all work is May 31, 2021. “This contract illustrates the Army’s and MASPO’s continued confidence in MD Helicopters’ ability to successfully manage our CLS contract,” says Nick Nenadovic, Vice President of Aftermarket and Customer Support for MD Helicopters, Inc. “We have delivered 60 aircraft to the Afghan Air Force and we maintain a vested interest in ensuring the highest level of support to keep the entire fleet mission ready.” The enhanced MD 530F Cayuse Warrior is a light armed attack helicopter revered for its power, safety, speed, agility, and unparalleled confined area capabilities. The aircraft supports a wide range of training and operational missions, providing safe, efficient multi-mission support with an increased performance profile. About MD Helicopters, Inc. MD Helicopters, Inc. (MDHI), is a leading rotorcraft manufacturer of American Made commercial, military, law enforcement, and air-rescue helicopters. The MDHI family of rotorcraft is world renowned for its value, versatility, and performance.
    [Show full text]
  • 36723669.Pdf
    Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 1994-03 Wind tunnel performance comparative test results of a circular cylinder and 50% ellipse tailboom for circulation control antitorque applications Fisher, David T. Monterey, California. Naval Postgraduate School http://hdl.handle.net/10945/30901 NA VAL POSTGRADUATE SCHOOL Monterey, California THESIS WIND TUNNEL PERFORMANCE COMPARATIVE TEST RESULTS OF A CIRCULAR CYLINDER AND 50% ELLIPSE T AILBOOM FOR CIRCULATION CONTROL ANTITORQUE APPLICATIONS by David T. Fisher March, I994 Th e sis E. Roberts Wood pJPI9585 Thesis Advisor: Approved for public release; distribution is unlimited DUDLEY KNOX LIBRARY NAVAL POSTGRADUATE SCHOOl MONTEREY CA 93943-5101 l,nch.sSlfled <;f(l'RTlYClAS<;lrT('TIO'lOfll-ll'iPAGf REPORT DOCUMENTA TlON PAGE Appro'ved for public release: distribution IS unlimited WIND TlJ}P\,cL PERFORMA!'J"CE COMPARATIVE TEST RESULTS OF A CIRCLLAR CYLINDER A~D 50% ELLIPSE T AILBOOM FOR ClRCULATIO~ CONTROL ANTITORQUE APPLlCATIO?\S by David T. t'isher Lieutenant, unite'll States Kavy 8.s., U.s. Naval Academy. 1985 Submitted in partIal fulfillment of the requirements for the degree of \.1ASTER OF SCIENCE Il'\ AERO:"J"AlITICAL ENGIT\[EERTI\G from the NAY A..L POSTGRADUATE SCHOOL March 1994 Author: DaVid T. Fi~her Approved by: -'•••••• l~----- E. Robens Wood, The~i~ Ad\'i~or Richard M. Howard, Second Reader Department-----~ of Aeronautics and Astronautics ABSTRACT \ hn\ 5p~ed wind tunnel stud) to quantltall\el) e\aluate the perfomMnce (11ft and drag) of a circular cylinder and <:omparable 50'}n e1hpse (;ir(;ulallOn control Ia!lboom mudel \\J~ conducted Circular c:lindel perfonnance was e\aluated <It ~I\lt p051hon~ of scr to 135' measured relati.e to freestream, 50% ellipse perfonnall"e wa~ mea~ur~d for Jngles of attack between ~5' and 3(f Tcsts were conducttd at three blowJnll (:oefficienb.
    [Show full text]
  • Summary of Measurements, Data and Analysis for the MD 600N Helicopter
    DOT-VNTSC-FAA-03-11 Crows Landing Noise Measurement Study: Summary of Measurements, Data and Analysis for the MD 600N Helicopter Clay N. Reherman Christopher J. Roof Gregg G. Fleming David R. Read U.S. Department of Transportation Research and Special Programs Administration John A. Volpe National Transportation Systems Center Environmental Measurement and Modeling Division, DTS-34 Cambridge, MA 02142 May 2004 U.S. Department of Transportation Federal Aviation Administration Notice This document is disseminated under the sponsorship of the Department of Transportation in the interest of information exchange. The United States Government assumes no liability for its contents or use thereof. Notice The United States Government does not endorse products or manufacturers. Trade or manufacturers’ names appear herein solely because they are considered essential to the objective of this report. REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188), Washington, DC 20503. 1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED Letter Report, November 1996 May 2004 4. TITLE AND SUBTITLE 5.
    [Show full text]
  • Linear Modeling of Rotorcraft for Stability Analysis and Preliminary Design
    Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 1993-09 Linear modeling of rotorcraft for stability analysis and preliminary design Wirth, Walter M. Monterey, California. Naval Postgraduate School http://hdl.handle.net/10945/40013 NAVAL POSTGRADUATE SCHOOL Monterey, California AD-A274 869 lSTA|HS,"D A. A oj :SDTIC ELECTE THESIS LINEAR MODELING OF ROTORCRAFT FOR STABILITY ANALYSIS AND PRELIMINARY DESIGN by Walter M. Wirth, Jr. September, 1993 Thesis Advisor: E. Roberts Wood Approved for public release; distribution is unlimited. 94-02079 I1111 iIi 11 Iillll 9lID9 4 1 24 04 6 REPORT DOCUMENTATION PAGE IForm Approved 0MB No. 0704 Public reporting burden for this collection of information is estimated to average I hour per response, including the time for reviewing instruction. searching existing data sources, gathering end maintaining the data meeded. and completing and reviewing the collection of information. Send commnents regarding this burden estimate or any other aspect of this collection of information. including suggestions for reducing this burden, to Washingon headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget. Paperwork Reduction Project (0704-0 198) Washington DC 20503. 1. AGENCY USE ONLY (Leave blank) 12. REPORT DATE 13. REPORT TYPE AND DATES COVERED 11993, September. Master's Thesis 4. TITLE AND SUBTITLE LINEAR MODELING OF ROTORCRAFT 5. FUNDING NUMBERS FOR STABILITY ANALYSIS AND PRELIMINARY DESIGN 6. AUTHOR(S) Walter M. Wirth, Jr. 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING Naval Postgraduate School ORGANIZATION Monterey CA 93943-5000 REPORT NUMBER 9.
    [Show full text]
  • Report to Congress: Nonmilitary Helicopter Urban Noise Study
    REPORT TO Federal Aviation Administration CONGRESS Nonmilitary Helicopter Urban Noise Study ______________________________________________________________________________ Washington, DC 20591 December 2004 Report of the Federal Aviation Administration to the United States Congress Pursuant to Section 747 of the Wendell H. Ford Aviation Investment and Reform Act for the 21stCentury (AIR-21) TABLE OF CONTENTS NONMILITARY HELICOPTER URBAN NOISE STUDY Page 1.0 Executive Summary...........................................................................................................1-1 2.0 Introduction........................................................................................................................2-1 2.1 Mandate..........................................................................................................................2-1 2.2 Background .....................................................................................................................2-2 2.3 FAA Study Process .........................................................................................................2-3 2.4 Report Format .................................................................................................................2-3 3.0 Noise Effects on Individuals..............................................................................................3-1 3.1 Health Effects - Introduction.......................................................................................3-1 3.2 Noise Effects on Communications and
    [Show full text]
  • Open Willcavillafana-Msc.Pdf
    The Pennsylvania State University The Graduate School College of Engineering ROTORCRAFT NOISE ABATEMENT PROCEDURES DEVELOPMENT A Thesis in Aerospace Engineering by Willca Villafana © 2016 Willca Villafana Submitted in Partial Fulfillment of the Requirements for the Degree of Master of Science December 2016 The thesis of Willca Villafana was reviewed and approved∗ by the following: Kenneth S. Brentner Professor of Aerospace Engineering Thesis Advisor Joseph F. Horn Professor of Aerospace Engineering Philip J. Morris Professor of Aerospace Engineering Head of the Department of Aerospace Engineering ∗Signatures are on file in the Graduate School. ii Abstract A rotorcraft noise prediction system has recently been developed as part of a project to develop and evaluate helicopter noise abatement procedures for a range of aircraft. The aim of this thesis is to demonstrate the noise prediction system capabilities and then consider simple noise abatement procedures for three different helicopters of varying technology levels and maximum gross weights. First, the codes that have been assembled into the noise prediction system are described. A brief presentation of acoustic theory on which the noise prediction is based is given as a reminder. Then, the noise prediction system has been validated with the Bell 430 helicopter flying in a level forward flight. The prediction system has also demonstrated its capacity to predict blade vortex interaction (BVI) noise and BVI noise reduction. Finally several abatement procedures have been examined. The two first ones underscored the benefits of flying higher and slower by using the S-76C+ as an example. Then, a S-76C+, Bell 430 and BK 117 helicopters were compared in a level forward flight.
    [Show full text]
  • Hughes Oh-6 Cayuse / Model 500
    HUGHES OH-6 CAYUSE / MODEL 500 OH-6 / MODEL 500 SERVICE Manufacturer: Hughes Tool Co., Aircraft Division, Culver City, California, USA (In 1972, became Hughes Helicopter Division, Summa Corp.) (In 1981, became Hughes Helicopters Inc., Hughes Corp.) (In 1984, became McDonnell Douglas Helicopter Co., McDonnell Douglas Corp., Mesa, Arizona, USA) (In 1997, became Boeing Helicopter Co., The Boeing Co.) (In 1999, became MD Helicopters Inc.) Models: 369; 500 (Renamed Model MD 500 in 1984) Designations: H-6; HO-6 Names: Cayuse, Little Bird First official flight: YOH-6A 27/02/1963 Model 500 13/09/1966 Factory production period: 1962 – present Primary service period: 1966 – present Last official flight: - - OH-6 / MODEL 500 VARIANTS OH-6 Cayuse 1963 Model 369 YOH-6A 10 1965 Model 369A OH-6A 1438 Total: 1448 Model 500 1966 Model 369 Model 500 Series 3215 Total: 3215 Total: 4663 A / MH-6 Little Bird 1981 Model 369D EH-6E 3 1981 Model 369D MH-6E 15 1984 Model MD 500E AH-6F 9 1984 Model MD 500E AH-6G 4 1988 Model MD 530F MH-6H 3 1989 Model MD 530F AH-6J 20 1991 Model MD 530F MH-6J 1 - Model MD 540F AH-6M 0 - Model MD 540F MH-6M 5 Total: 0060 OH-6 / MODEL 500 PRODUCTION OH-6 Cayuse YOH-6A Prototype, single-engined, 4-bladed rotor, observation helicopter for US Army. 4 civil airframes for testing also in army colors. Original designation was YHO-6. produced 1962 – 1964 Hughes Culver City, California (HU) Static Test Airframe 0001 N9696F / N9699F (civil reg.) 0002 / 0005 - N9698F to s/n: 62-12624.
    [Show full text]