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Aircraft Accident Investigation Preliminary Accident Report 5Y-KDL 03.03.2019
MINISTRY OF TRANSPORT, INFRASTRUCTURE, HOUSING, URBAN DEVELOPMENT AND PUBLIC WORKS STATE DEPARTMENT FOR TRANSPORT Aircraft Accident Investigation Preliminary Accident Report 5Y-KDL 03.03.2019 BELL 505 CENTRAL ISLAND NATIONAL PARK, TURKANA March 11, 2019 PRELIMINARY REPORT SUMMARY OPERATOR : Kwae Island Development Limited AIRCRAFT TYPE : Bell 505 MANUFACTURER : Bell Helicopter Canada Ltd. YEAR OF MANUFACTURE : 2013 i AIRCRAFT REGISTRATION : 5Y-KDL AIRCRAFT SERIAL NUMBER : 65037 DATE OF REGISTRATION : 18 July 2018 NUMBER AND TYPE OF ENGINE : One Turbomeca Arrius 2R Turboshaft DATE OF OCCURRENCE : 3 March 2019 LAST POINT OF DEPARTURE : Turkana Central Island (3°30′06″N 36°02′26″E) POINT OF INTENDED LANDING : Lobollo Camp TIME OF OCCURRENCE : 2035 hours Local Time (LT) LOCATION OF OCCURRENCE : Central Island National Park Turkana TYPE OF FLIGHT : Commercial (Passenger) PHASE OF FLIGHT : Take-off NUMBER OF PERSONS ON BOARD : Five (5) INJURIES : Fatal (5) NATURE OF DAMAGE : Aircraft destroyed CLASS OF OCCURRENCE : Accident PILOT IN COMMAND : YK-4964-AL PIC’s FLYING EXPERIENCE : 5500 hours All times given in this report are East African Local Time (UTC +3) OBJECTIVE This preliminary report contains factual information which has been determined up to the time of publication. The information in this report is published to inform the aviation industry and the public of the general circumstances of the accident. ii This investigation has been carried out in accordance with The Kenya Civil Aviation (Aircraft Accident and Incident Investigation) Regulations, 2018 and Annex 13 to the ICAO Convention on International Civil Aviation. The sole objective of the investigation of an accident or incident under these Regulations shall be the prevention of accidents and incidents. -
1.1.3 Helicopters
Information on the Company’s Activities / 1.1 Presentation of the Company 1.1.3 Helicopters Airbus Helicopters is a global leader in the civil and military The HIL programme, for which the Airbus Helicopters’ H160 rotorcraft market, offering one of the most complete and modern was selected in 2017, was initially scheduled for launch range of helicopters and related services. This product range in 2022 by the current military budget law. Launching the currently includes light single-engine, light twin-engine, medium programme earlier will enable delivery of the fi rst H160Ms to and medium-heavy rotorcraft, which are adaptable to all kinds of the French Armed Forces to be advanced to 2026. The H160 mission types based on customer needs. See “— 1.1.1 Overview” was designed to be a modular helicopter, enabling its military for an introduction to Airbus Helicopters. version, with a single platform, to perform missions ranging from commando infi ltration to air intercept, fi re support, and anti-ship warfare in order to meet the needs of the army, the Strategy navy and the air force through the HIL programme. The new fi ve-bladed H145 is on track for EASA and FAA Business Ambition certifi cation in 2020. To ensure these certifi cations, two fi ve- bladed prototypes have clocked more than 400 fl ight hours Airbus Helicopters continues to execute its ambition to lead the in extensive fl ight test campaigns in Germany, France, Spain, helicopter market, build end-to-end solutions and grow new Finland, and in South America. First deliveries of the new H145 VTOL businesses, while being fi nancially sound. -
H1 2019 Results
AEROSTRUCTURES & INTERCONNECTION SYSTEMS H1 2019 RESULTS SEPTEMBER 4, 2019 DISCLAIMER Certain statements contained in this document are forward-looking statements. These statements includes, without limitation, statements that are predictions of or indicate future events, trends, plans, expectations or objectives. Examples of forward-looking statements include statements relating to business strategy, objectives, delivery schedules or future performance. Words such as “anticipates”, “believes”, “estimates”, “seeks”, “intends”, “may” and similar expressions are used to identify these forward-looking statements. Such statements are, by their nature, subject to known and unknown risks and uncertainties. These uncertainties may cause our actual future results to be materially different than those expressed in our forward-looking statements as these are dependent on risk factors such as the variation of the exchange rates, program delays, industrial risks relating to safety, the evolution of regulations and the general economic and financial conditions and other matters of national, regional and global scale, including those of a political, economic, competitive and regulatory nature. Please refer to the section “Risks management” of the latest Latécoère’s Annual Report, for a description of certain important factors, risks and uncertainties that may affect Latécoère’s business. Latécoère makes no commitment to update or revise any of these forward-looking statements, whether to reflect new information, future events or circumstances or otherwise. This document is the property of Latécoère. It can not be disclosed or reproduced, even partially, without authorization. 2 H1 2019 HIGHLIGHTS 80% €372M 60/40% €28M TRANSFORMATION REVENUE AEROSTRUCTURES/ Rec. EBITDA 2020 TARGETED INTERCONNECTION SYSTEMS SAVINGS This document is the property of Latécoère. -
Decision 2005/07/R
DECISION No 2005/07/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 19-12-2005 amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to Regulation (EC) No 1592/2002 of 15 July 2002 on common rules in the field of civil aviation (hereinafter referred to as the Basic Regulation) and establishing a European Aviation Safety Agency1 (hereinafter referred to as the “Agency”), and in particular Articles 13 and 14 thereof. Having regard to the Commission Regulation (EC) No 2042/2003 of 28 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.2 Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part-66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered as a permanent rulemaking task for the Agency. This decision represents the first update according to an accelerated procedure accepted by AGNA and SSCC. -
Md Helicopters Md Explorer Twin-Engined Light Helicopter, Usa
MD HELICOPTERS MD EXPLORER TWIN-ENGINED LIGHT HELICOPTER, USA The MD Explorer twin-engined light helicopter entered service in 1994 and is in service with private and corporate customers, law enforcement agencies and emergency services around the world. It is manufactured by MD Helicopters Inc of Mesa, Arizona, a subsidiary of the Netherlands-based MD Helicopters of the RDM Group. The company acquired the business rights of the former McDonnell Douglas Helicopters from Boeing in February 1999, excluding that of the AH-64 Apache helicopter which remains within Boeing's business interest. As well as the Explorer, MD Helicopters' products include the MD 500, 520N, 530F and the 600N. In August 2005, Patriarch Partners of New York bought a controlling interest in MD Helicopters from RDM. Over 100 MD Explorers have been delivered. The Explorer is in service with law enforcement agencies, including the US Coast Guard, US Drug Enforcement Agency, Rijkswacht and the Gendarmerie in Belgium, German State Police, Dutch National Police, the Mexican Navy and UK Police Aviation Services. The helicopter can be fitted with a selection of federal or military systems, e.g. forward looking infrared (FLIR) observation system. HELLFIRE GUIDED MISSILE AND GUN-MOUNTED DESIGN The MD Combat Explorer can be armed with 70mm rocket pod, GAU-19/A 0.50 calibre Gatling gun, M-134 7.62mm miniguns, Hellfire laser-guided missiles and Rafael N-TD dual-operation missiles. For the US Coast Guard the helicopter carries the designation MH-90 Enforcer and is armed with an M240 7.62mm gun pintle mounted at the side door. -
Save a Turbine Engine: Serve It Water
Clare Leavens Award Joe Chase Award Aviall High Achievement Award Transport Canada Approved for R/T Save a turbine engine: serve it water Minimum equipment lists and dispatch deviation guides PAMA and AME news February -March 2015 Volume 13/Issue 5 Publication Mail Agreement No. 0041039024 and Return Undeliverable Canadian Addresses to Alpha Publishing Group (2004) Inc. Unit 7, 11771 Horseshoe Way, Richmond, BC, V7A 4V4 email: [email protected] $7.95 AMU-OFC-IFC.indd 1 1/29/15 7:28 PM AMU-OFC-IFC.indd 2 1/29/15 7:28 PM In perspective: Departments the P&WC PT6 nd here some of you thought Gran- 4 Upcoming Events dad put a lot of miles and years on his good ol’ Harley Flathead 45. Hah! 6 STCs & New Products AThat was nothing. Pratt & Whitney Canada 8 Industry Forum recently tweeted out that its venerable PT6 turbine has now clocked 400 million hours 20 AME Association of flight operation. and PAMA News Four hundred million! What does that 39 Classified even mean? Let’s calculate (roughly): There are 8,760 hours in any 365-day year. Di- 42 AMU Chronicles vide 400 million by 8,760 and you get By Sam Longo 45,662.100456621. Round that number off — without fac- toring in Leap, Aztec or dog years (this is al- Features ready getting too complicated for my lousy math)—and you’re now standing at 46,000 10 subscribe and download at www.amumagazine.com AMU is viewable online: years of service. Did I just do that right? As- Save a Turbine Engine: Serve it Water 10 suming I did (and that’s a big ask, I know) By Mike Broderick then we can break down that history into bite-sized pieces. -
In-Flight Break-Up Involving Robinson R44, VH-ZNZ, 41 Km NW Mossman
In-flightInsert document break-up involving title Robinson R44, VH-ZNZ Location41 km NW | Date Mossman, Queensland | 18 November 2016 ATSB Transport Safety Report Investigation [InsertAviation Mode] Occurrence Occurrence Investigation Investigation XX-YYYY-####AO-2016-156 Final – 5 March 2019 Cover photo: Ian McDonell Released in accordance with section 25 of the Transport Safety Investigation Act 2003 Publishing information Published by: Australian Transport Safety Bureau Postal address: PO Box 967, Civic Square ACT 2608 Office: 62 Northbourne Avenue Canberra, Australian Capital Territory 2601 Telephone: 1800 020 616, from overseas +61 2 6257 4150 (24 hours) Accident and incident notification: 1800 011 034 (24 hours) Facsimile: 02 6247 3117, from overseas +61 2 6247 3117 Email: [email protected] Internet: www.atsb.gov.au © Commonwealth of Australia 2019 Ownership of intellectual property rights in this publication Unless otherwise noted, copyright (and any other intellectual property rights, if any) in this publication is owned by the Commonwealth of Australia. Creative Commons licence With the exception of the Coat of Arms, ATSB logo, and photos and graphics in which a third party holds copyright, this publication is licensed under a Creative Commons Attribution 3.0 Australia licence. Creative Commons Attribution 3.0 Australia Licence is a standard form license agreement that allows you to copy, distribute, transmit and adapt this publication provided that you attribute the work. The ATSB’s preference is that you attribute this publication (and any material sourced from it) using the following wording: Source: Australian Transport Safety Bureau Copyright in material obtained from other agencies, private individuals or organisations, belongs to those agencies, individuals or organisations. -
We Find Igor Sikorsky III in Northern Maine
GETAWAYS | SIKORSKY WEEKEND | Summer camp We find Igor Sikorsky III in northern Maine BY JULIE SUMMERS WALKER PHOTOGRAPHY BY CHRIS ROSE 78 | AOPA PILOT March 2016 www.aopa.org/pilot AOPA PILOT | 79 IGOR SIKORSKY III sits on the dock at Bradford Camps on Munsungan Lake in northern Maine. That’s his 1968 Cessna 172 on floats behind him (right). Visitors relax on Adirondack chairs overlooking the lake (below). eep in the woods of Maine, the grandson of one of the most loving man who led a charmed life. During his fireside talks in the influential aircraft designers hosts “Sikorsky Weekend” sporting camp lodge, with a massive moose head and equally massive each year, telling tales of his grandfather, Russia before the deer head overlooking the room, the entertaining younger Sikorsky DBolshevik revolution, and the early days of helicopter design—and shares his grandfather’s years in Russia, the construction of the four- taking visitors seaplane flying and fishing. Meet Igor Sikorsky III. engine Le Grand for the czar, his early years in the United States as a Sikorsky and his wife, Karen, run the 100-year-old Bradford nearly penniless immigrant with big ideas, the Pan Am flying boats, Camps on the shores of Munsungan Lake, a four-mile-long body of and life as a test pilot building helicopters for United Aircraft (later pristine water that is home to trout, salmon, and perch. Bradford is United Technologies). Rich with original photographs, drawings, a traditional sporting camp, with eight waterfront log cabins—the and correspondence, the experience is truly a taste of history. -
Rotorcraft (2011)
Rotorcraft Overview The rotorcraft industry produces aircraft, powered by either turboshaft or reciprocating engines, capable of performing vertical take-off and landing (VTOL) operations. The rotorcraft sector includes helicopters, gyrocopters, and tiltrotor aircraft. Helicopters, which employ a horizontal rotor for both lift and propulsion, are the mainstay of the industry. Gyrocopters are produced in much smaller quantities, primarily for use in recreational flying. Tiltrotor aircraft, such as the V-22 Osprey1, can take off vertically and then fly horizontally as a fixed-wing aircraft. Rotorcraft are manufactured in most industrialized countries, based on indigenous design or in collaboration with, or under license from, other manufacturers. Manufacturers in the United States of civilian helicopters include American Eurocopter, Bell, Enstrom, Kaman, MD Helicopters, Robinson, Schweizer (now a subsidiary of Sikorsky), and Sikorsky. Bell moved its civilian helicopter production to Canada, with the last U.S. product completed in 1993.2 American Eurocopter—a subsidiary of the European manufacturer and subsidiary of EADS NV—has manufacturing and assembly facilities in Grand Prairie, Texas and Columbus, Missouri. European producers include AgustaWestland, Eurocopter, NHIndustries, and PZL Swidnik. Russian manufacturers including Mil Moscow, Kamov and Kazan helicopters, as well as a number of other rotorcraft related companies, have been consolidated under the Russian government majority-owned OAO OPK Oboronprom.3 (See this report’s Russia -
Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor
Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems تحليل اﻹلتواء الديناميكي ﻷنظمة الحركة في المروحية العمودية )Schweizer 300C( by HAITHAM KHAMIS MOHAMMED AL-SAEEDI Dissertation submitted in fulfilment of the requirements for the degree of MSc SYSTEMS ENGINEERING at The British University in Dubai January 2019 DECLARATION I warrant that the content of this research is the direct result of my own work and that any use made in it of published or unpublished copyright material falls within the limits permitted by international copyright conventions. I understand that a copy of my research will be deposited in the University Library for permanent retention. I hereby agree that the material mentioned above for which I am author and copyright holder may be copied and distributed by The British University in Dubai for the purposes of research, private study or education and that The British University in Dubai may recover from purchasers the costs incurred in such copying and distribution, where appropriate. I understand that The British University in Dubai may make a digital copy available in the institutional repository. I understand that I may apply to the University to retain the right to withhold or to restrict access to my thesis for a period which shall not normally exceed four calendar years from the congregation at which the degree is conferred, the length of the period to be specified in the application, together with the precise reasons for making that application. ___________________ Signature of the student COPYRIGHT AND INFORMATION TO USERS The author whose copyright is declared on the title page of the work has granted to the British University in Dubai the right to lend his/her research work to users of its library and to make partial or single copies for educational and research use. -
Over Thirty Years After the Wright Brothers
ver thirty years after the Wright Brothers absolutely right in terms of a so-called “pure” helicop- attained powered, heavier-than-air, fixed-wing ter. However, the quest for speed in rotary-wing flight Oflight in the United States, Germany astounded drove designers to consider another option: the com- the world in 1936 with demonstrations of the vertical pound helicopter. flight capabilities of the side-by-side rotor Focke Fw 61, The definition of a “compound helicopter” is open to which eclipsed all previous attempts at controlled verti- debate (see sidebar). Although many contend that aug- cal flight. However, even its overall performance was mented forward propulsion is all that is necessary to modest, particularly with regards to forward speed. Even place a helicopter in the “compound” category, others after Igor Sikorsky perfected the now-classic configura- insist that it need only possess some form of augment- tion of a large single main rotor and a smaller anti- ed lift, or that it must have both. Focusing on what torque tail rotor a few years later, speed was still limited could be called “propulsive compounds,” the following in comparison to that of the helicopter’s fixed-wing pages provide a broad overview of the different helicop- brethren. Although Sikorsky’s basic design withstood ters that have been flown over the years with some sort the test of time and became the dominant helicopter of auxiliary propulsion unit: one or more propellers or configuration worldwide (approximately 95% today), jet engines. This survey also gives a brief look at the all helicopters currently in service suffer from one pri- ways in which different manufacturers have chosen to mary limitation: the inability to achieve forward speeds approach the problem of increased forward speed while much greater than 200 kt (230 mph). -
Robinson Helicopters: Mast Bumping Accidents in NZ
Watchlist Robinson helicopters: mast bumping accidents in NZ What is the problem? rotor systems, as used on Robinson helicopters, are particularly susceptible to mast bumping in ‘low-G’ conditions. Low-G The Transport Accident Investigation can be caused by large or abrupt flight Commission is concerned about the number control inputs or by turbulence. The risk of of accidents in New Zealand in which mast bumping in turbulence increases with Robinson helicopters have experienced ‘mast high power settings and operating at high bumping’. These accidents have raised speed and light weight. concerns about the risks of flying these helicopters in the mountainous terrain and What is the solution? weather conditions that are common in New Zealand. Operators must select a type of aircraft Mast bumping is contact between an inner suited to the risk profile of the intended use. part of a main rotor blade or a rotor hub and Similarly, all pilots must understand the the main rotor drive shaft (or ‘mast’). Serious helicopter’s operating limitations, avoid mast bumping in flight usually results in the circumstances which could see these helicopter breaking up in flight, which is fatal inadvertently exceeded, and receive proper for those on board. training in the causes, dangers, and prevention of mast bumping, including in low- Part of the problem is that the available G conditions. It is particularly important for evidence has not allowed the circumstances Robinson pilots to be aware of the risks of and causes of all of these ‘mast bumping’ flying a lightly loaded helicopter at high speed accidents to be fully determined.