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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. -
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). -
Aip Supplement 012/2019 United Kingdom
AIP SUPPLEMENT 012/2019 UNITED KINGDOM Date Of Publication 14 Mar 2019 UK Aeronautical Information Services Notes NATS Swanwick (a) All times are UTC. Room 3115 (b) References are to the UK AIP. Sopwith Way (c) Information, where applicable, Southampton SO31 7AY [email protected] should also be used to amend http://www.ais.org.uk appropriate charts. 07469-441832 (Content - DfT/Aviation Policy Division) 0191-203 2329 (Distribution - Communisis UK) LONDON HEATHROW, LONDON GATWICK AND LONDON STANSTED AIRPORTS NOISE RESTRICTIONS NOTICE 2019 (Published on behalf of the Department for Transport) Whereas: a) By virtue of the Civil Aviation (Designation of Aerodromes) Order 1981(a) Heathrow Airport - London, Gatwick Airport - London and Stansted Airport - London (‘the London Airports’) are designated aerodromes for the purposes of Section 78 of the Civil Aviation Act 1982 (‘the Act’)(b); b) Pursuant to the powers set out in section 78 of the Act, the Secretary of State considers it appropriate, for the purpose of avoiding, limiting or mitigating the effect of noise and vibration connected with the taking-off or landing of aircraft at the London Airports, to prohibit aircraft of specified descriptions from taking off or landing and to limit the number of occasions on which other aircraft may take off or land at those aerodromes during periods specified in this Notice throughout the period specified as the summer season 2019 in this Notice; c) For the purposes of Section 78(4)(a) of the Act, the circumstances under which a particular occasion or series of occasions on which aircraft take off or land at the London Airports will be disregarded for the purposes of this Notice are specified in paragraph 11 of this Notice. -
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 ........................................................................................................................ -
Pzl-10 Turboshaft Engine – System Design Review
Journal of KONES Powertrain and Transport, Vol. 26, No. 1 2019 ISSN: 1231-4005 e-ISSN: 2354-0133 DOI: 10.2478/kones-2019-0003 PZL-10 TURBOSHAFT ENGINE – SYSTEM DESIGN REVIEW Michal Czarnecki Rzeszow University of Technology, Department of Aircraft and Aircraft Engines Powstancow Warszawy Av. 8, 35-959 Rzeszow, Poland tel.: +48 17 8651609, fax: +48 17 8543116 e-mail: [email protected] John Olsen School of Mechanical and Manufacturing Engineering The University of New South Wales, Sydney, Ainsworth Building, N.S.W. 2052, Sydney, Australia tel.: +61 2 9385 5217, fax: +61 2 9663 1222 e-mail: [email protected] Ruixian Ma School of Energy Science and Engineering Harbin Institute of Technology Harbin, 150001, Heilongjiang, China e-mail: [email protected] Abstract The PZL – 10-turboshaft gas turbine engine is straight derivative of GTD-10 turboshaft design by OKMB (Omsk Engine Design Bureau). Prototype engine first run take place in 1968. Selected engine is interested platform to modify due gas generator layout 6A+R-2, which is modern. For example axial compressor design from successful Klimov designs TB2-117 (10A-2-2) or TB3-117 (12A-2-2) become obsolete in favour to TB7-117B (5A+R-2-2). In comparison to competitive engines: Klimov TB3-117 (1974 – Mi-14/17/24), General Electric T-700 (1970 – UH60/AH64), Turbomeca Makila (1976 – H225M) the PZL-10 engine design is limited by asymmetric power turbine design layout. This layout is common to early turboshaft design such as Soloview D-25V (Mil-6 power plant). Presented article review base engine configuration (6A+R+2+1). -
Loss of Control and Collision with Water Involving Eurocopter EC120B, VH
Loss of control and collision with water involving Eurocopter EC120B, VH-WII Hardy Reef, 72 km north-north-east of Hamilton Island Airport, Queensland on 21 March 2018 ATSB Transport Safety Report Aviation Occurrence Investigation (Systemic) AO-2018-026 Final – 16 June 2021 Cover photo: CQ Plane Spotting 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, ACT 2601 Telephone: 1800 020 616, from overseas +61 2 6257 2463 Accident and incident notification: 1800 011 034 (24 hours) Email: [email protected] Website: www.atsb.gov.au © Commonwealth of Australia 2021 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 licence 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. Where you want to use their material you will need to contact them directly. -
The Flying Doctors Aeromedical Transportation Focus
Volume 7 Number 4 August/September 2013 The flying doctors Aeromedical transportation focus EAST SIDE ENERGY STREET STORY SUPPLEMENTS SMARTS Asian market report Powerplant technology Urban flight safety www.rotorhub.com RH_AugSep13_OFC.indd 1 19/08/2013 10:18:30 RH_AugSep13_IFC.indd 2 19/08/2013 10:25:14 ROTORHUB CONTENTS 1 CONTENTS 8 Volume 7 Number 4 August/September 2013 Comment 3 News 4 • Canadian Coast Guard project heads to the courts • EC225 resumes full mission operability worldwide Cover story 13 • Bell Helicopter launches new light single The largest provider of air • Scepticism greets Eurocopter rebranding medical transportation Payloads: Right down the line 39 services in the US HEMS Platform for Industry: A variety of different sensor technologies are now market, Air Methods Methodical approach 8 available to assist helicopter operators carrying out operates around 390 Air medical transportation is a fundamental infrastructure inspection flights for utility companies. helicopters across 45 states. element of a country’s comprehensive healthcare RotorHub weighs up the options. (Photo: Air Methods) infrastructure. Aaron Todd, CEO of Air Methods, 13 talks to RotorHub about how his company is Type Focus: Eurocopter AS332 46 providing both widespread and reliable services in Despite more advanced platforms at a similar this hectic sector. size being available – even from the same manufacturer – the AS332 Super Puma is still EMS: On a role 13 holding its own. RotorHub charts its history and HEMS has become big business for operators and considers its place in the current market. airframers alike. RotorHub looks at some of the latest offerings in terms of platforms and mission Urban flying: Street smarts 51 31 equipment. -
CRD) to Notice of Proposed Amendment (NPA) 03-2006
Comment Response Document (CRD) to Notice of Proposed Amendment (NPA) 03-2006 for amending the Executive Director Decision No. 2005/07/R of 19 December 2005 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 of 20 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 APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCE CRD to NPA 03/2006 Explanatory Note I. General 1. The purpose of the Notice of Proposed Amendment (NPA) 03/2006, dated 20 April 2006 was to propose an amendment to Decision N° 2005/07/R of the Executive Director of the Agency of 19 December 2005 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 of 20 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 (ED Decision 2005/07/R). II. Consultation 2. The draft Executive Director Decision (ED Decision) amending ED Decision 2005/07/R was published on the web site (www.easa.europa.eu) on 21 April 2006. By the closing date of 2 June 2006, European Aviation Safety Agency (the Agency) had received 107 comments from 20 National Aviation Authorities, professional organisations and private companies. III. Publication of the CRD 3. All comments received have been acknowledged and incorporated into a Comment Response Document (CRD). This CRD contains a list of all persons and/or organisations that have provided comments and the answers of the Agency. -
Proposed Rules Federal Register Vol
1946 Proposed Rules Federal Register Vol. 72, No. 10 Wednesday, January 17, 2007 This section of the FEDERAL REGISTER Seventh Street, SW., Nassif Building, between 9 a.m. and 5 p.m., Monday contains notices to the public of the proposed Room PL–401, Washington, DC 20590– through Friday, except Federal holidays. issuance of rules and regulations. The 0001. The Docket Office (telephone (800) 647– purpose of these notices is to give interested • Fax: (202) 493–2251. 5227) is located on the plaza level of the persons an opportunity to participate in the • Hand Delivery: Room PL–401 on Department of Transportation Nassif rule making prior to the adoption of the final rules. the plaza level of the Nassif Building, Building at the street address stated in 400 Seventh Street, SW., Washington, ADDRESSES. Comments will be available DC, between 9 a.m. and 5 p.m., Monday in the AD docket shortly after the DEPARTMENT OF TRANSPORTATION through Friday, except Federal holidays. Docket Management Facility receives You may examine the comments on them. this proposed AD in the AD docket on Federal Aviation Administration Discussion the Internet at http://dms.dot.gov. 14 CFR Part 39 FOR FURTHER INFORMATION CONTACT: Tara GE released version 5.10 software for Chaidez, Aerospace Engineer, Engine FADECs installed in CF34–10E series [Docket No. FAA–2006–26585; Directorate turbofan engines. The software was Identifier 2006–NE–44–AD] Certification Office, FAA, Engine & Propeller Directorate, 12 New England released to change the engine’s High RIN 2120–AA64 Executive Park, Burlington, MA 01803; Pressure Turbine Active Clearance telephone (781) 238–7773; fax (781) Control. -
Study on Effects of Combustible Gas on Helicopter Operations
Aviation Safety Support Services for the Bureau of Safety and Environmental Enforcement Task C.4.5: Study on Effects of Combustible Gas on Helicopter Operations August 31, 2015 Aviation Safety Support Services for BSEE Task C.4.5: Study on Effects of Combustible Gas on Helicopter Operations Table of Contents Abbreviations and Acronyms .................................................................................... 4 1. Introduction....................................................................................................... 6 1.1 Other Mishaps Consistent With APG Ingestion .............................................................7 2. Analysis ...........................................................................................................12 2.1 Subtask C.4.5.1 – review and assess helideck construction standards .........................12 2.2 Subtask C.4.5.2 (a) – conduct technical analysis ..........................................................32 2.3 Subtask C.4.5.2 (b) – identify and list each helicopter (make, model, and engine) used on OCS facilities under BSEE jurisdiction. ..........................................................34 2.4 Subtask C.4.5.2 (c) – (1) determine the vapor density for each flammable gas (lighter or heavier than air) to determine how the placement of vents would affect helicopter operations; and (2) determine the flammability limits for each flammable gas to determine the effect on helicopter operations...................................35 2.5 Subtask C.4.5.2 (d) – (1) determine -
HAI PUBLICATIONS Convention News
DAY 2 March 6, 2019 HAI PUBLICATIONS Convention News Heli-Expo attendees crowded the Kopter booth on the show’s opening day as CEO Andreas Löwenstein revealed the company’s plan to build new SH09 helicopters for the U.S. market at a former Bell facility in Lafayette, Louisiana. The single-engine SH09 is near design freeze, and certification is planned in 2020. Löwenstein expects more than 50 percent of sales to be in the U.S., and plans call for another factory in Asia to serve those markets. MARIANO ROSALES Industry Pre-owned sales on Kopter lands in Bayou State the rise › page 24 by Curt Epstein OEMs Swiss OEM Kopter selected Lafayette, Loui- The state initially funded construction proceeding, according to Don Pierson, Lou- Airbus snags major siana, as the location for its U.S. production of the $25.3 million facility, which occupies isiana’s economic development secretary. medevac order › page 3 and service facility, company CEO Andreas nearly 15 acres at Lafayette Regional Air- “We have here a turnkey solution,” said Löwenstein and Louisiana Gov. John Bel port/Paul Fournet Field. While the lease on Löwenstein. “It’s a facility that has been Edwards (D) jointly announced yester- the facility was clear for reassignment, lit- built to assemble and deliver helicopters.” Technology day morning at Heli-Expo 2019. Kopter is igation against the former occupant is still continues on page 30 ASU designs, builds preparing to freeze the design on its large- cabin, single engine SH09 helicopter ahead own NVGs › page 20 of anticipated certification in the second quarter of 2020. -
Annex to Decision 2015/020/R
Annex to ED Decision 2015/020/R The text of the amendment is arranged to show deleted, new or amended text as shown below: — deleted text is marked with strike through; — new or amended text is highlighted in grey; and — an ellipsis (…) indicates that the remaining text is unchanged in front of or following the reflected amendment. Appendix I to Annex IV to ED Decision 2003/019/RM is hereby amended as follows: APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCES The following aircraft type ratings should be used to ensure a common standard throughout the Member States. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under the Basic Regulation and its Implementing Rules,; this list is only intended for the maintenance purposes. In order to keep this list current and the type ratings consistent, such information should be first passed on to the Agency using the Rulemaking Enquiry form (http://easa.europa.eu/webgate/rulemaking-enquiry/) in case a Member State needs to issue a type rating that is not included in this list. Notes on when the licences should be modified: When a modification is introduced by this Decision to an aircraft type rating or to an engine designation in the rating which affect licences already issued, the ratings on the Aircraft Maintenance Licences (AMLs) may be modified at the next renewal or when the licence is reissued, unless there is an urgent reason to modify the licence. Notes on aircraft modified by Supplemental Type Certificate (STC): It is not the intention of this document to include all aircraft modified by STCs because a great number of STCs were approved before 2003 and are unknown to the Agency.