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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. -
Comparison of Helicopter Turboshaft Engines
Comparison of Helicopter Turboshaft Engines John Schenderlein1, and Tyler Clayton2 University of Colorado, Boulder, CO, 80304 Although they garnish less attention than their flashy jet cousins, turboshaft engines hold a specialized niche in the aviation industry. Built to be compact, efficient, and powerful, turboshafts have made modern helicopters and the feats they accomplish possible. First implemented in the 1950s, turboshaft geometry has gone largely unchanged, but advances in materials and axial flow technology have continued to drive higher power and efficiency from today's turboshafts. Similarly to the turbojet and fan industry, there are only a handful of big players in the market. The usual suspects - Pratt & Whitney, General Electric, and Rolls-Royce - have taken over most of the industry, but lesser known companies like Lycoming and Turbomeca still hold a footing in the Turboshaft world. Nomenclature shp = Shaft Horsepower SFC = Specific Fuel Consumption FPT = Free Power Turbine HPT = High Power Turbine Introduction & Background Turboshaft engines are very similar to a turboprop engine; in fact many turboshaft engines were created by modifying existing turboprop engines to fit the needs of the rotorcraft they propel. The most common use of turboshaft engines is in scenarios where high power and reliability are required within a small envelope of requirements for size and weight. Most helicopter, marine, and auxiliary power units applications take advantage of turboshaft configurations. In fact, the turboshaft plays a workhorse role in the aviation industry as much as it is does for industrial power generation. While conventional turbine jet propulsion is achieved through thrust generated by a hot and fast exhaust stream, turboshaft engines creates shaft power that drives one or more rotors on the vehicle. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2014. By Aaron M. U. Church, Associate Editor I 2015 USAF Almanac BOMBER AIRCRAFT flight controls actuate trailing edge surfaces that combine aileron, elevator, and rudder functions. New EHF satcom and high-speed computer upgrade B-1 Lancer recently entered full production. Both are part of the Defensive Management Brief: A long-range bomber capable of penetrating enemy defenses and System-Modernization (DMS-M). Efforts are underway to develop a new VLF delivering the largest weapon load of any aircraft in the inventory. receiver for alternative comms. Weapons integration includes the improved COMMENTARY GBU-57 Massive Ordnance Penetrator and JASSM-ER and future weapons The B-1A was initially proposed as replacement for the B-52, and four pro- such as GBU-53 SDB II, GBU-56 Laser JDAM, JDAM-5000, and LRSO. Flex- totypes were developed and tested in 1970s before program cancellation in ible Strike Package mods will feed GPS data to the weapons bays to allow 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft weapons to be guided before release, to thwart jamming. It also will move added 74,000 lb of usable payload, improved radar, and reduced radar cross stores management to a new integrated processor. Phase 2 will allow nuclear section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in and conventional weapons to be carried simultaneously to increase flexibility. Iraq during Desert Fox in December 1998. -
Limits to Principles of Electric Flight
AIRCRAFT DESIGN AND SYSTEMS GROUP (AERO) Limits to Principles of Electric Flight Dieter Scholz Hamburg University of Applied Sciences https://doi.org/10.5281/zenodo.4072283 Deutscher Luft- und Raumfahrtkongress 2019 German Aerospace Congress 2019 Darmstadt, Germany, 30.09. - 02.10.2019 Abstract Purpose – This presentation takes a critical look at various electric air mobility concepts. With a clear focus on requirements and first principles applied to the technologies in question, it tries to bring inflated expectations down to earth. Economic, ecologic and social (noise) based well accepted evaluation principles are set against wishful thinking. Design/methodology/approach – Aeronautical teaching basics are complemented with own thoughts and explanations. In addition, the results of past research and student projects are applied to the topic. Find ings – Electric air mobility may become useful in some areas of aviation. Small short-range general aviation aircraft may benefit from battery-electric or hybrid-electric propulsion. Urban air mobility in large cities will give time advantages to super-rich people, but mass transportation in cities will require a public urban transport system. Battery- electric passenger aircraft are neither economic nor ecologic. How overall advantages can be obtained from turbo- electric distributed propulsion (without batteries) is not clear. Maybe turbo-hydraulic propulsion has some weight advantages over the electric approach. Research limitations/implications – Research findings are from basic considerations only. A detailed evaluation of system principles on a certain aircraft platform may lead to somewhat different results. Practical implications – The discussion about electric air mobility concepts may get more factual. Investors may find some of the information provided easy to understand and helpful for their decision making. -
Military Vehicle Options Arising from the Barrel Type Piston Engine
Journal of Power Technologies 101 (1) (2021) 22–33 Military vehicle options arising from the barrel type piston engine Pawe l Mazuro1 and Cezary Chmielewski1,B 1Warsaw University of Technology B [email protected] Abstract in terms of efficiency, meaning that piston engines can deliver enhanced range and endurance. This is benefi- The article reviews knowledge about requirements for engines in cial in missions requiring a stopover for refueling and state-of-the-art unmanned aerial vehicles and tanks. Analysis of particularly useful for unmanned supply, observation design and operational parameters was carried out on selected and maritime missions. turboshaft and piston engines generating power in the range of 500 - 1500 kW (0.5 - 1.5 MW). The data was compared In contrast, land combat vehicles have significantly with the performance of innovative, barrel type piston engines, different drive unit requirements. High mobility en- which are likely to become an alternative drive solution in the ables the vehicle to rapidly change location after de- target vehicle groups. tection. To this end, the torque curve as a function of the rotational speed of the shaft is of decisive im- portance. Keywords: military UAV, tanks, turboshaft engines, piston engines, barrel type piston engines The complexity of tank engines adds an additional layer of requirements, impacting the reliability and durability of the power unit, and they come with re- 1 Introduction lated manufacturing and operating costs. In military land vehicles, the engine should be as small This article consolidates knowledge on options and as possible; the space saved can be used for other capabilities arising from use of the barrel type piston purposes. -
Annex to ED Decision 2013/024/R 10/09/2013
Annex to ED Decision 2013/024/R 10/09/2013 APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCE 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 type ratings consistent, such information should be first passed on to the Agency via contact us 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 AML licences may be modified at next renewal or when the licence is re-issued, unless there is an urgent reason to modify the licence. Notes on aircraft modified by 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. When an aircraft has been modified by an STC for installation of another engine, the Part-66 type rating of this aircraft may change i.e. from Group 2 to Group 1. This is not reflected in this document. In case the applicant to a licence faces such a case, he/she or his/her competent authority can inform the Agency and a new type rating will be defined by the Agency. -
Manufacturer Air Safety Investigator Contact List DECEMBER 4, 2019
Manufacturer Air Safety Investigator Contact List Alphabetical by company name. Air Tractor Major Product Lines AT-402, AT-502, AT-602, AT-802 (+1) 940-564-5616 (Primary) 24-hr Phone Number (+1) 940-447-1331 (Afterhours) Fax Number (+1) 940-564-5612 Contact Person(s) Kyle Schroeder, Aviation Safety Investigator Electronic Contact [email protected] 1524 Leland Snow Way Address Olney, TX 67374 USA Airbus Helicopters Eurocopter, Aerospatiale, Messerschmitt Bolkow Bloehm, SNIAS, Major Product Lines Sud Aviation Helicopters (+1) 214-605-9365 (Primary) 24-hr Phone Number (+1) 972-641-8090 Contact Person(s) Seth Buttner, Manager, Accident Investigation Electronic Contact [email protected] 2701 Forum Dr. Address Grand Prairie, TX 75052 USA AmSafe, Inc. Major Product Lines Aircraft restraints and airbag systems 24-hr Phone Number (+1) 602-850-2850 James Crupi, Business Development & Technical Support Mgr. (+1) 602-628-0349 Contact Person(s) Lee Langston, Aviation Program Manager (+1) 602-628-0336 [email protected] Electronic Contact [email protected] 1043 N. 47th Ave Address Phoenix, AZ 85043 USA DECEMBER 4, 2019 Page 1 of 12 Manufacturer Air Safety Investigator Contact List Ballistic Recovery Systems, Inc. Major Product Lines Whole-aircraft parachute systems (+1) 763-226-6110 (First Responders) 24-hr Phone Number (+1) 651-457-7491 (Main Line) Fax Number (+1) 651-457-8651 Contact Person(s) Enrique Dillon, President: (+1) (305)777-0174 Direct Line Electronic Contact [email protected] 380 Airport Road Address South St. Paul, -
Lycoming Engine Development, June 1963
VOLUME 1, NU BER 3 JUNE, 1963 B. H. WARREN NOW VICE PRESIDENT, GENERAL MANAGER--------------------------- The appointment of Beverly H. Warren as vice president and general manager of Lycoming Division has been announced by James R. Kerr, president and cbief operating officer of AVCO Corporation. General Warren has been vice president of AVCO's Defense and Industrial Products Group since April, 1961, and director of its Operational Missiles Subdivision since September, 1960. He is a veteran of more than 25 years service with the U.S. Air Force, and retired in 1960 with the rank of Major General. In other organizational changes, General Warren announced the appointment of Dr. Anselm Franz as vice president and general manager, gas turbines, and of Paul A. Deegan as director of administration. Dr. Franz in turn announced that Dr. Heinrich Adenstedt bas been named to the position of vice president, gas turbines operations. LYCOMING SALES DEPARTMENT ACTIVE------------------------------------------- Sales promotion efforts during the Summer will be centered on demonstrations of the Bell 2u4B, commercial version of the Army's Iroquois helicopter, and sales proposals for Lycoming's T55 turboprop and turbofan engines to potential users in Europe, Canada, and the United States. The Bell 204B helicopter is owered by the 1100 shaft horsepower Lycoming T5309 gas turbine engine which differs from the T53-L-9 military engine only in the use of fireproof fuel and oil lines. Two aircraft will make three month demonstration tours, one heading West, the other East. Customers will be invited to demonstrations by the Bell Helicopter egional sales manager in their area, who will be assisted by Bob McCalpin of Lycoming's sales staff. -
CAR Part II Chapter 7 Aircraft Maintenance Engineer Licensing to (Mainly)
NOTICE OF PROPOSED AMENDMENT 2019-01 Issue 01 Date of Issue: 14 April 2019 SUBJECT; CAR PART II CHAPTER 7 – CAR 66 AIRCRAFT MAINTENANCE ENGINEER LICENSING REASON; The GCAA has recently conducted a review of (CAR PART II Chapter 7) as a result of a Consultative Committee outcome (OTTG). The review has concluded that, there is a need to amend CAR Part II Chapter 7 Aircraft Maintenance Engineer Licensing to (mainly): 1. Introduce the category L licence for hot air balloons with its associated basic knowledge and training requirements; 2. further clarify on the examination process and basic knowledge/experience requirements for the issue and validity of a CAR 66 licence. 3. Transfer content of Appendix 1 to CAR 66.70 into CAR 66.50 and CAR 66.70 including the applicable AMC and GM; 4. create an appendix to identify limitations added to a CAR 66 licence and further define the reason and applicability for each limitation and the implications. The proposed initial entry into force date of the amendment is 01 August 2019. The layout and paragraph numbering may change through the NPA process; however the content will remain the same. This notice is published to announce to the public this amendment and to entitle all concerned parties to: 1. Review the attached proposed regulation; and 2. Submit their comments online through the GCAA website within 30 days from the date of this NPA. Comments must be submitted through the GCAA Website – E-Publication – Notice of Proposed Amendment, using the Action of “Submit NPA Feedback Request.” Comments and Responses may be viewed in the Comments Response Document CRD pertaining to this NPA on the GCAA website. -
Annex to ED Decision 2011/003/R 10/05/2011
Annex to ED Decision 2011/003/R 10/05/2011 APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCE Amendment 10 (Corrigendum) 10 May 2011 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 Regulation 1702/2003, this list is only intended for the maintenance purposes. In order to keep this list current and type ratings consistent, such information should be first passed on to the Agency at [email protected] in case a Member State needs to issue a type rating that is not included in this list. Notes: Note 1. For aeroplanes in lists 1 and 2, and helicopters in lists 11, 12 and 13, the table of Appendix I include 3 columns: o column 1: TC holder designation o column 2: aircraft model and, when available, the aircraft commercial designation, o column 3: aircraft designation for endorsement on the Part-66 licence. Only the designations in column 3 should be used for endorsing ratings on Part-66 licences. In the tables of the remaining lists 3 to 10 the TC holder designation is added. Note 2. 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 AML licences may be modified at next renewal or when the licence is re-issued. -
Tm-1-2840-252-23-3
TM 1-2840-252-23-3 TECHNICAL MANUAL AVIATION UNIT AND AVIATION INTERMEDIATE MAINTENANCE MANUAL ENGINE, GAS TURBINE MODEL T55-L-714 NSN 2840-01-353-7635 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. HEADQUARTERS, DEPARTMENT OF THE ARMY 1 DECEMBER 1994 TM 1–2840–252–23–3 CHANGE HEADQUARTERS DEPARTMENT OF THE ARMY NO. 1 WASHINGTON, D.C., 31 January 2003 TECHNICAL MANUAL Aviation Unit and Aviation Intermediate Maintenance Manual ENGINE, GAS TURBINE, MODEL T55–L–714 (NSN 2840–01–353–7635) OZONE DEPLETING CHEMICAL INFORMATION This document has been reviewed for the presence of class I ozone depleting chemicals. As of the basic, dated 1 December 1994, all references to Class I ozone depleting chemicals have been removed from this document by substitution with chemicals by the Engineering, Environment, and Logistics Oversight Office that do not cause atmospheric ozone depletion. DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited TM 1–2840–252–23–3, 1 December 1994, is changed as follows: 1. Remove and insert pages as indicated below. New or changed text material is indicated by a vertical bar in the margin. An illustration change is indicated by a miniature pointing hand. Remove pages Insert pages – – A and B i and ii i and ii A–1 and A–2 A–1 and A–2 C–3 and C–4 C–3 and C–4 C–7 and C–8(blank) C–7 and C–8(blank) G–123 and G–124 G–123 and G–124 Index–3 and Index–4 Index–3 and Index–4 2. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2015. By Aaron M. U. Church, Senior Editor ■ 2016 USAF Almanac BOMBER AIRCRAFT B-1 Lancer Brief: Long-range bomber capable of penetrating enemy defenses and de- livering the largest weapon load of any aircraft in the inventory. COMMENTARY The B-1A was initially proposed as replacement for the B-52, and four proto- types were developed and tested before program cancellation in 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft added 74,000 lb of usable payload, improved radar, and reduced radar cross section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in Iraq during Desert Fox in December 1998. Its three internal weapons bays accommodate a substantial payload of weapons, including a mix of different weapons in each bay. Lancer production totaled 100 aircraft. The bomber’s blended wing/ body configuration, variable-geometry design, and turbofan engines provide long range and loiter time. The B-1B has been upgraded with GPS, smart weapons, and mission systems. Offensive avionics include SAR for tracking, B-2A Spirit (SSgt. Jeremy M. Wilson) targeting, and engaging moving vehicles and terrain following. GPS-aided INS lets aircrews autonomously navigate without ground-based navigation aids Dimensions: Span 137 ft (spread forward) to 79 ft (swept aft), length 146 and precisely engage targets. Sniper pod was added in 2008. The ongoing ft, height 34 ft. integrated battle station modifications is the most comprehensive refresh in Weight: Max T-O 477,000 lb.