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Taurus Manual ENG 250Special.Indd
Flight manual and Maintenance manual applies to Taurus 503 equipped with Rotax 503 engine REV. 0 (21 June, 2006) This is the original manual of Pipistrel d.o.o. Ajdovščina Should third-party translations to other languages contain any discreptancies, Pipistrel d.o.o. Ajdovščina denies all responsibility. WARNING! This booklet MUST be present inside the cockpit at all times! Should you be selling the aircraft make sure this manual is handed over to the new owner. 2 TAURUS motorglider www.pipistrel.si REV. 0 Taurus model: Factory serial number: Date of manufacture: Aircraft empty weight (kg): Available crew weight (no front ballast): Available crew weight (9 kg front ballast): Available luggage weight: List of equipment included in aircraft empty weight: Date and place of issue: Ajdovščina, www.pipistrel.si TAURUS motorglider 3 REV. 0 Pipistrel d.o.o. Ajdovščina, Goriška cesta 50a, SI-5270 Ajdovščina, Slovenija tel: +386 (0)5 3663 873, fax: +386 (0)5 3661 263, e-mail: [email protected] www.pipistrel.si Flight manual and Maintenance manual for Taurus motorglider Model: Taurus 503 (Rotax 503) Slovenian Data Sheet number: TC 02/001 - AT/ULN 04 Factory serial number: Registration number: Date of Issue: June, 2006 Pages signed under “Approval” in section Index of revisions and List of valid pages (pages 4 and 5 of this manual) are approved by: Authority: Signature: Stamp: Original date of Approval: This aircraft is to be operated in compliance with information and limitations contained herein. The original English Language edition of this manual has been approved as operating instruction according to “Pravilnik o ultralahkih letalnih napravah” of Republic of Slovenia. -
Aero Ae 45 & Ae
This production list is presented to you by the editorial team of "Soviet Transports" - current to the beginning of January 2021. Additions and corrections are welcome at [email protected] Aero Ae 45 & Ae 145 181 Ae 45 built by Aero at Prague-Vysocany from 1947 to 1951 The c/n consisted of the year of manufacture and a sequential number. 1 OK-BCA Ae 45 Aero f/f 21jul47 the first prototype; rgd 11sep47; underwent trials with the SVZÚ sep47 OK-BCA Ae 45 Ministers. dopravy trf unknown Ministry of Transport OK-BCA Ae 45 CSA trf unknown canx 1953 2 OK-CCA Ae 45 Aero rgd 09apr48 the second prototype; f/f 12mar48 OK-CCA Ae 45 Celulozka Bratisl. trf unknown Celulozka Bratislava; canx 1958 not known Ae 45 Czechoslovak AF trf unknown 49 003 G-007 (1) Ae 45 Hungarian AF d/d 15may49 HA-AEB Ae 45 MÉM Rep. Szolgálat trf 06apr52 Hungarian Flying Association; damaged 29apr52 when the landing gear broke HA-AEB Ae 45 OMSZ trf 18jun57 Hungarian Air Ambulance; w/o (or canx ?) 22nov62 49 004 OK-DCB Ae 45 rgd 21apr49 canx to Italy I-CRES Ae 45 Aero Club Milano rgd 18jul59 Aero Club Milano of Linate; owner also reported as Franco Rol; based at Torino; canx 1970 F-GFYA Ae 45 Pierre Cavassilas res aug88 Pierre Cavassilas of Chavenay; possibly never fully registered F-AZJX Ae 45 Pierre Cavassilas rgd 08jul94 seen Chavenay 20may94 with a 'W' taped over the 'A' of the registration; still current in 2007; under restoration near Paris in 2008; was to be reflown jan09; seen Compiègne 19jun09 and 27jun09 in all-grey c/s with large blue registration, in great condition; seen Soissons-Courmelles 28may12 with smaller black registration; l/n Compiègne 15jun13, active 49 005 OK-DCA Ae 45 rgd 23apr49 I-AERA Ae 45 Luigi Leone rgd 11oct61 based at Torino 49 006 HB-EKF Ae 45 Mr. -
Thatcherism Czech Style
TITLE : Thatcherism, Czech Style : Organized Labor and the Transition to Capitalism in the Czech Republic AUTHOR: Peter Rutland Wesleyan University THE NATIONAL COUNCI L FOR SOVIET AND EAST EUROPEA N RESEARC H 1755 Massachusetts Avenue, N .W . Washington, D .C . 20036 INFORMATIONPROJECT :* CONTRACTOR : Brown University PRINCIPAL INVESTIGATOR : Linda J . Coo k COUNCIL CONTRACT NUMBER : 807-24 DATE : April 30, 199 3 COPYRIGHT INFORMATION Individual researchers retain the copyright on work products derived from research funded b y Council Contract. The Council and the U.S. Government have the right to duplicate written reports and other materials submitted under Council Contract and to distribute such copies within th e Council and U.S. Government for their own use, and to draw upon such reports and materials for their own studies; but the Council and U.S. Government do not have the right to distribute, o r make such reports and materials available outside the Council or U.S. Government without th e written consent of the authors, except as may be required under the provisions of the Freedom o f Information Act 5 U.S.C. 552, or other applicable law . The work leading to this report was supported by contract funds provided by the National Council fo r Soviet and East European Research . The analysis and interpretations contained in the report are those of th e author. CONTENT S Executive Summary i Roots i i The Political Consolidation of the Market Reformers i i The Economic Reform Program iii The Role of Labor Unions in the Transition t o -
TŘICÁTÁ LÉTA – ZLATÝ VĚK Třicátá Léta – Zlatý Věk
TŘICÁTÁ LÉTA – ZLATÝ VĚK Třicátá léta – zlatý věk Světová hospodářská krize, která vypukla v roce prací přidělovalo jednotlivým aeroklubům. Kromě 1929, se v negativním smyslu slova podepsala tradičních výrobců letadel Aero, Avia a Letov zamě- i na rozvoji našeho sportovního letectví. Průmys- řených spíše na státní a zejména vojenské zakázky lová výroba prudce klesala, v roce 1933 až na 60 % se výrobou sportovních letadel začaly zabývat firma úrovně dosažené v roce 1929, a úměrně s klesající Baťa v Otrokovicích, kopřivnická Tatra, leteckou průmyslovou produkcí rostla nezaměstnanost, která výrobu v koncernu ČKD takřka v hodině dvanácté v roce 1934 dosáhla více než 17 %. Tato situace se zachraňuje slavná Praga E 114 Air Baby a 1. dubna pochopitelně odrazila i poklesem aktivity v oblasti roku 1935 je založena firma Ing. Pavel Beneš, Ing. J. sportovního letectví. Ve výrobních programech Mráz, továrna na letadla v Chocni. Kromě sportov- našich leteckých továren nebylo pro sportovní leta- ních letadel vzniká celá řada projektů tzv. lidových dla místo, ostatně nebyl nikdo, kdo by je kupoval, letadel. Druhá polovina třicátých let minulého století a tak byl výrobní program orientován až na výjimky by se skutečně mohla nazvat zlatým věkem v historii na zakázky určené pro Ministerstvo národní obrany. našeho letectví. V aeroklubech si museli letečtí nadšenci vystačit s letitými „Branďáky“ – Aero A-1, A-15 a A-26, pří- padně „Sardinkami“ Letov Š-10. Pokud se aeroklubu Letov Š-25 1930 anebo i jednotlivým soukromníkům podařilo získat Cvičný, pokračovací výcvik – prototyp z armády vyřazené Letovy Š-18, Š-118, Š-218 nebo Avii BH-9, BH-10, BH-11, dalo se mluvit o velkém Na základě soutěže, kte- Technická data štěstí a možnosti létat s moderním letadlem umožňu- rou v roce 1931 vypsalo jícím akrobatické prvky. -
Download (4MB)
https://theses.gla.ac.uk/ Theses Digitisation: https://www.gla.ac.uk/myglasgow/research/enlighten/theses/digitisation/ This is a digitised version of the original print thesis. Copyright and moral rights for this work are retained by the author A copy can be downloaded for personal non-commercial research or study, without prior permission or charge This work cannot be reproduced or quoted extensively from without first obtaining permission in writing from the author The content must not be changed in any way or sold commercially in any format or medium without the formal permission of the author When referring to this work, full bibliographic details including the author, title, awarding institution and date of the thesis must be given Enlighten: Theses https://theses.gla.ac.uk/ [email protected] RESEARCH, DEVELOPMENT AND MANUFACTURING POTENTIAL OF THE GENERAL AVIATION AIRCRAFT INDUSTRY IN THE CZECH REPUBLIC L. SMRCEK Department of Aerospace Engineering University of Glasgow. September 1996 © L. Smrcek ProQuest Number: 10391352 All rights reserved INFORMATION TO ALL USERS The quality of this reproduction is dependent upon the quality of the copy submitted. In the unlikely event that the author did not send a com plete manuscript and there are missing pages, these will be noted. Also, if material had to be removed, a note will indicate the deletion. uest ProQuest 10391352 Published by ProQuest LLC (2017). Copyright of the Dissertation is held by the Author. All rights reserved. This work is protected against unauthorized copying under Title 17, United States C ode Microform Edition © ProQuest LLC. ProQuest LLC. -
Los Motores Aeroespaciales, A-Z
Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 < aeroteca.com > Depósito Legal B 9066-2016 Título: Los Motores Aeroespaciales A-Z. © Parte/Vers: 1/12 Página: 1 Autor: Ricardo Miguel Vidal Edición 2018-V12 = Rev. 01 Los Motores Aeroespaciales, A-Z (The Aerospace En- gines, A-Z) Versión 12 2018 por Ricardo Miguel Vidal * * * -MOTOR: Máquina que transforma en movimiento la energía que recibe. (sea química, eléctrica, vapor...) Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 Este facsímil es < aeroteca.com > Depósito Legal B 9066-2016 ORIGINAL si la Título: Los Motores Aeroespaciales A-Z. © página anterior tiene Parte/Vers: 1/12 Página: 2 el sello con tinta Autor: Ricardo Miguel Vidal VERDE Edición: 2018-V12 = Rev. 01 Presentación de la edición 2018-V12 (Incluye todas las anteriores versiones y sus Apéndices) La edición 2003 era una publicación en partes que se archiva en Binders por el propio lector (2,3,4 anillas, etc), anchos o estrechos y del color que desease durante el acopio parcial de la edición. Se entregaba por grupos de hojas impresas a una cara (edición 2003), a incluir en los Binders (archivadores). Cada hoja era sustituíble en el futuro si aparecía una nueva misma hoja ampliada o corregida. Este sistema de anillas admitia nuevas páginas con información adicional. Una hoja con adhesivos para portada y lomo identifi caba cada volumen provisional. Las tapas defi nitivas fueron metálicas, y se entregaraban con el 4 º volumen. O con la publicación completa desde el año 2005 en adelante. -Las Publicaciones -parcial y completa- están protegidas legalmente y mediante un sello de tinta especial color VERDE se identifi can los originales. -
Training Guide for Weight-Shift Ultralights
TTrraaiinniinngg GGuuiiddee ffoorr WWeeiigghhtt--SShhiifftt UUllttrraalliigghhttss Safety Information for Instructors and Students EAA Weight-Shift Ultralight Training Guide Version 1.3 ______________________________________________________________________________ Introduction Ultralight aviation in the United States is the most unencumbered opportunity for solo flight in the world. Tremendous freedoms are given to ultralight pilots. However, at the same time there are strict limitations that must be followed. With this freedom, however, come responsibilities to ensure the safety of other individuals in the airspace as well as on the ground. In 1982 the FAA issued Federal Aviation Regulation Part 103, Ultralight Vehicles. With this regulation, the FAA chose to identify ultralights as vehicles and not aircraft. Because they are vehicles and not aircraft, this regulation allows individuals to operate ultralight vehicles without requiring FAA pilot or vehicle certification. Upon publishing Part 103 the FAA said it did not wish to issue pilot certificates for ultralight operators. Instead, the FAA said individuals who want to fly ultralights should participate in industry-established self-regulation and training programs. Since 1983 EAA has maintained programs to support Part 103 and has held an exemption to Part 103 that allowed the operation of 2-place ultralight training vehicles by authorized ultralight flight instructors. In 2004, the FAA passed the sport pilot & light-sport aircraft regulations. One specific purpose of this new rule was to transition 2-place ultralight training vehicles to experimental light-sport aircraft. As a result, after the training exemption expires on 1/31/08 there will no longer be a way to fly a 2-place ultralight to train ultralight pilots. -
White Eng 17 1.Cdr
WHITE PAPER I’M AERO White paper - I’M AERO First and the only ultralight coaxial helicopter This document is not a securities oering or a scheme of collective investment, nor does it require the registration or approval of the Monetary Authority of Singapore. The participants are advised to carefully read this document and be cautious when investing funds. 1. Introduction 2. Company’s products and their description 2.1. Ultralight aviation and coaxial system in helicopter industry 2.2. Manufacturing facilities of I’M AERO 2.3. Application range of the helicopters of I’M AERO 2.4. Review of the models and technical peculiarities of the I’M AERO helicopters 2.4.1. Ultralight airplane Nestling 21 2.4.2. Ultralight coaxial helicopter Helicopter R-34 2.4.3. Unmanned aerial vehicle Aerobot A-34 2.5. Geography of product application 3. Implementation of the blockchain 4. I’M AERO meets market needs 5. Business model 6. Marketing research 7. Roadmap of the Project 8. Project team 9. Structure of the Token Sale 10. Jurisdiction 11. Contacts * The current version of White Paper is not final and can be adjusted. The final parameters will be presented a few days before the Token Sale starts. Introducon The aim of the I AM AERO Project is to create a series production of ultralight aircraft that meet the needs of the population at the level of everyday use, as well as to meet the challenges of private business and the demands of government agencies. I’M AERO is a specialized aviation enterprise engaged in the design, development and production of manned and unmanned aerial vehicles. -
Vzlu 01 Historie.Qxd
80 YEARS OF RESEARCH & DEVELOPMENT IN AERONAUTICS AERONAUTICAL RESEARCH AND TEST INSTITUTE, Ltd. BERANOV›CH 130, 199 05 PRAHA 9 - LET“ANY, CZECH REPUBLIC AERONAUTICAL RESEARCH AND TEST INSTITUTE, PRAGUE, 1922 - 2002 80 Years of Research & Development in Aeronautics VÝZKUMNÝ A ZKUEBNÍ LETECKÝ ÚSTAV AERONAUTICAL RESEARCH AND TEST INSTITUTE, PRAGUE, CZECH REPUBLIC 1922-2002 P r e f a c e On 1 May 1922 the Air Navigation Study Institute of the Ministry of Defence the predecessor of today Aeronau- tical Research and Test Institute, VZLÚ was officially established. This book has been published to mark the 80th anniversary of that event, so crucial for the Czech aviation industry. The first part gives an overview of the status and work of the Institute in the years 1922 through 2002 and high- lights most significant moments in its history. This is fol- lowed by the current projects and tasks carried out in particular divisions and fields of interest. Prospects for the future are also outlined along with VZLÚ international co-operation activities. Many men and women at various social and professional levels played remarkable roles throughout the Institutes history. This book is dedicated to all those who enthusiastically contributed to VZLÚ achievements, benefiting the Czech aviation. Prague Letòany, 1 May, 2002 CONTENTS Preface . 2 1. 80 Years of Aeronautical R & D Activities . 4 2. International Activities of VZLÚ . 24 3. Low Speed Aerodynamics . 27 Ing. Milan Holl, CSc. 4. High Speed Aerodynamics . 30 General Manager 5. Strength of Aircraft Structure . 33 6. Flight Test Division . 38 7. Aircraft Propellers . 42 8. -
DESIGN and ANALYSIS of WING of an ULTRALIGHT AIRCRAFT USING ANSYS Sarath Raj N
ISSN: 2277-9655 [Sarath Raj* et al., 6(4): April, 2017] Impact Factor: 4.116 IC™ Value: 3.00 CODEN: IJESS7 IJESRT INTERNATIONAL JOURNAL OF ENGINEERING SCIENCES & RESEARCH TECHNOLOGY DESIGN AND ANALYSIS OF WING OF AN ULTRALIGHT AIRCRAFT USING ANSYS Sarath Raj N. S*, Chithirai Pon Selvan M, Michael G. Bseliss Faculty Member in Aerospace Engineering, Amity University, Dubai, United Arab Emirates Faculty Member in Mechanical Engineering, Amity University, Dubai, United Arab Emirates Undergraduate Student in Aerospace Engineering, Amity University, Dubai, United Arab Emirates DOI: 10.5281/zenodo.569965 ABSTRACT Ultralight aircraft is the flying of lightweight, one or two seat fixed-wing aircraft. In this article, the high wing of an ultralight aircraft is designed and analyzed with the help of software ANSYS FLUENT. The wing configuration includes its underlying contemplations like planform choice, location in the aircraft and the auxiliary outline includes the design calculations for the determination of airfoil, range of the wing, wing loading attributes and weight of the wing. Finally using an analysis software ANSYS, the design is done for the estimated takeoff weight. KEYWORDS: Ultralight Aircraft, Wing Design, Analysis, CFD, Ansys, Lift, Drag INTRODUCTION An ultralight aircraft is a very light and small aircraft which is used for purposes like sports, personal hobby and recreational interests mainly. It is also referred to as a microlight aircraft. An ultralight light aircraft is very light in weight and flies very slowly, which is why they are not considered to be very hazardous. The usage of ultralight aircrafts came to play during the late 1970s and early 1980s, mostly stimulated by the gliding movement and many people were sought after affordable powered flight. -
Fixed-Wing Ultralights Found Today Are Conventional 3-Axis Designs, and Many Different Types of 3- Axis Light Aircraft Could Be Suitable for Dual Flight Training
TTrraaiinniinngg GGuuiiddee ffoorr FFiixxeedd--WWiinngg UUllttrraalliigghhttss Safety Information for Instructors and Students Introduction Ultralight aviation in the United States is the most unencumbered opportunity for solo flight in the world. Tremendous freedoms are given to ultralight pilots. However, at the same time there are strict limitations that must be followed. With this freedom, however, come responsibilities to ensure the safety of other individuals in the airspace as well as on the ground. In 1982 the FAA issued Federal Aviation Regulation Part 103, Ultralight Vehicles. With this regulation, the FAA chose to identify ultralights as vehicles and not aircraft. Because they are vehicles and not aircraft, this regulation allows individuals to operate ultralight vehicles without requiring FAA pilot or vehicle certification. Upon publishing Part 103 the FAA said it did not wish to issue pilot certificates for ultralight operators. Instead, the FAA said individuals who want to fly ultralights should participate in industry-established self-regulation and training programs. Since 1983 EAA has maintained programs to support Part 103 and has held an exemption to Part 103 that allowed the operation of 2-place ultralight training vehicles by authorized ultralight flight instructors. In 2004, the FAA passed the sport pilot & light-sport aircraft regulations. One specific purpose of this new rule was to transition 2-place ultralight training vehicles to experimental light-sport aircraft. As a result, after the training exemption expires on 1/31/08 there will no longer be a way to fly a 2-place ultralight to train ultralight pilots. The FAA has said they intend ultralight pilot training to be conducted in N-numbered aircraft by FAA flight instructors. -
Safety Study Ultralight Aviation Safety and Its Improvement Through
Safety study S1/2009L Ultralight Aviation Safety and its Improvement through Accident Investigation Translation of the Finnish original safety study According to Annex 13 to the Convention on International Civil Aviation, paragraph 3.1, the purpose of aircraft ac- cident and incident investigation is the prevention of accidents. It is not the purpose of aircraft accident investiga- tion or the investigation report to apportion blame or to assign responsibility. This basic rule is also contained in the Investigation of Accidents Act, 3 May 1985 (373/85) and European Council Directive 94/56/EC. Use of the re- port for reasons other than improvement of safety should be avoided. Onnettomuustutkintakeskus Centralen för undersökning av olyckor Accident Investigation Board Osoite / Address: Sörnäisten rantatie 33 C Adress: Sörnäs strandväg 33 C FIN-00500 HELSINKI 00500 HELSINGFORS Puhelin / Telefon: (09) 1606 7643 Telephone: +358 9 1606 7643 Fax: (09) 1606 7811 Fax: +358 9 1606 7811 Sähköposti: [email protected] tai [email protected] E-post: [email protected] eller förnamn.slä[email protected] Email: [email protected] or first name.last [email protected] Internet: www.onnettomuustutkinta.fi Henkilöstö / Personal / Personnel: Johtaja / Direktör / Director Veli-Pekka Nurmi Hallintopäällikkö / Förvaltningsdirektör / Administrative Director Pirjo Valkama-Joutsen Osastosihteeri / Avdelningssekreterare / Assistant Sini Järvi Toimistosihteeri / Byråsekreterare / Assistant Leena Leskelä Ilmailuonnettomuudet / Flygolyckor / Aviation