L'industrie Aéronautique Et Spatiale Française
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Cockpit Juni 2011 Als PDF Herunterladen
Das Schweizer Luftfahrt-Magazin Nr. 06/Juni 2011 CHF 8.20 / € 5.50 Virtual Swiss Air Force Cover Story AERO 2011 – Fliegen wir in Zukunft «elektrisch»? Military Aviation Civil Aviation Helicopter Stealth-Heli auf 75 Jahre SKYe SH09 –Schweizer Terroristenjagd Aer Lingus Heli der Extraklasse real watches for real people Oris Swiss Hunter Team PS Edition Automatik-Werk Datumsanzeige Verschraubte Krone Wasserdicht bis 10 bar/100 m www.oris.ch Cockpit 06 2011 Editorial 3 Take-off Liebe Leserinnen und Leser «Ohne Flugplätze kein Luftverkehr!» heisst der dem seit Anfang Jahr eingeführten «Landefranken» tragen auch die Flug- eingängige Slogan des Verbandes Schweizer Flug- platznutzer einen kleinen Beitrag dazu bei, dass die VSF-Vertreter fach- plätze. Diese vier Worte bringen es auf den Punkt. lich und zeitgerecht den Regulierern in Brüssel und Köln auf Augenhöhe Flugplätze, ob klein oder gross, haben oft eine lange begegnen können. Piloten und Flugplatzbetreiber sitzen in einem Boot Tradition. Über Jahrzehnte hinweg dienten sie der – ganz im Sinne des Slogans «Ohne Flugplätze kein Luftverkehr!» Le- Schulung, dem Geschäfts- und Linienverkehr oder sen Sie bitte dazu den Beitrag des Geschäftsführers des VSF, Dr. Pierre dem fliegerischen Freizeitvergnügen. An Flugplät- Moreillon (Seite 26). zen entstanden Wartungs- und Zulieferbetriebe, Anfang Mai ist Cockpit mit dem VSF eine Zusammenarbeit eingegangen. Restaurants und Hotels, Flugschulen und Charter- Monatlich wird der Verband über die wichtigsten und dringlichsten An- betriebe. Und in der Folge weitere Unternehmungen, deren Wertschöpfung liegen berichten. Aktuell und umfassend informiert auch die VSF-Website aus der Luftfahrt stammt. Kurz: Arbeitsplätze, Steuerzahler. aerodromes.ch. Hier finden Sie alles, was zum Thema von Relevanz ist. -
Police Aviation News August 2015
Police Aviation News August 2015 ©Police Aviation Research Number 232 August 2015 PAR Police Aviation News August 2015 2 PAN—Police Aviation News is published monthly by POLICE AVIATION RESEARCH, 7 Wind- mill Close, Honey Lane, Waltham Abbey, Essex EN9 3BQ UK. Contacts: Main: +44 1992 714162 Cell: +44 7778 296650 Skype: BrynElliott E-mail: [email protected] Police Aviation Research Airborne Law Enforcement Member since 1994—Corporate Member since 2014 SPONSORS Airborne Technologies www.airbornetechnologies.at AeroComputers www.aerocomputers.com Avalex Displays www.avalex.com Broadcast Microwave www.bms-inc.com FLIR Systems www.flir.com L3 Wescam www.wescam.com Powervamp www.powervamp.com Trakka Searchlights www.trakkacorp.com Airborne Law Enforcement Association www.alea.org EDITORIAL I have just returned from Houston and the ALEA annual convention. It may be many miles from my home shores and the words may have been spoken by an American but they rang somewhat true to the situation at home where the new and developing National Police Air Service is still finding its feet. I was sitting in on the Unit Managers Course when the instructor, a greatly respected man who earned his respect by running a large and successful air operation, reminded his stu- dents of their purpose in life. “If the cops on the street are not screaming for you to come in the expectation of getting [air support] help, the operation is flawed and should be considered a failure” Bryn Elliott LAW ENFORCEMENT BRAZIL PARA: Emergency services aviation in Brazil has reportedly fallen on hard times. A few years ago the sector had in place a major forward plan that encompassed most of Brazil’s States and most of the airborne service provision and was expected to see growth in re- sources and manpower controlled within a number of complex governing groups [DFNSP, CAVSEG, CONAV, AEAP, SENASP] but when President Rousseff took power in 2011 she swept them away leaving a vacuum. -
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. -
Aircraft Name Stage Flights Aircraft Hours AEROSPATIALE AS350 NO
Public Transport Air Taxi Operations (a) for Year 2019 Table 1.13 Aircraft Name Stage Flights Aircraft Hours AEROSPATIALE AS350 NO MASTER SERIES 3 169 3 307 ASSIGNED AEROSPATIALE AS355 NO MASTER SERIES 4 418 5 715 ASSIGNED AEROSPATIALE AS365 NO MASTER SERIES 8 978 1 916 ASSIGNED AGUSTA A109 NO MASTER SERIES ASSIGNED 12 221 5 323 AGUSTA AW139 NO MASTER SERIES ASSIGNED 16 161 11 514 AGUSTA AW169 NO MASTER SERIES ASSIGNED 8 120 2 198 AGUSTA AW189 NO MASTER SERIES ASSIGNED 5 773 5 120 AIRBUS A321 200N 1 1 ATR ATR42 500 6 17 ATR ATR72 200 2 079 1 896 BAE JETSTREAM 4100 4100 1 783 1 185 BEECH 200 NO MASTER SERIES ASSIGNED 9 396 9 178 BEECH 300 NO MASTER SERIES ASSIGNED 15 14 BEECH 400 NO MASTER SERIES ASSIGNED 1 726 2 721 BEECH 90 NO MASTER SERIES ASSIGNED 202 188 BELL 206 B 9 792 2 264 BELL 429 NO MASTER SERIES ASSIGNED 1 053 951 BOMBARDIER BD100 1A10 NO MASTER SERIES 201 348 ASSIGNED BRITTEN NORMAN BN2A UNDESIGNATED MASTER 7 495 2 242 SERIES BRITTEN NORMAN BN2T NO MASTER SERIES 510 687 ASSIGNED CANADAIR CL600 2B16 600 813 1 438 CESSNA 310 NO MASTER SERIES ASSIGNED 765 747 CESSNA 402 NO MASTER SERIES ASSIGNED 233 199 CESSNA 404 NO MASTER SERIES ASSIGNED 67 57 CESSNA 421 NO MASTER SERIES ASSIGNED 162 167 CESSNA 510 NO MASTER SERIES ASSIGNED 1 044 1 066 CESSNA 525 NO MASTER SERIES ASSIGNED 1 524 1 986 CESSNA 550 NO MASTER SERIES ASSIGNED 1 442 1 902 CESSNA 560 NO MASTER SERIES ASSIGNED 2 970 3 576 CESSNA 680 NO MASTER SERIES ASSIGNED 308 528 CESSNA F406 NO MASTER SERIES ASSIGNED 894 672 DASSAULT FALCON 2000 NO MASTER SERIES 775 1 192 ASSIGNED -
AD 2012-0170R2 [Task 2014.211] TGB Oil Level and Magnetic Chip Detector Insp and Pitch Control Rod Bearing Insp
EASA AD No.: 2012-0170R2 EASA AIRWORTHINESS DIRECTIVE AD No.: 2012-0170R2 Date: 20 June 2014 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation. This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an aircraft to which an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [EC 2042/2003 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemption]. Design Approval Holder’s Name: Type/Model designation(s): AIRBUS HELICOPTERS SA 365, AS 365, SA 366 and EC 155 helicopters TCDS Number: EASA.R.105 Foreign AD: Not applicable Revision: This AD revises EASA AD 2012-0170R1, dated 18 October 2013. ATA 05 Time Limits and Maintenance Checks – Tail Rotor Gearbox (TGB) Oil Level and Magnetic Chip Detector – Inspection ATA 65 Tail Rotor – Pitch Control Rod Bearing – Inspection / Replacement Manufacturer(s): Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aerospatiale). Applicability: SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and EC 155 B1 helicopters, all serial numbers, except those modified in accordance with Eurocopter (EC) modification (mod) 07 65B63. -
Helideck Manual
English version HELIDECK MANUAL Helicopter operations on offshore installations In cooperation with Revision date 01.09.2016 revisjonsdato 01.12.2015 Changes in this edition: • “OLF” is systematically changed to “Norwegian Oil and Gas Association” • References to Authority regulations updated • Relevant EN-standards updated • Minor changes in health requirements • Minor addition in refueling procedures • Enclosure F1 updated • Enclosure F2 updated • Enclosure F3 cancelled • Enclosure G updated • Enclosure I updated • Enclosure L updated DOKUMENTNR: REVISONSNR: REVISJONSDATO: Final 01.09.2016 Side 2 TABLE OF CONTENTS 1 General .......................................................................................................................... 5 1.1 Purpose and scope ......................................................................................................... 5 1.2 Responsibilities ............................................................................................................... 5 1.3 Approval ......................................................................................................................... 5 1.4 Distribution and Amendments ......................................................................................... 5 1.5 References ..................................................................................................................... 6 1.6 Definitions ....................................................................................................................... 6 2 -
201311 General Aviation Report November 2013
OCCURRENCE LISTING Aircraft Below 5700kg OCCURRENCES RECORDED BETWEEN 01 November 2013 and 30 November 2013 FIXED WING AIRCRAFT AERO AT3 BOMBARDIER ROTAX Standing EGBK (ORM): 08/11/2013 201314409 912 Northampton/Sywell Numerous flights carried out and not entered in aircraft Tech Logs. Over a period from March 2009 to July 2013, there have been 152 flights (approx 120 flight hours) carried out using four aircraft. No Tech Log entries have been made for any of these flights. There are significant airworthiness implications for the aircraft involved. All four aircraft are currently grounded. Appropriate CAA action is being taken as a result of this incident. AUSTER AUSTER J (J5K) OTHER (Blackburn Rejected take-off Watchford Farm Strip 06/10/2013 201315059 Cirrus Minor IIA) UK Reportable Accident: Aircraft overran runway during rejected take-off and struck a fence. Damage to rear fuselage and tail plate. Two POB, no injuries. Subject to AAIB AARF investigation. AVIONS ROBIN DR400 LYCOMING En-route Casablanca FIR 06/10/2013 201314382 360 FAMILY DR400 infringed an active area closed by NOTAM within the Casablanca FIR. Content: This list contains occurrences and accidents to aircraft of 5700kg and below recorded on the MOR database during the period shown above. The list includes information reported to the CAA, information from CAA investigations and deductions by CAA staff. The authenticity of the contents or absence of errors and omissions cannot be guaranteed. The list contains preliminary information. Purpose: The information is supplied for flight safety purposes only. Queries & Contact Safety Data Department, Civil Aviation Authority, Aviation House, Gatwick Reporting: Airport, W Sussex, RH6 0YR. -
Organisations Approved in Accordance with Part M, Subpart G Published 04 September 2018 That Have ARC Privileges
Organisations approved in accordance with Part M, Subpart G Published 04 September 2018 that have ARC privileges Approval Address Aircraft Type Reference UK.MG.0231 2 Excel Aviation Limited Extra EA200/300 Series The Tiger House Sywell Aerodrome Piper PA31 AOC No GB2299 Sywell Beech 200 Series Northamptonshire NN6 0BN Boeing 727 Tel: 01778 590448 Eurocopter EC135 Series Email: [email protected] Boeing 737 300/400/500 Regional Office: Shared Service Centre UK.MG.0661 A2B Aero Limited EUROCOPTER AS355 SERIES Hangar 4S Oxford Airport SIKORSKY S76 SERIES AOC No Kidlington BELL 429 SERIES Oxfordshire OX5 1RA EUROCOPTER AS365 SERIES Tel: 01844 352239 / 07777 236 0123 EUROCOPTER EC135 SERIES Email: [email protected] SINGLE TURBINE ENGINE HELICOPTERS NOT E AGUSTA WESTLAND AW139 Regional Office: Shared Service Centre EUROCOPTER BO105 EUROCOPTER DEUTSCHLAND MBB-BK 117 SERI EUROCOPTER EC155 SERIES MD HELICOPTERS 902 ROBINSON R22/R44 AGUSTA AW109 SERIES BELL 212/AGUSTA AB212 BELL 412/AGUSTA AB412 AIRBUS HELICOPTERS EC225 AIRBUS HELICOPTERS AS332 UK.MG.0494 Acropolis Aviation Limited AIRBUS A319-100 SERIES Business Aviation Centre Farnborough AOC No 2363 Airport Farnborough Hampshire GU14 6XA Tel: 01458 241112 Email: aidan.murphy@acropolis- aviation.com Regional Office: Shared Service Centre UK.MG.0385 ACS Aviation Limited SINGLE TURBOPROP AEROPLANES NOT EXCEED Hangar 4 Perth Airport PISTON ENGINE AEROPLANES - METAL STRUCT AOC No Scone PISTON ENGINE AEROPLANES - COMPOSITE ST Perthshire PH2 6PL PISTON ENGINE AEROPLANES - WOODEN STRU -
4. Operational Management 3. References 2. Entities Involved 1
Airport Manual Ed. 3. Operating Procedures 15/01/2016 Ciampino - G.B.Pastine 02 May 2007 MOV/14/Movement of Helicopters on the Apron Page 1/7 Airport 1. Purpose This procedure concerns the regulation of the movement rotating-wing aircraft in the apron area, identifying routes that ensure the presence of adequate safety precautions, in accordance with Appendix 14, Volume II. 2. Entities Involved - AdR Flight Control - AdR Operational Security (SAR) - ENAV TWR - INAER - VV.F. - State Forestry Department - Handlers 3. References - Appendix 14 ICAO, Vol. II (Fourth Edition July 2013) - ENAC Regulations for the Construction and Exercise of Heliports 4. Operational Management The rules for using the taxiways, published in AIP AD 2 LIRA 1-12 ITEM 3, provide for the following: Helicopter traffic is not permitted on the segment of the TC junction from the SG junction to the SD junction and the SD junction. Helicopters are only permitted on this junction if towed with their engines shut down. On the apron, operations for lengths exceeding 20m are only permitted if towed with engines shut down. The operational management of helicopters on the apron described below does not concern helicopters managed by the Military Airforce (Aeronautica Militare - A.M.) Below are the operational management procedures for helicopters on the apron shared with ENAV: a) The use of the TC taxilanes, in the segment between taxilanes SD and SG, and SD does not permit the movement of helicopters with engines switched on, whether taxiing or hovering. Therefore, helicopters that need to park in the hangars (Forestry Department/INAER) located in front of the intercepting taxilanes or helicopters needing to pass Airport Manual Ed. -
Varga Béla Helikopter Gázturbinás Hajtóművek Technikai Elemzése
Varga Béla HELIKOPTER GÁZTURBINÁS HAJTÓMŰVEK TECHNIKAI ELEMZÉSE A helikopterek erőforrásainak jelentős fejlődése, ami főképpen a hajtómű teljesítménytömegviszony, a hatásfok és fajlagos-tüzelőanyag fogyasztás, valamint megbízhatóság, és üzemeltethetőségben jelenik meg, természetesen kiha- tással volt a helikopterek harcászati technikai jellemzőire. Ezek a tények kutatásra érdemessé teszi ezt a területet. A cikkben végig követem a helikopter hajtóművek időbeni fejlődési folyamatát. Ismertetem működésük jellegzetességeit, a legfontosabb gyártókat és gyártmányokat. Statisztikai kimutatásokon keresztül szemléltetem, hogy milyen teljesít- mény paraméterekkel rendelkeztek a múltban és rendelkeznek a jelenleg alkalmazott helikopter hajtóművek. Kulcsszavak: Helikopter gázturbinás hajtóművek, turboshaft, tengelyteljesítmény, fajlagos tüzelőanyag fogyasz- tás, termikus hatásfok, fajlagos hasznos munka. A GÁZTURBINÁS KORSZAK KEZDETE A II. világháború végére a dugattyús légcsavaros repülőgépek elérték fejlődésük csúcspontját. Ez azt jelentette, hogy a sebességük valamivel meghaladta a 700 km/h-t. A repülési magasságuk elérte egy átlagos vadászrepülőgép esetében a 12 km-t, speciális felderítő változatok esetében pedig a 1415 km-t. Jól példázza ezt a folyamatot a II. világháború egyik legismertebb és talán legtöbb fejlesztési fázison átesett vadászrepülőgépe, a Messerschmitt Bf 109. Az 1. táblázat- ban táblázatban a teljesség igénye nélkül felsoroltam néhány fő változatát ennek a repülőgép- nek, szemléltetve, hogy az egyre nagyobb teljesítményű motorok nem hoztak átütő eredményt a repülőgépek sebesség növekedése szempontjából. Típus változat Év Motor Teljesítmény (Le) Sebesség (km/h) Bf 109B 1937 Jumo 210 720 466 Bf 109D 1938 DB 600 960 514 Bf 109E 1939 DB 601A 1175 569 Bf 109F 1941 DB 601N 1200 614 Bf 109G 1942 DB 605 1475 643 Bf 109K 1944 DB 605D 2000 (metanol befecsk.) 724 1. táblázat Bf 109 teljesítmény adatai [1] Ezek a korlátok ismertek voltak már a II. -
Military Simulator Census 2014 Flightglobal Insight | 3
IN ASSOCIATION WITH SPECIAL REPORT MILITARY SIMULATOR CENSUS 2014 Flightglobal Insight | 3 Flightglobal_Partner of Choice_Oct2014_AM310.indd 1 2014-10-28 8:37 AM MILITARY SIMULATOR CENSUS 2014 CONTENTS ABBREViaTIONS 4Mil 16 Indonesia 22 ANALYSIS 5Mitsubishi 17 Iran 22 NH Industries 17 Iraq 22 CENSUS BY aiRCRAFT MANUfacTURER Northrop Grumman 17 Israel 22 Aero Vodochody 7 Panavia 17 Italy 23 AgustaWestland 7 Pilatus 17 Japan 23 AIDC 7PZL 17 Jordan 23 Airbus Military 7 Raytheon 18 Kuwait 23 Alenia Aermacchi 8 Saab 18 Malaysia 23 AMX International 8 SEPECAT 18 Mexico 23 Antonov 8 Shenyang 18 Morocco 24 BAE Systems 8 Sikorsky 18 Myanmar 24 Beechcraft 8 Sukhoi 19 Netherlands 24 Bell 9 Transall 19 New Zealand 24 Bell Boeing 10 Tupolev 19 Nigeria 24 Boeing 10 Westland 19 Norway 24 Boeing Vertol 12 Oman 24 Boeing/BAS Systems 12 CENSUS BY OPERATOR COUNTRY Pakistan 24 Chengdu Aviation/Pakistan Aeronautical Complex 12 Algeria 20 Peru 24 CASA 12 Argentina 20 Poland 24 Dassault 12 Australia 20 Portugal 24 Dassault/Dornier 13 Austria 20 Qatar 24 Dassault-Breguet 13 Bahrain 20 Romania 24 Douglas 13 Belgium 20 Russia 24 Embraer 13 Brazil 20 Saudi Arabia 25 Enstrom 13 Brunei 20 Singapore 25 Eurocopter 13 Canada 20 Slovakia 25 Eurofighter 14 Chile 21 South Africa 25 Fairchild Republic 14 Colombia 21 South Korea 25 Hawker Beechcraft 14 Croatia 21 Spain 25 Hindustan Aeronautics 14 Czech Republic 21 Sudan 26 Hongdu 14 Denmark 21 Switzerland 26 IAR 14 Ecuador 21 Taiwan 26 Israel Aerospace Industries 14 Egypt 21 Thailand 26 Korea Aerospace Industries 14 Finland -
Design of a Hoistable Helicopter Platform for 60M Yacht
Design of a hoistable helicopter platform for 60m yacht Zsolt Papp Master Thesis presented in partial fulfillment of the requirements for the double degree: “Advanced Master in Naval Architecture” conferred by University of Liege "Master of Sciences in Applied Mechanics, specialization in Hydrodynamics, Energetics and Propulsion” conferred by Ecole Centrale de Nantes developed at University of Genoa in the framework of the “EMSHIP” Erasmus Mundus Master Course in “Integrated Advanced Ship Design” Ref. 159652-1-2009-1-BE-ERA MUNDUS-EMMC Supervisor: Prof. Dario Boote, University of Genoa Reviewer: Prof. Philippe Rigo, University of Liege Genoa, February 2012 2 Zsolt PAPP TABLE OF CONTENTS DECLARATION OF AUTHORSHIP ................................................................................... 6 ACKNOWLEDGEMENTS ................................................................................................... 7 ABSTRACT (English)........................................................................................................... 8 PRESENTAZIONE (Italiano) ................................................................................................ 9 ABSTRAKTE (Deutsch) ......................................................................................................10 1. INTRODUCTION ...........................................................................................................11 1.1. Overview ..................................................................................................................11