AMC a GM K Částem M, 145, 66, 147

Total Page:16

File Type:pdf, Size:1020Kb

AMC a GM K Částem M, 145, 66, 147 Konsolidované zn ění Evropská agentura pro bezpe čnost letectví AMC a GM k Částem M, 145, 66, 147 Přijatelné zp ůsoby pr ůkazu a poradenský materiál k na řízení Komise (ES) č. 2042/2003 ze dne 20. listopadu 2003 pro zachování letové zp ůsobilosti letadel a leteckých výrobk ů, letadlových částí a za řízení a schvalování organizací a personálu zapojených do t ěchto úkol ů Ve zn ění: Datum ú činnosti Rozhodnutí výkonného ředitele č. 2003/19/RM 28. 11. 2003 ze dne 28. listopadu 2003 Rozhodnutí výkonného ředitele č. 2005/07/R 19. 12. 2005 ze dne 19. prosince 2005 Rozhodnutí výkonného ředitele č. 2006/01/R 16. 05. 2006 ze dne 16. kv ětna 2006 Rozhodnutí výkonného ředitele č. 2006/06/R 07. 08. 2006 ze dne 31. července 2006 Rozhodnutí výkonného ředitele č. 2006/11/R 25. 12. 2006 ze dne 18. prosince 2006 Rozhodnutí výkonného ředitele č. 2006/14/R 27. 12. 2006 ze dne 20. prosince 2006 Rozhodnutí výkonného ředitele č. 2007/001/R 20. 03. 2007 ze dne 13. b řezna 2007 Konsolidované zn ění Rozhodnutí výkonného ředitele č. 2007/002/R 20. 03. 2007 ze dne 13. b řezna 2007 Rozhodnutí výkonného ředitele č. 2007/003/R 20. 03. 2007 ze dne 13. b řezna 2007 Rozhodnutí výkonného ředitele č. 2007/009/R 02. 05. 2007 ze dne 25. dubna 2007 ZÁM ĚRN Ě NEPOUŽITO AMC k Části M Konsoidované zn ění AMC a GM k Části M ČÁST M OBSAH Přijatelné zp ůsoby pr ůkazu k Části M ODDÍL A – Technické požadavky A – A – 1 Hlava A – Všeobecn ě A – A – 1 Hlava B – Odpov ědnost ě A – B – 1 AMC M.A.201 (h) Odpov ědnosti A – A – 1 AMC M.A.201 (h) 1 Odpov ědnosti A – B – 1 AMC M.A.201 (h) 2 Odpov ědnosti A – B – 3 AMC M.A.202 (a) Hlášení událostí A – B – 3 AMC M.A.202 (b) Hlášení událostí A – B – 4 Hlava C - Zachování letové zp ůsobilosti A – C – 1 AMC M.A.301 -1 Úkoly zachování letové zp ůsobilosti A – C – 1 AMC M.A.301 -2 Úkoly zachování letové zp ůsobilosti A – C – 1 AMC M.A.301 -3 Úkoly zachování letové zp ůsobilosti A – C – 2 AMC M.A.301 -4 Úkoly zachování letové zp ůsobilosti A – C – 2 AMC M.A.301 -5 Úkoly zachování letové zp ůsobilosti A – C – 2 AMC M.A.301 -7 Úkoly zachování letové zp ůsobilosti A – C – 3 AMC M.A.302 Program údržby A – C – 3 AMC M.A.302(c) Vyhov ění programu údržby A – C – 3 AMC M.A.302 (d) Program údržby - programy spolehlivosti A – C – 4 AMC M.A.304 Údaje pro modifikace a opravy A – C – 4 AMC M.A.305 (d) Systém záznam ů zachování letové zp ůsobilosti letadla A – C – 4 AMC M.A.305 (h) Systém záznam ů zachování letové zp ůsobilosti letadla A – C – 5 AMC M.A.305 (h) 6 Systém záznam ů zachování letové zp ůsobilosti letadla A – C – 6 AMC M.A.306 (a) Systém technického deníku provozovatele A – C – 6 AMC M.A.306 (b) Systém technického deníku provozovatele A – C – 8 AMC M.A.307 (a) Převod záznam ů zachování letové zp ůsobilosti letadla A – C – 8 Hlava D – Normy údržby A – D – 1 AMC M.A.401 (b) Údaje pro údržbu A – D – 1 AMC M.A.401 (c) Údaje pro údržbu A – D – 1 AMC M.A.402 (a) Provád ění údržby A – D – 2 AMC M.A.402 (b) Provád ění údržby A – D – 3 AMC M.A.402 (d) Provád ění údržby A – D – 4 AMC M.A.402 (e) Provád ění údržby A – D – 4 AMC M.A.403 (d) Závady letadla A – D – 4 Hlava E – Letadlové celky A – E – 1 AMC M.A.501 (a) Zástavba A – E – 1 AMC M.A.501 (b) Zástavba A – E – 2 AMC M.A.501 (c) Zástavba A – E – 2 AMC M.A.501 (d) Zástavba A – E – 3 AMC M.A.504 (a) Řízení letadlových celk ů neschopných provozu A – E – 3 AMC M.A.504 (b) Řízení letadlových celk ů neschopných provozu A – E – 4 AMC M.A.504 (c) Řízení letadlových celk ů neschopných provozu - nepoužitelné letadlové celky A – E – 4 AMC M.A.504 (d) 2 Řízení letadlových celk ů neschopných provozu A – E – 5 AMC M.A.504 (e) Řízení letadlových celk ů neschopných provozu A – E – 5 0 – 1 Rozhodnutí č. 2007/001/R 20.03.2007 Konsolidované zn ění AMC a GM k Části M Hlava F – Organizace k údržb ě A – F – 1 AMC M.A.601 Rozsah A – F – 1 AMC M.A.602 Žádost A – F – 1 AMC M.A.603 (a) Rozsah oprávn ění A – F – 1 AMC M.A.603 (b) Rozsah oprávn ění A – F – 1 AMC M.A.604 Příru čka organizace údržby A – F – 3 AMC M.A.605 (a) Provozní prostory A – F – 3 AMC M.A.605 (b) Provozní prostory A – F – 3 AMC M.A.605 (c) Provozní prostory A – F – 3 AMC M.A.606 (a) Požadavky na personál A – F – 4 AMC M.A.606 (b) Požadavky na personál A – F – 4 AMC M.A.606 (c) Požadavky na personál A – F – 4 AMC M.A.606 (d) Požadavky na personál A – F – 5 AMC M.A.606 (e) Požadavky na personál A – F – 5 AMC M.A.606 (f) Požadavky na personál A – F – 5 AMC M.A.607 Osv ědčující personál A – F – 6 AMC M.A.607 (c) Osv ědčující personál A – F – 7 AMC M.A.608 (a) Letadlové celky, vybavení a ná řadí A – F – 7 AMC M.A.608 (b) Letadlové celky, vybavení a ná řadí A – F – 7 AMC M.A.609 Údaje pro údržbu A – F – 8 AMC M.A.613 (a) Osv ědčení o uvoln ění letadlového celku do provozu A – F – 8 AMC M.A.614 (a) Záznamy údržby A – F – 12 AMC M.A.614 (c) Záznamy údržby A – F – 12 AMC M.A.616 Kontrola organizace A – F – 12 AMC M.A.617 Zm ěny organizace oprávn ěné k údržb ě A – F – 13 Hlava G - Organizace k řízení zachování letové zp ůsobilosti A – G – 1 AMC M.A.704 Výklad řízení zachování letové zp ůsobilosti A – G – 1 AMC M.A.705 Provozní prostory A – G – 3 AMC M.A.706 Požadavky na personál A – G – 3 AMC M.A.706 (e) Požadavky na personál A – G – 4 [AMC M.A.706 (f) Požadavky na personál A – G – 4 ] AMC M.A.707 (a) Personál kontroly letové zp ůsobilosti A – G – 4 [AMC M.A.708 (b)3 Řízení zachování letové zp ůsobilosti A – G – 5 ] AMC M.A.708 (c) Řízení zachování letové zp ůsobilosti A – G – 5 AMC M.A.708 (c) (1) Řízení zachování letové zp ůsobilosti – neplánovaná údržba A – G – 6 AMC M.A.710 (b) a (c) Kontrola letové zp ůsobilosti A – G – 7 AMC M.A.710 (e) Kontrola letové zp ůsobilosti A – G – 7 AMC M.A.711 (b) Práva organizace A – G – 7 AMC M.A.712 (a) Systém jakosti A – G – 7 AMC M.A.712 (b) Systém jakosti A – G – 8 AMC M.A.712 (f) Systém jakosti A – G – 9 AMC M.A.713 Zm ěny organizace oprávn ěné k řízení zachování letové zp ůsobilosti A – G – 9 AMC M.A.714 Uchovávání záznam ů A – G – 9 Hlava H – Osv ědčení o uvon ění do provozu - CRS A – H – 1 AMC M.A.801 (b) Osv ědčení o uvoln ění letadla do provozu A – H – 1 AMC M.A.801 (d) Osv ědčení o uvoln ění letadla do provozu A – H – 1 AMC M.A.801 (e) Osv ědčení o uvoln ění letadla do provozu A – H – 1 AMC M.A.801 (f) Osv ědčení o uvoln ění letadla do provozu A – H – 2 AMC M.A.802 Osv ědčení o uvoln ění letadlového celku do provozu A – H – 2 AMC M.A.803 Oprav ňování pilotem-vlastníkem A – H – 2 Rozhodnutí č. 2007/001/R 0 – 2 20.03.2007 Konsoidované zn ění AMC a GM k Části M Hlava I – Osv ědčení kontroly letové zp ůsobilosti A – I – 1 AMC M.A.901 (a) Kontrola letové zp ůsobilosti letadla A – I – 1 AMC M.A.901 (b) Kontrola letové zp ůsobilosti letadla A – I – 1 AMC M.A.901 (c) 2 Kontrola letové zp ůsobilosti letadla A – I – 1 AMC M.A.901 (d) Kontrola letové zp ůsobilosti letadla A – I – 1 AMC M.A.901 (e) Kontrola letové zp ůsobilosti letadla A – I – 2 AMC M.A.903 (a) 1 Převod letadel zapsaných v leteckém rejst říku v rámci EU A – I – 3 AMC M.A.903 (b) Převod letadel zapsaných v leteckém rejst říku v rámci EU A – I – 3 AMC M.A.904 (a) 1 Kontrola letové zp ůsobilosti letadel dovážených do EU A – I – 3 AMC M.A.904 (a) 2 Kontrola letové zp ůsobilosti letadel dovážených do EU A – I – 3 AMC M.A.904 (b) Kontrola letové zp ůsobilosti letadel dovážených do EU A – I – 4 ODDÍL B – Postupy pro p říslušný ú řad B – A – 1 Hlava A - Všeobecn ě B – A – 1 AMC M.B.102 (a) Příslušný ú řad – Všeobecn ě B – A – 1 AMC M.B.102 (c) Příslušný ú řad - Kvalifikace a výcvik B – A – 1 AMC M.B.102 (d) Organizace p říslušného ú řadu - Postupy B – A – 2 AMC M.B.104 (a) Uchovávání záznam ů B – A – 2 AMC M.B.104 (f) Uchovávání záznam ů B – A – 2 AMC M.B.105 (a) Vzájemná vým ěna informací B – A – 3 Hlava B - Zodpov ědnost B – B – 1 Hlava C – Zachování letové zp ůsobilosti B – C – 1 AMC M.B.301 (a) Program údržby B – C – 1 AMC M.B.301 (b) Program údržby B – C – 1 AMC M.B.301 (c) Program údržby B – C – 2 AMC M.B.301 (d) Program údržby B – C – 2 AMC M.B.303 (b) Sledování zachování letové zp ůsobilosti B – C – 2 AMC M.B.303 (c) Sledování zachování letové zp ůsobilosti B – C – 2 AMC M.B.303 (d) Sledování zachování letové zp ůsobilosti letadla B – C – 2 Hlava D – Normy údržby B – D – 1 Hlava E – Letadlové celky B – E – 1 Hlava F – Organizace k údržb ě B – F – 1 AMC M.B.602 (a) První oprávn ění B – F – 1 AMC M.B.602 (b) První oprávn ění B – F – 1 AMC M.B.602 (e) První oprávn ění B – F – 1 AMC M.B.602 (f) První oprávn ění B – F – 2 AMC M.B.602 (g) První oprávn ění B – F – 2 AMC M.B.603 (a) Vydání oprávn ění B – F – 2 AMC M.B.603 (c) Vydání oprávn ění B – F – 2 AMC M.B.604 (b) Pr ůběžný dozor B – F – 2 AMC M.B.605 (b) 1 Nálezy B – F – 3 AMC M.B.606 Zm ěny B – F – 3 Hlava G Organizace k řízení zachování letové zp ůsobilosti B – G – 1 AMC M.B.701 (a) Žádost B – G – 1 AMC M.B.702 (a) První oprávn ění B – G – 1 AMC M.B.702 (b) První oprávn ění B – G – 1 AMC M.B.702 (c) První oprávn ění B – G – 1 AMC M.B.702 (e) První oprávn ění B – G – 2 AMC M.A.702 (f) První oprávn ění B – G – 2 AMC M.A.702 (g) První oprávn ění B – G – 2 AMC M.B.703 (a) Vydání oprávn ění B – G – 2 0 – 3 Rozhodnutí č.
Recommended publications
  • 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.
    [Show full text]
  • 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, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber.
    [Show full text]
  • Annex III to Decision 2015/029/R
    AMC/GM TO ANNEX III (PART-66) TO REGULATION (EU) No 1321/2014 APPENDICES TO AMC TO PART-66 APPENDICES TO AMC TO PART-66 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 Regulation (EC) No 216/2008 and its Implementing Rules; this list is only intended for 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): — This Appendix I intends to include the type ratings of aircraft resulting from STCs for installation of another engine. These STCs are those approved by the Agency and those approved by the Member States before 2003 and grandfathered by the Agency.
    [Show full text]
  • 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.
    [Show full text]
  • Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights
    JOURNAL OF PROPULSION AND POWER Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights Daniele Cirigliano,∗ Aaron M. Frisch,† Feng Liu,‡ and William A. Sirignano‡ University of California, Irvine, California 92697 DOI: 10.2514/1.B36547 Comparisons are made for propulsion systems for unmanned flights with several hundred kilowatts of propulsive power at moderate subsonic speeds up to 50 h in duration. Gas-turbine engines (turbofans and turboprops), two- and four-stroke reciprocating (diesel and spark-ignition) engines, and electric motors (with electric generation by a combustion engine) are analyzed. Thermal analyses of these engines are performed in the power range of interest. Consideration is given to two types of generic missions: 1) a mission dominated by a constant-power requirement, and 2) a mission with intermittent demand for high thrust and/or substantial auxiliary power. The weights of the propulsion system, required fuel, and total aircraft are considered. Nowadays, diesel engines for airplane applications are rarely a choice. However, this technology is shown to bea very serious competitor for long-durationunmanned air vehicle flights. The two strongest competitors are gas-turbine engines and turbocharged four-stroke diesel engines, each type driving propellers. It is shown that hybrid-electric schemes and configurations with several propellers driven by one power source are less efficient. At the 500 KW level, one gas-turbine engine driving a larger propeller is more efficient for durations up to 25 h, whereas several diesel engines driving several propellers become more efficient at longer durations. The decreasing efficiency of the gas-turbine engine with decreasing size and increasing compression ratio is a key factor.
    [Show full text]
  • ATP® Libraries Catalog
    2 ATP® Libraries Catalog Revision Date May 24 2016 ATP 101 South Hill Drive Brisbane, CA 94005 (+1) 415-330-9500 www.atp.com ATP® Policies and Legal www.atp.com/policy © Copyright 2016, ATP. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted in any form by any means, electronic, mechanical, photocopying, recording or otherwise, without prior written permission of ATP. The information in this catalog is subject to change without notice.ATP, ATP Knowledge, ATP Aviation Hub, HubConnect, NavigatorV, and their respective logos, are among the registered trademarks or trademarks of ATP. All third-party trademarks used herein are the property of their respective owners and ATP asserts no ownership rights to these items. iPad and iPhone are trademarks of Apple Inc., registered in the U.S. and other countries. App Store is a service mark of Apple Inc. All original authorship of ATP is protected under U.S. and foreign copyrights and is subject to written license agreements between ATP and its subscribers. Visit www.atp.com/policy for more information ATP Customer Support Please visit www.atp.com/support for customer support information ATP® Libraries Catalog – Revision Date: May 24 2016 3 CONTENTS CONTENTS ...................................................................................................................................................................... 3 REGULATORY LIBRARIES .............................................................................................................................................
    [Show full text]
  • SFTE FTE Reference Handbook
    SFTE Reference Handbook Third Edition 2013 Society of Flight Test Engineers Reference Handbook Third Edition 2013 Page - i SFTE Reference Handbook Third Edition 2013 Society of Flight Test Engineers Reference Handbook 2013 Edition Corporate support supplied by Cessna Aircraft for printing the 2007 Edition And The National Test Pilot School Contributing Authors Al Lawless (sections 1-8, 10-12, 15, 18) Greg Lewis (section 2.6) Bill Norton (sections 9, 13) Dan Hrehov (section 14) Steven Arney (section 16) John Minor (section 19) David Kidman, Christopher Moulder, Craig Stevens (section 17) Edited by Lee Gardner & Darcy Painter 1998-2006 Harold Weaver 2006-2013 The SFTE handbook committee continually seeks corporate sponsors for this book and authors for new sections (including but not limited to INS, GPS, EMI/EMF, radar, avionics, R&M, E-O, human factors, orbital mechan- ics, armament) Page - ii SFTE Reference Handbook Third Edition 2013 Publication Policy Copyright (C) 2013 by Society Of Flight Test Engineers All rights reserved. This Technical Handbook is for the exclusive use of the Society of Flight Test Engineers individual and Corporate Members. The Technical information contained herein may not be reproduced by any other individual or organization in any form without writ- ten permission from the Society of Flight Test Engineers. The Society reserves the exclusive right of publication. For further information concerning the publication policy, write to: Society of Flight Test Engineers 44814 N. Elm Avenue Lancaster, California 93534 USA Or: Contact the Society of Flight Test Engineers through their web site at www.sfte.org. Please submit corrections or additions to SFTE Handbook Committee 44814 N.
    [Show full text]
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • THE AERO INDIA ISSUE Safran I/ 2015 I/ 2015 Aerospace & Defence Review
    I/ 2015 Aerospace & Defence Review AERO INDIA 2015 THE AERO INDIA ISSUE Safran I/ 2015 I/ 2015 Aerospace & Defence Review The Indian source’ assessment of the LCA’s status, In an interview with General Dalbir Singh, 42 with a no–holds bar examination of this the Indian Army COAS enumerates Aerospace Riddle light fighter programme. Focus must his vision and focus areas for the Indian be on weight reduction improvement Army, including plans for integrating which is the key as also some re-designs attack helicopters in the combined arms including lengthening of the fuselage and environment. tweaking of the wing. AERO INDIA 2015 Airbus A350XWB THE AERO INDIA ISSUE Thunder from the 94 VAYU Cover I-2015.indd 3 06-02-2015 11:59:31 71 to Qatar Airways Artist’s impression of IAF Su-30MKIs conducting an Air Marshal Brijesh Jayal writes on the North-West (of India) air strike as a pair of Tejas LCAs provide top cover. ‘riddle’ where ‘aerospace shines and The Su-30MKI is the IAF’s primary combat aircraft, aeronautics whines!’ Even while feat of while the Tejas LCA has recently been accepted into the Mars Orbiter Mission, Mangalyaan service. Both aircraft types are on display at Aero India 2015 (Digital art by Priyanka Joshi) has impressed the world, the country struggles to develop basic training aircraft. EDITORIAL PANEL A contrasting look at the Sino-Pakistani MANAGING EDITOR Aerospace Power JF-17 Thunder light fighter which Vikramjit Singh Chopra 46 development programme began in Vayu was present at Toulouse when the in the 21st Century 1999 and one which has ‘over taken’ EDITORIAL ADVISOR first Airbus A350XWB was handed over the LCA in terms of clearance for Admiral Arun Prakash to Qatar Airways.
    [Show full text]
  • Comprehensive and Cost-Effective Global Coverage for the TPE331 Honeywell Aerospace 1944 E
    A60-0942-000-001 TPE331:Layout 1 7/16/2007 3:29 PM Page 1 TPE331 Maintenance Service Plan Find out more Honeywell Aerospace Business & General Aviation 23, Rue du 19 Mars 1962 92230 Gennevilliers France Phone: 33 (0) 1 40 80 59 11 Mobile: 33 (0) 6 32 55 06 08 Fax: 33 (0) 1 40 80 59 67 e-mail: [email protected] Comprehensive and cost-effective global coverage for the TPE331 Honeywell Aerospace 1944 E. Sky Harbor Circle turboprop engine Phoenix, AZ 85034 Toll Free: 1-800-601-3099 International: 602-365-3099 A60-0942-000-001 July 2007 www.honeywell.com © 2007 Honeywell International Inc. A60-0942-000-001 TPE331:Layout 1 7/16/2007 3:29 PM Page 3 Honeywell’s MSP...Extended Coverage COVERED ITEMS NON-COVERED ITEMS Scheduled Maintenance Routine Inspection S.O.A.P. kit and analysis (if obtained from an Authorized Service Center) Routine periodic inspection labor Hot Section Inspection (HSI) by an Authorized Major Service Center MSP Operator Advantages Enhanced aircraft resale value: Inspection labor Consumable parts The TPE331 MSP Program is available to executive/corporate Accrued engine value transferable to new owner Other required parts operators of Honeywell TPE331-5/-6/-8/-10/-11/-12 or -14 Component repair labor (if required) Aircraft value not reduced due to engine repairs powered aircraft. No other maintenance program offers such Cycle life-limited parts comprehensive coverage at an affordable price. With the Enhanced aircraft value offsets program cost Engine removal and reinstallation and/or access time flexibility of receiving service at over 125 authorized service Gearbox Inspection (GBI) by an Authorized Major Service Center centers worldwide, you receive the most up-to-date service Honeywell’s MSP .
    [Show full text]
  • 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.
    [Show full text]