Offset Management a Case Study of Saab AB
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Technical Supplements
Technical Supplements S1 The IG JAS Investment In this Technical Supplement the JAS 39 Gripen product concept is outlined, the procurement process documented, the Industry Group IG JAS presented and the critical role of the competent public procurement agency, the FMV, highlighted. S1.1 The Procurement of the JAS 39 Gripen Aircraft with Swing-Role Capabilities The JAS 39 Gripen multirole combat aircraft (J stands for fighter, A for Attack and S for Surveillance/reconnaissance) is a fourth generation aircraft that entered operational service in 1997. It replaced the Viggen, the last of which was taken out of service in 2006. JAS 39 Gripen is a combat aircraft with swing-role capabilities that can change mission in flight. This swing-role capability was unique when Gripen was launched but has later been introduced on the French Rafale and the Eurofighter. Other competing multirole aircraft first have to land to reconfigure its information, guidance, and weapons systems for a new role. Gripen was the first “unstable” aircraft in the world which meant that in order for the aircraft to be stable at all speeds and in all maneuvers many more navigation surfaces are needed than the pilot can possibly control himself to minimize air friction at each moment. He needs incredibly sophisticated computer systems support to maneuver the aircraft effectively and safely. Competing fourth generation combat aircraft are F-35/JSF (the USA, not yet (2009) delivered to market), the Eurofighter Typhoon (the UK, etc.) and Rafale (Dassault, France). JAS 39 Gripen also competes with upgraded versions of the third generation aircraft of Lockheed Martin F-16 (the USA, first delivered in 1978), Boeing F/A18 Hornet (the USA, first delivered in 1983), Dassault Mirage 2000 (France, first delivered in 1983), and Mig-29 (the former Soviet Union, first delivered in 1977). -
Saab AB, Saab Aerosystems Airplanes
Federal Register / Vol. 77, No. 98 / Monday, May 21, 2012 / Rules and Regulations 29855 Issued in Washington, DC, on May 15, § 609.10 Loan Guarantee Agreement. Engineer, International Branch, ANM– 2012. * * * * * 116, Transport Airplane Directorate, David G. Frantz, (d) * * * FAA, 1601 Lind Avenue SW., Renton, Acting Executive Director, Loan Programs (17) If Borrower is to make payment Washington 98057–3356; telephone Office. in full or in part for the Credit Subsidy (425) 227–1112; fax (425) 227–1149. For the reasons set forth in the Cost of the loan guarantee pursuant to SUPPLEMENTARY INFORMATION: preamble, DOE hereby amends Part 609 section 1702(b)(2) of the Act, such Discussion of chapter II of title 10 of the Code of payment must be received by DOE prior Federal Regulations as set forth below: to, or at the time of, closing; We issued a notice of proposed * * * * * rulemaking (NPRM) to amend 14 CFR PART 609—LOAN GUARANTEES FOR [FR Doc. 2012–12218 Filed 5–18–12; 8:45 am] part 39 to include an AD that would PROJECTS THAT EMPLOY BILLING CODE 6450–01–P apply to the specified products. That INNOVATIVE TECHNOLOGIES NPRM was published in the Federal Register on February 28, 2012 (77 FR ■ 1. The authority citation for part 609 DEPARTMENT OF TRANSPORTATION 11791). That NPRM proposed to correct continues to read as follows: an unsafe condition for the specified Authority: 42 U.S.C. 7254, 16511–16514. Federal Aviation Administration products. The MCAI states: ■ 2. In § 609.8 revise paragraph (d) to Environmentally friendly de-/anti-icing 14 CFR Part 39 read as follows: agents (acetates or formats) are a known [Docket No. -
Federal Register/Vol. 84, No. 127/Tuesday, July 2, 2019
31526 Federal Register / Vol. 84, No. 127 / Tuesday, July 2, 2019 / Proposed Rules and Airworthiness Division, but during (d) Subject Transport Standards Branch, FAA; or the this transition period, the Executive Air Transport Association (ATA) of European Aviation Safety Agency (EASA); or Director has delegated the authority to America Code 54, Nacelles/pylons. Saab AB, Saab Aeronautics’ EASA Design issue ADs applicable to transport Organization Approval (DOA). If approved by (e) Reason category airplanes and associated the DOA, the approval must include the DOA-authorized signature. appliances to the Director of the System This AD was prompted by reports of loose Oversight Division. and irregular fasteners at the forward end of (j) Related Information the nacelle upper longeron, where the Regulatory Findings bulkhead frame and struts are attached to the (1) Refer to Mandatory Continuing engine mounting structure (EMS). The FAA Airworthiness Information (MCAI) EASA AD The FAA determined that this is issuing this AD to address loose and 2019–0054, dated March 18, 2019, for related proposed AD would not have federalism irregular fasteners of the EMS which could information. This MCAI may be found in the implications under Executive Order cause development of cracks in the EMS, AD docket on the internet at http:// 13132. This proposed AD would not leading to failure of the affected engine www.regulations.gov by searching for and have a substantial direct effect on the mount-to-airplane structural connection, locating Docket No. FAA–2019–0520. States, on the relationship between the possibly resulting in significant airframe (2) For more information about this AD, vibrations and detrimental effects on the contact Shahram Daneshmandi, Aerospace national Government and the States, or Engineer, International Section, Transport on the distribution of power and surrounding pylon/nacelle structure, and loss of structural integrity. -
Offsets in the Aerospace and Defence Industry
Offsets in the Aerospace and Defence Industry 1 Table of Contents 1 Introduction ..................................................................................................... 4 1.1 IFBEC and the Basel Institute on Governance .......................................................................... 5 2 Definitions and Context ................................................................................. 7 2.1 Definitions of offset ................................................................................................................................... 7 2.2 Some specific elements of offset programmes ......................................................................... 9 2.2.1 Valuation Methods .............................................................................................................................. 9 2.2.2 Excess credits and banking ......................................................................................................... 10 2.2.3 Offset credit swapping .................................................................................................................... 11 2.2.4 Financial penalties for companies ........................................................................................... 11 2.3 Size of the defence market ............................................................................................................... 11 2.4 Size of offset programmes ............................................................................................................... -
Saab 340, Saab 2000
TRANSPARENCY BULLETIN SPRING 2009 COCKPIT WINDOWS Saab 340, Saab 2000 Main Windshield Features Benefits All-Glass Design • Chemical, abrasion, scratch resistance • Uniform thermal expansion for greater resistance to delamination • Better fit in the airframe Herculite ® II Glass by PPG • High strength-to-weight ratio • Lightweight window • Greater hardness • Less deflection Superior Optical Quality • Safety Copyright Saab AB • Enhanced visibility PPG Aerospace – Transparencies is a leading and experi- Nesatron ® Anti-ice System • Excellent heating uniformity enced manufacturer of replacement windshields and side • Optical clarity cockpit windows for Saab 340 and Saab 2000 airplanes. • No burnout from electrical hot spots OEM Manufacturer • Latest design configuration and upgrades The PPG windshields and cockpit windows are constructed • Fully approved by Saab for the of three glass plies for unmatched durability, exceptional fit manufacture and supply of spares to in the airframe and greater resistance to delamination. The operators design takes advantage of the inherent benefits of glass to • Proven reliability provide superior chemical, abrasion and scratch resistance PPG 112 Interlayer • Provides maximum adhesion to glass on inboard and outboard surfaces as well as optical clarity. for increased resistance to delamination Herculite® II chemically strengthened glass by PPG is used and extends service life for its high strength-to-weight ratio to produce a durable • Elasticity at low temperatures dramatically reduces potential for cold transparency that is comparable in weight to acrylic. The chipping all-glass designs meet the challenging operating environment for the Saab 340 and Saab 2000 airplanes. Side Cockpit Window Features Benefits Operators know they can count on PPG Aerospace for All-Glass Design • Chemical, abrasion, scratch resistance transparencies that provide significant value because of their • Uniform thermal expansion for greater reduced life-cycle cost as a result of their service life. -
Docket No. FAA-2020-0855; Project Identifier MCAI-2020-00909-T]
This document is scheduled to be published in the Federal Register on 10/01/2020 and available online at federalregister.gov/d/2020-21544, and on govinfo.gov [4910-13-P] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2020-0855; Project Identifier MCAI-2020-00909-T] RIN 2120-AA64 Airworthiness Directives; Saab AB, Support and Services (Formerly Known as Saab AB, Saab Aeronautics) Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) for all Saab AB, Support and Services Model SAAB 2000 airplanes. This proposed AD was prompted by a report of inadvertently reversed connections of the outboard and inboard channel harnesses of the wheel speed transducers in the main landing gear (MLG) wheel axles. This proposed AD would require an inspection for correct installation of the MLG anti-skid system harnesses and corrective actions if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which will be incorporated by reference. The FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this proposed AD by [INSERT DATE 45 DAYS AFTER DATE OF PUBLICATION IN THE FEDERAL REGISTER]. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: 202-493-2251. • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. -
The Case of Saab Automobile AB from Core Capabilities Into Core Rigidities - a Trajectory Towards Demise
Master Degree Project in Knowledge-based Entrepreneurship The case of Saab Automobile AB From core capabilities into core rigidities - A trajectory towards demise Giacomo Buzzoni and Magnus Eklund Supervisor: Evangelos Bourelos Master Degree Project No. 2016:148 Graduate School The Case of Saab Automobile AB From Core Capabilities into Core Rigidities - A Trajectory Towards Demise © Giacomo Buzzoni & Magnus Eklund School of Business, Economics and Law, University of Gothenburg, Vasagatan 1, P.O. Box 600 SE 40530 Gothenburg, Sweden All rights reserved No part of this master thesis may be reproduced without prior written permission from the authors Acknowledgements First of all, we would like to thank our supervisor Evangelos Bourelos for his patience and effort in providing us with meaningful advice throughout these months of intense research. We would also like to express our appreciation and gratitude towards all our respondents who have allocated their valuable time to help us interpret this interesting case. Your passion, knowledge and commitment guided us through this journey, and we have enjoyed every single day of it. Finally, we would like to thank our peer students and all the people close to us for your support during our years of university studies. Without you, this would not have been possible. ABSTRACT This master thesis is addressing the case of Saab Automobile AB, creating a full historical reconstruction using primarily extensive quotes derived from semi-structured interviews with former Saab employees and other relevant actors. The aim is to depict and discuss the roots behind the company’s historically unique capabilities and its trajectory towards failure, together with the influence of General Motors’ ownership in this detrimental process. -
Study on the Effects of Offsets on the Development of a European Defence Industry and Market
Final Report of 06-DIM-022 Study on the effects of offsets on the Development of a European Defence Industry and Market By E. Anders Eriksson with contributions by Mattias Axelson, Keith Hartley, Mike Mason, Ann-Sofie Stenérus and Martin Trybus 12 July 2007 2007-07-12 Final report of 06-DIM-022 LIST OF CONTENTS Executive summary............................................................................................................................... 3 1 Introduction................................................................................................................................... 9 1.1 Understanding the assignment: our working hypotheses ................................................................ 9 1.2 Delimitation of study..................................................................................................................... 10 1.3 Protection of respondents and data................................................................................................ 11 1.4 Outline of report............................................................................................................................ 11 1.5 The FOI/SCS team ........................................................................................................................ 11 2 Offset conceptual framework .................................................................................................... 13 2.1 Offset taxonomy used in the study............................................................................................... -
Theorem Dimas Irion Alves , Bruna Gregory Palm , Hans Hellsten, Senior Member, IEEE, Viet Thuy Vu , Senior Member, IEEE, Mats I
5560 IEEE JOURNAL OF SELECTED TOPICS IN APPLIED EARTH OBSERVATIONS AND REMOTE SENSING, VOL. 13, 2020 Wavelength-Resolution SAR Change Detection Using Bayes’ Theorem Dimas Irion Alves , Bruna Gregory Palm , Hans Hellsten, Senior Member, IEEE, Viet Thuy Vu , Senior Member, IEEE, Mats I. Pettersson , Renato Machado , Member, IEEE, Bartolomeu F. Uchôa-Filho , Senior Member, IEEE, and Patrik Dammert, Senior Member, IEEE Abstract—This article presents Bayes’ theorem for wavelength- acquisitions separated in time can be found in SAR images with resolution synthetic aperture radar (SAR) change detection method a change detection method. development. Different change detection methods can be derived Among these applications, it is possible to highlight the using Bayes’ theorem in combination with the target model, clutter-plus-noise model, iterative implementation, and nonitera- detection of concealed targets in foliage-penetrating (FOPEN) tive implementation. As an example of the Bayes’ theorem use for applications, which has been of great interest for a long time [5]. wavelength-resolution SAR change detection method development, However, when change detection is employed in conventional we propose a simple change detection method with a clutter-plus- microwave SAR images for FOPEN applications, a large number noise model and noniterative implementation. In spite of simplicity, of false alarms are observed. Ultrahigh frequency and very high the proposed method provides a very competitive performance in terms of probability of detection and false alarm rate. The best frequency SAR systems are excellent options to overcome this result was a probability of detection of 98.7% versus a false alarm limitation [5]. rate of one per square kilometer. -
Federal Register/Vol. 86, No. 33/Monday, February 22, 2021
Federal Register / Vol. 86, No. 33 / Monday, February 22, 2021 / Rules and Regulations 10447 Manager, Seattle ACO Branch, FAA, to make Issued on December 30, 2020. www.regulations.gov by searching for those findings. To be approved, the repair Lance T. Gant, and locating Docket No. FAA–2020– method, modification deviation, or alteration Director, Compliance & Airworthiness 0855. deviation must meet the certification basis of Division, Aircraft Certification Service. Examining the AD Docket the airplane, and the approval must [FR Doc. 2021–01823 Filed 2–19–21; 8:45 am] specifically refer to this AD. You may examine the AD docket on BILLING CODE 4910–13–P (4) For service information that contains the internet at https:// steps that are labeled as Required for www.regulations.gov by searching for Compliance (RC), the provisions of DEPARTMENT OF TRANSPORTATION and locating Docket No. FAA–2020– paragraphs (k)(4)(i) and (ii) of this AD apply. 0855; or in person at Docket Operations (i) The steps labeled as RC, including Federal Aviation Administration between 9 a.m. and 5 p.m., Monday substeps under an RC step and any figures through Friday, except Federal holidays. identified in an RC step, must be done to 14 CFR Part 39 The AD docket contains this final rule, comply with the AD. If a step or substep is any comments received, and other labeled ‘‘RC Exempt,’’ then the RC [Docket No. FAA–2020–0855; Project information. The address for Docket requirement is removed from that step or Identifier MCAI–2020–00909–T; Amendment 39–21385; AD 2021–02–02] Operations is U.S. -
Defence Offsets Addressing the Risks of Corruption & Raising Transparency
DEFENCE OFFSETS ADDRESSING THE RISKS OF CORRUPTION & RAISING TRANSPARENCY www.defenceagainstcorruption.org www.transparency.org Transparency International (TI) is the civil society organisation leading the global fight against corruption. Through more than 90 chapters worldwide and an international secretariat in Berlin, Germany, TI raises awareness of the damaging effects of corruption, and works with partners in government, business and civil society to develop and implement effective measures to tackle it. For more information go to: www.transparency.org TI’s international defence programme, Defence Against Corruption (DAC) helps to build integrity and reduce corruption in defence and security establishments worldwide through supporting counter-corruption reform in nations, raising integrity in arms transfers, and influencing policy in defence and security. To achieve this, the DAC team works with governments, defence companies, multilateral organisations and civil society. DAC is led by Transparency International-UK on behalf of the TI movement. Information on Transparency International’s work in the defence and security sector to date, including background, overviews of current and past projects, and publications, is available on TI’s Defence Against Corruption website, www.defenceagainstcorruption.org First published April 2010 Publisher: Transparency International-UK Acknowledging the debt Transparency Authors: Ben Magahy, Francisco Vilhena International-UK (TI-UK) owes to all those Reproduction in whole or in parts is da Cunha and Mark Pyman. who have contributed to and collaborated permitted, providing that full credit is Editing : Julia Muravska and in the preparation of this publication, given to Transparency International-UK, Anne-Christine Wegener. we should make clear that TI-UK alone and provided that any such reproduction, Design: www.onehemisphere.se is responsible for the content of the whether in whole or in parts, is not sold document. -
Offsets in Defense Trade Eleventh Report to Congress
Offsets in Defense Trade Eleventh Report to Congress January 2007 U.S. Department of Commerce Bureau of Industry and Security Offsets in Defense Trade Eleventh Study Conducted Pursuant to Section 309 of the Defense Production Act of 1950, as Amended U.S. Department of Commerce Bureau of Industry and Security Office of Strategic Industries and Economic Security January 2007 For more information, please contact the Office of Strategic Industries and Economic Security at 202-482-4506 www.bis.doc/osies i Table of Contents EXECUTIVE SUMMARY ............................................................................................................iii 1 BACKGROUND ..................................................................................................................1-1 1-1 STATUTES AND REGULATIONS.........................................................................................1-1 1-2 U.S. GOVERNMENT POLICY ............................................................................................1-2 1-3 OFFSETS TERMINOLOGY .................................................................................................1-3 1-4 COUNTRIES AND REGIONS..............................................................................................1-5 1-5 SCOPE OF REPORT..........................................................................................................1-6 2 STATISTICAL OVERVIEW ..................................................................................................2-1 2-1 GENERAL OVERVIEW.......................................................................................................2-1