DOCSLIB.ORG

Minor Change / Minor Repair Easa.Europa.Eu

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Minor Change / Minor Repair Easa.Europa.Eu Minor Change / Minor Repair easa.europa.eu EASA Rev. Associated Technical Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation Issue Number 10073014 MINOR CHANGE 21JAERODESIGN CFM56-3 VSV System - Installation of Feedback The Certification Basis for the original Design Change Document None 15/04/2020 Active LIMITED Coupling.Replacement VSV Feedback product as amendedby thefollowing DCD-0112M issue 1, 19 Mar Coupling P/N 2028M21P01AP for the additional or alternative 2020<(>,<)>Aircraft Manual CFM56-3C-1Engine. airworthiness requirements:the Supplement: AMS-ALL- following paragraph(s) at a later CFM56-3-EIPC Rev 1, 19 Mar amendment: CS-E amdt 5 paras: 2020or later revisions of the 10,20, 25, 50, 90, 100, 110, 510.The above listed document(s) requirements for environmental approved/acceptedunder the protection and the associatedcertif... EASA system. 10073411 MINOR CHANGE ADANAIR S.L. P.68 "OBSERVER" Installation of ASIVE CONSOLE in the interior The Certification Basis (CB) for the MASTER DATA LIST MDL001- Prior to installation of this change/ 05/06/2020 Active of Vulcanair P.68 ObserverThe modification original product remains applicableto Revision 1<(>,<)>Or later repair it must be determined involves the introduction in aircraft this certificate/ approval.The revisions of the above listed thatthe interrelationship between PARTENAVIAS P68of a console for reading of requirements for environmental document(s) approved/ this change/repair and any radio signals in a determined GPS protection and the acceptedunder the EASA otherpreviously installed change position.These signals will be usedfor associatedcertified noise and/ or system. and/ or repair willintroduce no checking the accuracy of ground emissions levels of the product are adverseeffect upon the equipmentcalibration. unchangedand remain applicable to airworthiness of the product. this certificate/approval without any im... 10077231 MINOR CHANGE ADANAIR S.L. B200 Installation of an ASIVE CONSOLE for The Certification Basis (CB) for the Installed and maintained in This design change only covers the 09/09/2021 Active calibration of external instruments original product remains applicableto accordance with ASIVE SB002 installation of the this certificate/ approval.The Revision 1<(>,<)>or later SIVEconsole,wiring and antennas requirements for environmental revisions of the above listed are installed in accordance with protection and the document(s) approved/ STC EASA 10077176.The approval associatedcertified noise and/ or acceptedunder the EASA holder shall fulfill the obligations emissions levels of the product are system. of Part 21, Point21A.109.Prior to unchangedand remain applicable to installation of this change/repair it this certificate/approval without any must be determined thatthe im... interrelatio... 10072968 MINOR CHANGE AERO AT Sp. z.o.o. AT-3R100 Removal of the errors noted in AFM The Certification Basis for the original Revision No 24 dated 04.03 None 03/04/2020 Active product remains applicable tothis 2020 to Airplane Flight certificate/ approval.The Manual (AFM) Doc. requirements for environmental NoATL3.03 (Polish language protection and the version) and Doc. No ATL3.04 associatedcertified noise and/ or (English languageversion)< emissions levels of the product are (>,<)>Or later revisions of the unchangedand remain applicable to above listed document(s) this certificate/ approval without any approved/acceptedunder the impact... EASAsystem. 10075129 MINOR CHANGE AEROCLUB LOUIS DR 400/140 B Avionics upgrade on DR 400/140B aircraft S/ The Certification Basis for the original Definition of modification in This modification only applies to 10/12/2020 Active BONTE N 2086Installation of Garmin GTN650 and product as amendedby thefollowing accordance with section 3 of aircraft S/N 2086.The approval related modifications for VFRoperations additional or alternative ACLB_MC_001Revision holder shall fulfill the obligations airworthiness requirements:- The 1.1Installation in accordance of Part 21, Point21A.109. following paragraph(s) at a later with section 4 of amendment:23.1301(a),23.1301(b), ACLB_MC_001 Revision 23.1301(c), 23.1301(d), 23.1309(e), 1.1Instruction for continued 23.1361(a), 23.1365,23.1367(d), airworthiness in accordance 23.1431(b), 23.1519 from CS23... with section 5 ofACLB_MC_001 Revision 1.1Operation in accordance with section 6 and Appendix 1R... 10074228 MINOR CHANGE AERO CLUB PA-28-181 (ARCHER III) Installation of four (4) Cylinder Head The Certification Basis (CB) for the Minor change description F- This design change approval does 10/09/2020 Active NATIONAL DU Temperature (CHT) and Exhaust original product remains applicableto GYNN, compiled by Patrick not allow replacement of PERSONNELDES GasTemperature (EGT) probes along with this certificate/ approval.The Bezault, Revision0, dated 9 existingengine instruments.This INDUSTRIES cabling anda circuit breaker tosupport requirements for environmental September 2020or later design change approval excludes ELECTRIQUE ET installation of a graphic engine monitoring protection and the revisions of the above listed installation of any graphic GAZIER(ANEG) instrument. associatedcertified noise and/ or document(s) approved/ enginemonitoring emissions levels of the product are acceptedunder the EASA instrument.Graphic engine unchangedand remain applicable to system. monitoring instrument may be this certificate/approval without any installed if specificallyapproved by im... an EASA design approval or allowed by CS-... This report lists certificates issued during the period 01/01/2020 until 28/09/2021. In case you need a certificate not included, please contact [email protected]. Page 1 of 62 An agency of the European Union Minor Change / Minor Repair easa.europa.eu EASA Rev. Associated Technical Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation Issue Number 10073818 MINOR CHANGE AERODESIGN AND ATR 72-212 A Installation of TELEX boomsets in ATR72 The Certification Basis for the original INSTALLATION INSTRUCTIONS The approval holder shall fulfill the 16/07/2020 Active MANUFACTURINGTE Cockpit for the observer seat product remains applicable tothis MOBT-1828-INS01, Revision obligations of Part 21, Point21.A. CHNOLOGY S.L. certificate/ approval.The 3CMM SUPPLEMENT 109.Prior to installation of this requirements for environmental MOBT-1828-CMMS01 change/repairit must be protection and the Revision 1Or later revisions of determined thatthe associatedcertified noise and/ or the above listed document(s) interrelationship between this emissions levels of the product are approved/acceptedunder the change/repair and any unchangedand remain applicable to EASA system. otherpreviously installed change this certificate/ approval without any and/ or repair will introduce no impact... adverseeffect upon the airworth... 10077177 MINOR CHANGE AERODESIGN AND ATR 72-212 A Introduction of Alternative Boomsets for the The Certification Basis for the original MASTER DATA LIST This approval is only applicable to 02/09/2021 Active MANUFACTURINGTE ATR 72-212 Flight Crew product remains applicable tothis MOBT-2015-MDL Rev.01 the following Aiprlanes:AIRPLANES CHNOLOGY S.L. ATR 72-211 certificate/ approval.The (31/08/2021)Or later ATR 72 Series; MSN 234, 171, 192, ATR 72-202 requirements for environmental revisions of the above listed 204, 207, 330, 416, 147,150, 274, ATR 72-201 protection and the document(s) approved/ 446, 494, 498, 550, 568, 595, 763, associatedcertified noise and/ or acceptedunder the EASA 809, 824AIRPLANES ATR 42 Series; emissions levels of the product are system. MSN 141, 218, 231, 242, 254, 321 unchangedand remain applicable to (ATR-42)The approval holder shall this certificate/ approval without any fulfill the obligations of2... impact... 10072386 MINOR CHANGE AERO ENGINEERING ATR 72-212 A Owner and Registration Plates Installation The Certification Basis for the original - Project Opening Sheet ATR 42 and ATR 72 all MSN.The 05/02/2020 Active SERVICES ATR 72-101/-102/-211/-212 product as amendedby thefollowing P00968-POS-001 Revision 00 approval holder shall fulfillthe ATR additional or alternative dated 04February2020- obligations of Part 21, Point21A. 42-200/-300/-320/-400/-500 airworthiness requirements:The Certification Report P00968- 109.Prior to installation of this following paragraph(s) at a later CR-001 Revision 00 dated 04 change/repair it must be amendment: CS 25 Amdt 4 - CS25.29; February 2020- Master Data determined thatthe CS 25.561(b); CS 25.603; CS 25.1529; List P00968-MDL-001 Revision interrelationship between this CS 25.1541 and CS 25.1557(b)& (c) 00 dated 04 February 2020- change/repair and any The requirements for environ... Service Bulletin P00968- otherpreviously installed change SB-001 Revision 00 dated 04 and/ or repair will introduce no February 2020or later advers... revisions ofu... 10073317 MINOR CHANGE AERO ENGINEERING CL-600-2E25 (RJ SERIES 1000) Live Animals Cargo Stowage Installation The Certification Basis for the original - Project Opening Sheet CL-600-2C10 MSN 10032; 10036; 29/05/2020 Active SERVICES CL-600-2C10 (RJ 700, 701, product as amendedby thefollowing P00592-POS-001 Revision 00 10037; 10089; 10093; 10096; 702) additional or alternative dated 19May 2020- Service 10198; 10245;10263 to 10265 airworthiness requirements:The Bulletin P00592-SB-001 included, and<(>,<)>CL-600-2E25
Load more

Recommended publications
  • FLARM: Collision Threat Identification Influenced by Pilot’S Mental Model of the Cockpit Display
    FLARM: Collision Threat Identification Influenced by Pilot’s Mental Model of the Cockpit Display Christoph G. Santel Uwe Klingauf [email protected] [email protected] Institute of Flight Systems and Automatic Control Technische Universitat¨ Darmstadt Darmstadt, Germany Abstract During the last decade, low-cost collision alerting systems have become available to assist glider pilots in their task of seeing and avoiding other traffic. These systems present pilots with traffic information on different displays. Previous work by the authors shows that many glider pilots make systematic errors in interpreting traffic information shown on one such display, the popular FLARM display. This is the case whenever the pitch angle, bank angle or drift angle deviate from zero. In this paper data from the aforementioned research are analyzed using analytical modeling of the pilots’ mental models in order to explain these systematic errors. Results show that the majority of glider pilots rely on a glider-fixed reference system when interpreting the traffic indications on the FLARM display. This is attributed to the available in-cockpit clues on the display. Since the data displayed on the FLARM display are actually derived from a FLARM-specific coordinate system — and is not glider-fixed — it is only natural that many pilots make systematic errors in predicting the position of traffic shown on the display. At the end of the paper possible courses of action to reduce these interpretation errors are discussed. Introduction Gliding is an air sports activity that is mostly carried out un- ρ der visual flight rules. Consequently, in most airspace classes glider pilots are responsible for visually detecting and avoiding other traffic [1, section 2.6].
    [Show full text]
  • Skyecho 2 User and Installation Guide REV H-AIC
    SkyEcho 2 Installation and Pilot’s Guide UAV-1002156-001 ECCN 7A994 Page 1 | 33 © 2019 uAvionix Corporation. All rights reserved. uAvionix Corporation 300 Pine Needle Lane Bigfork, MT 59911 http://www.uavionix.com [email protected] Except as expressly provided herein, no part of this guide may be reproduced, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of uAvionix. uAvionix grants permissions to download a single copy of this guide onto an electronic storage medium to be viewed for personal use, provided that the complete text of this copyright notice is retained. Unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. uAvionix® is a registered trademark of uAvionix Corporation, and may not be used without express permission of uAvionix. UAV-1002156-001 ECCN 7A994 Page 2 | 33 1 Revision History Revision Date Comments A 8/8/18 Pre-transmit release of SE2. ADS-B only B 8/28/18 Mode C/S Bearingless Targets, DoCC Approval C 9/11/18 User feedback corrections D 12/24/18 FLARM Functionality E 02/09/19 Regional Setting F 05/21/19 Removal of Mode C/S Bearingless Targets G 10/26/19 Firmware Update Procedures / Removal of FlarmBridge H 12/12/19 Review for AIC publication UAV-1002156-001 ECCN 7A994 Page 3 | 33 2 Warnings / Disclaimers All device operational procedures must be learned on the ground. Received traffic information is to be used as an aid to situational awareness and is merely supplemental and advisory in nature.
    [Show full text]
  • FLARM Aircraft Flight Manual Supplement
    Date: 2020-10-28 Version: 1.0 AIRCRAFT FLIGHT Page: 1 of 19 FLARM Technology Ltd MANUAL SUPPLEMENT Document Number: Hinterbergstrasse 15 FTD-085-AFMS CH-6330 Cham FLARM COLLISION AVOIDANCE SYSTEM Registration: SE-ICL Date: 2021-03-26 Manufacturer Type Serial No. Aircraft PIPER AIRCRAFT, INC. PA-28 28-7990371 PowerFLARM FLARM Display This document must be carried in the aircraft at all times. It describes the operating procedures with FLARM installed. This supplement must be attached to the approved Aircraft Flight Manual. The information contained in this document supplements or supersedes the basic manual only in those areas listed. For limitations, procedures, performance, and loading information not contained in this supplement, consult the original Aircraft Flight Manual. This supplement is only approved for the individual aircraft listed above. The supplement can be validated by scanning the QR Code below. https://flarm.com/validate/3be9461b This Flight Manual Supplement is EASA approved. Approval Number: 10074703 Date of issue: 30 October 2020 Copyright © 2020 FLARM Technology Ltd. Date: 2020-10-28 Version: 1.0 AIRCRAFT FLIGHT Page: 2 of 19 FLARM Technology Ltd MANUAL SUPPLEMENT Document Number: Hinterbergstrasse 15 FTD-085-AFMS CH-6330 Cham Log of Revisions Ver. Date Summary of changes 1 2020-10-28 Initial version Copyright Notice Copyright © 2020 FLARM Technology Ltd. All rights reserved. Content may not be reproduced, downloaded, disseminated, published, or transferred in any form or by any means, except with the prior written permission of FLARM Technology Ltd. Copyright infringement is a violation of federal law subject to criminal and civil penalties.
    [Show full text]
  • Instructions for Continued Airworthiness
    Date: 2020-09-15 INSTRUCTIONS FOR Version: 1.0 CONTINUED Page: 1 of 24 FLARM Technology Ltd Document Number: Hinterbergstrasse 15 AIRWORTHINESS FTD-073 CH-6330 Cham Document status Published status Confidentiality status ☐ Draft ☐ Internal ☒ Released ☐ NDA ☐ Canceled ☒ Public Version control Ver. Date Summary of changes 1.0 2020-09-15 Initial version Scope and summary This Instructions for Continued Airworthiness (ICA) is intended to be used by entities responsible for the continuing airworthiness of aircraft with a FLARM system installed. It is also intended to be used by owners of portable FLARM devices. This document is general in scope and is applicable to all FLARM installations and devices listed herein. FLARM, as all radio equipment, requires considerate care and maintenance for continued high performance. Failure to comply with this ICA may lead to the FLARM system deteriorating in performance or becoming inoperable. Date: 2020-09-15 INSTRUCTIONS FOR Version: 1.0 CONTINUED Page: 2 of 24 FLARM Technology Ltd Document Number: Hinterbergstrasse 15 AIRWORTHINESS FTD-073 CH-6330 Cham Table of contents 1 Introduction ...................................................................................... 3 1.1 Purpose ................................................................................. 3 1.2 Scope .................................................................................... 3 1.3 Checklists ............................................................................... 3 1.4 Definitions .............................................................................
    [Show full text]
  • FLARM® As an Additional Tool When Searching a Missing Aircraft
    German text starts on page 5! FLARM® as an additional tool when searching a missing aircraft FLARM determines the aircraft’s position based on GPS and continually broadcasts its position and a device-specific identification-number (ID) to other nearby aircraft equipped with FLARM. This works within a distance of few kilometers. Based on real-time analysis of these data the nearby traffic can be displayed and approaching aircraft can be warned. This is the main functionality of FLARM. FLARM, furthermore, records the flight-log and makes it available in the so-called IGC-file. This file is analyzed in competitions by the organizer. It can also be up-loaded by the pilot at server-services such as Netcoupe, SIS-AT, SkyLines, XContest or OLC. FLARM- and PowerFLARM-devices (incl. Ediatec ECW-100, OzFlarm, MiniOz, LX-MiniBox, LX-RedBox, LX8***/LX9***, FlarmMouse, FAT201 (requires firmware v3 or higher, and the Flight Recorder setup must have “log other aircraft data” activated), Floice; not yet LX- Colibri, LX7***, Flytec, Bräuniger, Somax, Garrecht, AirAvionics, ISU, Oudie, PDA- applications) not only record one’s-own flight track in the IGC-file but also the clocked 3D- vectors and the IDs of received FLARM-data broadcasts of other aircraft. This means that aircraft that have been flying nearby for shorter or longer spans leave their traces in the FLARM’s IGC-file. These data are available for 3rd-party manufactures in the serial port as a PFLAL-command (for details see Data Port Specifications). The reason for this recording is that thereby the pilots get the opportunity to check the quality of their FLARM-installations – in particular of the transmitter/receiver and of the antennae – therefore, they up-load an IGC-file under flarm.com/support/tools- software/flarm-range-analyzer/ .
    [Show full text]
  • Scottish Gliding Union Flarm Trial
    Flarm Trial – Portmoak 2007 Scottish Gliding Union Flarm Trial (With emphasis on use during training and local ridge soaring) February to October 2007 @[email protected] Page 1 of 23 Flarm Trial – Portmoak 2007 CONTENTS Page Introduction 3 Trial Design 4 Results 6 Phase 1 6 Phase 2 6 Phase 3 7 Discussion 8 Conclusion and Recommendations 9 Appendices List 9 Acknowledgements 9 Appendix 1 10 Technical Issues 10 Human Factor Issues 13 Training Issues 16 Appendix 2 Questionnaire and Results Summary 17 Appendix 3 Flight Reference Card 19 Appendix 4 Example of Briefing Notes 21 @[email protected] Page 2 of 23 Flarm Trial – Portmoak 2007 Introduction Flarm is a GPS based aid to the See and Avoid method of collision avoidance. It was originally developed by pilots whose main soaring domain was the Swiss Alps and was introduced in 2004. Since then there has been a rapid and voluntary uptake of Flarm and at the time of writing over 9000 units are in use in Europe, Australia & South Africa. English language trials of pilot opinion, based on questionnaire evidence after thermal flying, have been published in South Africa and Australia. The basic operating method is that each unit computes a projection of its future path over the next 30 seconds and broadcasts that projection – other units receive all the other predicted paths within range and look for intersections with their own predicted paths. If there is such a predicted intersection then the Flarm unit displays both a visible and audible alert to the pilots of both aircraft. There are a number of different technical solutions for the display of this information but by far the most widely used at the present time is a small LED rose display either integral to, or mounted remote from, a small combined GPS/low power transceiver unit.
    [Show full text]
  • FTD-014 FLARM Configuration Specification
    Date: 2021-05-10 FLARM Version: 1.11 CONFIGURATION Page: 1 of 50 FLARM Technology Ltd Document Number: Hinterbergstrasse 15 SPECIFICATION FTD-014 CH-6330 Cham Document status Published status Confidentiality status ☐ Draft ☐ Internal ☒ Published ☐ NDA ☐ Canceled ☒ Public Version control Ver. Date Summary of changes 1.00 2015-07-23 Initial version 1.01 2015-07-27 Minor editorial changes 1.02 2015-08-04 Added missing AUDIOOUT 1.03 2015-12-16 Changed Classic FLARM default range Added ADSBWARNINGS item Corrected track information in stealth mode Added Note to ADSBRANGE item 1.04 2017-03-08 Corrected PCASBEEP description Added TASK item Separated information items from configuration items Added BRIGHTNESS and BATTERYTYPE items 1.05 2017-08-24 Removed restriction for the maximum number of characters in $PFLAC,R,LIC THRE, ID, CAP, LIC, DEVTYPE, and ADSBRANGE description and values changed HWVER and LIC deprecated Added new information item SWEXP Editorial changes 1.06 2018-07-11 Added FFS (force flight state) functionality Changed THRE values and defaults Added protocol version 8 1.07 2019-07-08 Added protocol version 9 Added DEVICEID 1.08 2019-07-31 Editorial changes 1.09 2020-03-02 Updated XPDR and MODESALT description Added ADSR license to LIC Added additional baud rates 1.10 2020-10-23 Fix maximum length of IGC fields Added REBROADCASTSERVICES Editorial changes 1.11 2021-05-10 Baud rate must be manually set for Garmin TIS protocol Added command termination for $PFLAC,A,TASK Date: 2021-05-10 FLARM Version: 1.11 CONFIGURATION Page: 2 of 50 FLARM Technology Ltd Document Number: Hinterbergstrasse 15 SPECIFICATION FTD-014 CH-6330 Cham Scope and summary The scope of this document is to provide a complete reference to the various configuration settings that can be applied to FLARM devices.
    [Show full text]
  • Factors Influencing the Usability of Collision Alerting Systems in Gliding
    Factors influencing the usability of collision alerting systems in gliding Einflussfaktoren auf die Gebrauchstauglichkeit von Kollisionswarnsystemen im Segelflug Dipl.-Ing. Christoph Georg Santel Dissertation D17 Darmstadt 2016 Fachbereich Maschinenbau Institut für Flugsysteme und Regelungs- technik Factors influencing the usability of collision alerting systems in gliding Einflussfaktoren auf die Gebrauchstauglichkeit von Kollisionswarnsystemen im Segelflug Vom Fachbereich Maschinenbau an der Technischen Universität Darmstadt zur Erlangung des Grades eines Doktor-Ingenieurs (Dr.-Ing.) genehmigte Dissertation vorgelegt von Dipl.-Ing. Christoph Georg Santel aus Köln Berichterstatter: Prof. Dr.-Ing. Uwe Klingauf Mitberichterstatter: Prof. Dr. phil. Joachim Vogt Tag der Einreichung: 26. November 2015 Tag der mündlichen Prüfung: 02. Februar 2016 Darmstadt 2016 D 17 Bitte zitieren Sie dieses Dokument als: URN: urn:nbn:de:tuda-tuprints-51707 URL: http://tuprints.ulb.tu-darmstadt.de/5170 Dieses Dokument wird bereitgestellt von tuprints, E-Publishing-Service der TU Darmstadt http://tuprints.ulb.tu-darmstadt.de [email protected] Die Veröffentlichung steht unter folgender Creative Commons Lizenz: Namensnennung – Nicht kommerziell – Keine Bearbeitung 3.0 Deutschland http://creativecommons.org/licenses/by-nc-nd/3.0/de/ Abstract The dissertation at hand identifies and analyzes how well glider pilots use low-cost collision alerting systems. While being generally recognized as a commendable tool for helping glider pilots see and avoid other traffic, these systems have been cited as possible contributing factors in several accidents. In literature, no in-depth research on how glider pilots may interpret or misinterpret their indications was found. At the beginning of this dissertation, a market study of human-machine inter- faces for low-cost collision alerting systems is presented.
    [Show full text]
  • Price List CH.2020.003 CH-6330 Cham Valid from 2020-10-25 Until Replaced
    FLARM Technology Ltd Hinterbergstrasse 15 Price list CH.2020.003 CH-6330 Cham Valid from 2020-10-25 until replaced www.flarm.com PowerFLARM devices PowerFLARM PowerFLARM PowerFLARM Core Portable Fusion Part number, E-version7 FLAPFC11E FLAPFP24E FLAFUS10W Part number, A-version8 FLAPFC11A FLAPFP24A Integrated display ● Built-in GPS Antenna ● Second FLARM Receiving Antenna1 ○ ○6 ● Option to run on batteries (6 AA; not included) ● SSR 1090 MHz Receiver (Mode-S) ● ● ● ADS-B 1090 MHz Receiver ● ● ● USB port for data readout and updates ● ● microSD Card slot for data readout and updates ● Data port #1, 8P8C/”RJ45” ● ● ● Data port #2, D-sub DE-9 ● ● 5V 500mA output for ext. devices (on USB port) ● ● External Audio Output ● ● IGC Flight Recorder Approval2 ● ○ ● Engine Noise Level (ENL) Recording3 ○ ○ ● Obstacle Database/License with Warnings4 ○ ○ ○ EASA Minor Change Approval (MCA)5 ○ ○ ○ Bluetooth/Wi-Fi connection to EFBs ● FLARM Hub mobile-friendly embedded web app ● Browser-based configuration and maintenance ● GDL 90 traffic data ● Manufacturer's suggested retail price (MSRP) EOL 1,990.00 1,660.00 ● Included; ○ Optional; 1Additional Antenna and License; 2Up to and including Diamonds; 3Requires IGC Flight Recorder Approval option; 4Available for selected regions; 5Available for selected aircraft types; 6License included; 7The E-version works in Europe, Africa, and New Zealand; 8The A-version works in North and South America, Australia, and Israel Licenses & MCA License Part number Price4 Activate Second FLARM Receiving Antenna1 LICRFB 149.00
    [Show full text]
  • IGC Vote Results 2007
    Decisions Taken at IGC Plenary February 29th - March 1st , 2008 The proposals can be found on the the IGC web: www.fai.org/gliding/igc_plenary08 A full report of the meeting will be published later. Agenda Topic Summary Outcome Item 6.4.5 30th FAI WGC 2008, Germany Bureau Decisions on entries - World Champions are additional to the class limit of 50 - Annex A procedure will be used to reduce class to 50 (plus World Champions) - Annex A procedure may be used to reduce overall entries to Organiser’s limit 6.4.6 30th FAI WGC 2008, Italy Bureau Decisions on Club Class - Two-seaters may compete in the Annex A 3.4.3 e Open Class - Future Handicap List management a. Addition and Deletion of aircraft will be a Plenum decision b. Amendments to the Handicap factors will be a Bureau decision 6.4.11 Sanction fees for the 1st South American Waiving of outstanding 1200EUR of Adopted Continental Championships sanction fees for first Continental Championships 9.1.1 Election of IGC Bureau members Bureau members to be elected for 2- Adopted year terms starting 2009 9.1.2 Long-term agreement with Air sports Amended to read “agreement with Adopted Limited” an appropriate party” covering internet publishing rights for Sailplane Grand Prix events 9.2 Creation of Country Development Working To foster and organize improved Adopted Group support to new counties developing the gliding sport 9.3 Adoption of common open standards for The aim is to allow for the Adopted. To be recommended to FAI critical electronic systems for gliding development of traffic awareness Navigation and Airspace Commission equipment for light aviation (NAVAC) 9.4.1 SC3 General Section, draft 2008 Edition Major update and simplification of Lost.
    [Show full text]
  • AGENDA Plenary Meeting FAI Gliding Commission (IGC)
    AGENDA Plenary Meeting FAI Gliding Commission (IGC) To be held in Istanbul Friday 8th and Saturday 9th March 2019 at Eresin Hotels Topkapı Version: 7 March 2019 FAI – FEDERATION AERONAUTIQUE INTERNATIONALE – THE WORLD AIR SPORTS FEDERATION Day 1, Friday 8 March 2019 Session 1: Opening and Reports (Friday 09.00 – 10.45) 1. Opening and Welcome (Eric Mozer) 1.1 Absent friends 1.2 Roll Call 1.3 Administrative matters (Vladimir Foltin) 1.4 Declaration of Conflicts of Interest 2. Minutes of previous meeting, Freudenstadt 2nd and 3rd March 2018 (Eric Mozer/Vladimir Foltin) 3. IGC President’s report (Eric Mozer) 3.1 Bureau Decisions taken since the last Plenary that need the IGC Plenary approval 3.2 Discharge of Bureau responsibility for decisions since last Plenary 4. Item moved to morning Day 2 (9:00 – 10:45) 5. Finance (Dick Bradley) 5.1 Treasurers Report and 2018 Financial Statement 5.2 2019 Budget 6. Reports not requiring voting Please note that written reports under Agenda items 6.1, 6.2, 6.3, 6.4 and 6.5 are made available on the IGC web-site, and will not necessarily be presented. The Committees and Specialists will be available for questions. 6.1 OSTIV report (Dr Rolf Radespiel) 6.2 Standing Committees 6.2.1 Sporting Code Section 3D Report (Ross Macintyre) 6.2.2 Sporting Code Section 3D, Annex A (Rick Sheppe) Sporting Code Section 3D, Annex A Handicaps (Christof Geissler) 6.2.3 Sporting Code Section 3D, Annex D (Reno Filla) 6.2.4 Air Traffic, Navigation, Display Systems (ANDS) Report (Rick Sheppe) 6.2.5 GNSS Flight Recorder Approval
    [Show full text]
  • Operating Manual Flarm Collision Warning Unit
    ® OPERATING MANUAL FLARM COLLISION WARNING UNIT Status Software Version 5.00 (March 01, 2011) This is a translation of the German manual. © 2003-2011 FLARM Technology GmbH Baar-Switzerland www.flarm.com [email protected] OPERATING MANUAL FLARM COLLISION WARNING UNIT 1. Welcome to the FLARM user community Thank you for purchasing FLARM, a modern low-cost collision-warning unit for sailplanes and light aircraft. The main task for FLARM is to support the pilot, while he scans the airspace ahead with his own eyes. FLARM is simple to use and does not distract the pilot from the main business in hand. Sport flying is an activity that is associated with considerable risks for crew, passengers, third parties and other objects. In order to make full and safe use of FLARM, it is absolutely essential to be fully aware of the risks, operating conditions, restrictions and limitations associated with the use of FLARM, ensure a proper installation and do regular software updates. This includes familiarity with and observance of this Operating Manual and the Installation Manual. Additional configuration information can be found in the ‘Data Port Specifications' document, e.g. how to suppress additional data at the serial port what might be required in international championships. We welcome user feedback and reports, suggestions for improvements, and pictures that will help us make further improvements to FLARM. Feedback reports should give a detailed description of the situation, quoting the Hardware and Software versions used, plus the flight data records in IGC format with short time recording intervals. The latest version of this handbook and other related documents can be found at the Website www.flarm.com.
    [Show full text]