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7.3.  IGC-License Certificate

FÉDÉRATION AÉRONAUTIQUE INTERNATIONALE

IGC-APPROVAL FOR GNSS FLIGHT RECORDER GARRECHT VOLKSLOGGER MODEL VL1.0

ISSUE 2 INCLUDING MOTOR GLIDER ENL FUNCTION

This document supersedes the original issue dated 15 April 1998 and adds the Motor Glider Engine Noise level (ENL) function. It
gives formal approval for this GNSS FR equipment to be used for validation of flights under the FAI Sporting Code 

Section 3

(Gliders and Motor Gliders) for FAI badge and record flights, subject to the conditions and notes given later. It is posted on the
FAI/IGC GNSS web site given at the top of this page. FAI reserves the right to alter the terms of this approval.
GFAC tests are concerned primarily with data accuracy, security, data transfer, conversion to and conformity with the standard
*.IGC file format. Other aspects of the equipment may not be tested and are a matter between the FR manufacturer and
customers.
The attention of NACs, Officials and Pilots is drawn to the latest edition of the FAI Sporting Code 

Section 3

, including

amendments. 

Annex A

 to this code deals with competition matters, 

annex B

 to the Code deals with equipment used in flight

validation, and a separate document published by FAI is entitled "

Technical Specification for IGC-Approved Flight Recorders

".

Copies of all of these documents may be obtained from the FAI/IGC web sites listed above and hyperlinks are provided from the
gliding/gnss page.
It is recommended that a copy of this approval including its annexes is kept with each unit of the equipment.

Manufacturer:

Garrecht Ingenieurgesellschaft
Raiffeisenstrasse 45-53
55270 Klein-Winternheim, Germany
Tel: +49 6136 89 931
Fax: +49 6136 89 043
Email: 

[email protected]

Web: 

www.segelflug.de/firmen/gcs

Contact: Dipl.–Ing. Georg Garrecht, Dipl.-Ing. Johannes Garrecht

Equipment:

Hardware:

Versions. The version number is shown on the LCD on start up. This document covers Version 3.2 or later, and Version 3.3 and
later includes the Engine Noise Level (ENL) function.
Description. The FR consists of a rectangular metal case about 100 x 50 x 54 mm, and weighs about 320 grammes. A LCD 60 x
17 mm is on the 100 x 50 mm face together with three buttons, and a circular external electrical connector is on an end face.
National regulations. These may apply to electrical and electronic equipment, such as the EC "CE" mark for compliance with EC
directives on EMC and voltages. Compliance with such regulations is not the responsibility of FAI. This equipment has the EU CE
mark.

Model Numbers.
Model VL1.0 has an integral antenna.
Model VL1.0E has a BNC-plug for an external antenna (E = External).
Model VL1.0C has both an internal antenna and the plug for an external antenna (C = Combined); when an external antenna is
connected, the internal antenna is disabled.

Firmware:

Version 3.4 or later, as shown on the LCD on start up.

External software:

Garrecht DATA and VALI program files Version 4.16 or later, although for the Engine Noise Level (ENL) figures to be
transferred, Version 4.23 or later is required. It is recommended that the latest versions of the program files are used, obtained
from the IGC GNSS site for software given below. These program files are backward compatible to previous versions of the FR.
For checks of electronic security by NACs, OOs and Data Analysts, the latest version of the VALI program should be used
(obtained from the ftp site below) so that it is compatible with the latest firmware releases.
Program file functions. The file DATA-GCS.EXE is for transferring flight data from the FR to a PC and also converts to the
*.IGC file format. The file VALI-GCS.EXE is for validation by NACs and FAI of the security and integrity of the *.IGC files.
Free availability. The DATA and VALI files are copyright of the FR manufacturer but are freeware, and the latest versions may be
obtained from the FAI site 

ftp://www.fai.org/gliding/software/gps/pc

Содержание VOLKSLOGGER

Страница 1: ...VOLKSLOGGER User Manual Edition 1 7 2 English 05 07 2000 for Volkslogger Firmware 3 6 Subrelease 174 Hardware 3 4 Garrecht Ingenieurgesellschaft Translation by ENTEC Technical Services Inc...

Страница 2: ...5 6 ELECTRONIC FLIGHT DECLARATION 29 Introduction 29 5 6 1 Overview 30 5 6 2 Input Editing 30 5 6 3 The Coordinate Template 34 5 7 BASICS OF DATA INPUT 36 Introduction 36 5 7 1 Field Types 36 5 7 2 Ed...

Страница 3: ...stem is being shipped with the following accessories Data Cable with a 220VDC 14VAC Power Supply transformer local dealers may supply locally adapted units for Readout and Programming of the Logger by...

Страница 4: ...MSL 3m Resolution Steps double every 5 500m 18 045 ft Temperature Error over entire Temperature Range 2 hPa 2 mb Coordinate Recording geogr Longitude geogr Latitude WGS 84 Format Resolution 1 60 000 1...

Страница 5: ...r Ethanol One has to be careful not to let any liquid penetrate into the instrument or damage the label seal on the back Do not use ACETONE or any other harsh solvents since these destroy the labels 3...

Страница 6: ...isplay The statements for mounting instruments and antenna are also valid for instruments with external GPS Antenna 3 3 2 Electrical Installation Power supply and communication with PC or flight compu...

Страница 7: ...omentary drops below the minimum voltage In particular during switching of batteries such voltage drops can take place which will lead to a separated flight record during readout This means that the r...

Страница 8: ...ding For correct GPS reception it is necessary to wait for the contact with valid satellite signals The number of received satellites is shown in the lower left of the display Only after 4 preferably...

Страница 9: ...the next higher level Key 2 has the Next function You can select the displayed menu items with it Besides this in modes where you can change a value Key 2 can be considered a Key Key 3 has the proper...

Страница 10: ...2 Introduction Screen Serial 06F HwR 3 2 FwR 3 5 Serial Number in base 36 Format Hardware Version Firmware Version 3 Introduction Screen Security Seal is OK Condition of the Electronic Seal Security...

Страница 11: ...is an instrument on which the seal is broken can no longer store setup data All parameters are returned to the default values during each turn on After initialization has taken place and the introduct...

Страница 12: ...layed navigational modes menus etc The only possibility for the pilot to interact with the recording process is in the modification of the recording cycle logging interval adjustment definition of the...

Страница 13: ...tantially from the speed and heading of flight in the air Note Heading is the direction of the nose of the glider while track is the path of the glider over the ground Bearing is the direction between...

Страница 14: ...s a useful additional instrument if used properly It can for instance if displayed in feet and set to standard pressure show the flight level directly to avoid entering limited flight access areas or...

Страница 15: ...page menus the presently shown page is indicated in the example Page 1 of the main menu The exact meaning of the individual abbreviations is explained in the following section Key Functions 1 Switches...

Страница 16: ...16 16 The methods for input of values in the different menus CFG1 CFG2 FAI are covered in detail in chapter 5 7 Basics of Data Input...

Страница 17: ...chapter 6 6 1 Flight Data Memory and 6 1 3 Flight Declaration Form Memory BAT Battery Voltage Shows the actual value of the Supply Voltage VL Shows the Volkslogger Introduction Screens See Chapter 5 1...

Страница 18: ...The actually necessary key pressure is indicated by a blinking cursor PC PC Communication Activates the PC communication of the logger This is a separate operating mode which cannot run in parallel w...

Страница 19: ...he fast interval recording mode and signals this acoustically through short beeps When sufficient valid points adjustable have been recorded the VL acknowledges this with a long beep The number of the...

Страница 20: ...of a warning on the screen Battery warning When the supply voltage drops below the value of 9 5 Volts Memory warning When the remaining storage capacity is less than 8 hours The automatic warnings are...

Страница 21: ...rse BEARING from the actual position to that point GPS Status information speed and course over ground TRACK are shown By skillful positioning of BRG and TRK on the Nav screen it becomes possible to o...

Страница 22: ...sk route as long as it is in existence This is communicated to the pilot by another acoustical signal one long beep duration 1s Figure 3 Observation Zone Sector Cylinder Start Finishgate Explanation o...

Страница 23: ...aration via NAV DCL or FAI EDIT TASK Route from the data base NAV RTE Operation Mode Single Point The single point mode is for the navigation to a single point which can be selected by the pilot in ma...

Страница 24: ...he observation zone cylinder and sector are activated whose radii are transferred from the actual menu setting CFIG1 LOG OZ An individual setting of the observation zone for separate points of the rou...

Страница 25: ...1 Adopts the point as the navigation target and returns the display to the screen Navigation 2 Displays the next place in the order of rank Important Note For the correct functioning of these features...

Страница 26: ...2 Display of the next Section Note The shown navigation route comprises the following points In navigation operating mode NAV DCL Home Airport Start Point All Turn and Check Points Finish Point In na...

Страница 27: ...e without influencing the contents of the actual IGC file It should however be considered that this change becomes visible at the latest during the next declaration through switching on again current...

Страница 28: ...d time of the flight declaration are generated and stored by the instrument during every flight declaration whether manual or automatic declaration They cannot and may not be changed by the user 5 6 2...

Страница 29: ...erased by the choice of this function thereafter the edit function is called up with empty field content The CLEAR function has the following effect on the various types of fields Character String Ch...

Страница 30: ...does not have to page through the whole database up to 500 points Nevertheless in databases with only a few entries paging through it manually can be the faster search method For this as mentioned ab...

Страница 31: ...d search function Official Airport or E Emergency Emergency landing field meadow farm field closed airport etc H Hard Surface Runway available Latitude Degrees Numeric two digits Latitude Prefix hemis...

Страница 32: ...inder Sector Radius Cylinder Radius Line Width Numeric Range 0 15 x 0 15km Note 0 Line not present Cylinder Radius Type Numeric Range 0 1500m in 100m steps Note 0 Cylinder not present Sector Radius Ty...

Страница 33: ...unctional capacity of the instrument The input of data requires some practice however since the whole spectrum of data types has to be covered with only three keys So is for instance after some famili...

Страница 34: ...lphabet Register Field Actual entry is displayed Key 1 Leave Editing mode adopt displayed entry Key 2 Jump to previous entry in the register Key 3 Jump to next entry in the register Character String A...

Страница 35: ...ected storage interval is taken into consideration during the display If one discovers during the flight that the memory might be full before the end of the flight the residual recording time can be i...

Страница 36: ...ration form FDF The access to this memory area takes place either by editing of the fields menu FAI DECLARE by filling out the flight declaration in the PC program or through other instruments flight...

Страница 37: ...he PC The VOLKSLOGGER display will show DATA TRANSFER READY Choose the flight to be read out by pressing the keys arrow up down To load the desired flight press Enter key upon which the logger will ca...

Страница 38: ...ensor referenced to 1013 2 hPA mb For use of this Data Set please order exact documentation from the manufacturer GPRMC GPVTG GTRMB GPBWC GPR00 GPRTE Standard NMEA Data Sets The adjustment takes place...

Страница 39: ...e version number is shown on the LCD on start up This document covers Version 3 2 or later and Version 3 3 and later includes the Engine Noise Level ENL function Description The FR consists of a recta...

Страница 40: ...ding For observation either a preflight check of the installation must be made and the glider must be under continuous observation by an OO until it takes off on the claimed flight or an OO must witne...

Страница 41: ...ngine noise is clearly received when the engine is giving power it should not be covered for instance although automatic gain will continue to ensure high ENL readings under power Pilots should note t...

Страница 42: ...by typing DATA GCS enter at a DOS prompt or by double clicking DATA GCS in a file list File Manager Windows Explorer etc and then following the menu actions in the DATA GCS file When the DATA file is...

Страница 43: ...namic noise B4 4 ENL during the approach to land ENL values are always higher on a landing approach due to aerodynamic noises such as due to airbrakes undercarriage sideslip etc Short term peaks due t...

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