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Annex B to IGC Approval Dated 10 May 1999

NOTES FOR OFFICIAL OBSERVERS AND NACs -

PART OF IGC APPROVAL FOR GARRECHT VL1.0 GNSS FR

To be read together with the main terms of approval to which this is an Annex. It is recommended that a copy of this approval
document is kept with the equipment concerned, for the use of pilots and Official Observers.

B1. Installation and Takeoff Records

B1.1. Installation in the Glider.

 An OO shall witness and record the position of the FR in the glider, the type and serial

number of the FR, the glider type and registration, date and time. Before flight, if requested, the OO shall then seal the FR to the
glider in a way acceptable to his NAC and to IGC, and such sealing may be at any time or date before flight. If sealing is not used,
either a preflight check of the installation must be made after which the glider must be under continuous observation by an OO
until it takes off on the claimed flight, or an OO must witness the landing and have the glider under continuous observation until
the FR installation is checked. This is to ensure that the installation is correct, and another FR has not been substituted in the
glider before the data transfer (

B2.3)

. See paras 

and 

3

 of the Conditions of Approval.

B1.2. At Takeoff

. The time and point of takeoff shall be recorded, either by an OO, other reliable witnesses, or by other means

such as an Air Traffic Control or official Club log of takeoffs and landings. This will be compared to the FR takeoff data.

B2. Landing.

B2.1. At Landing.

 The time and point of landing shall be recorded, either by an OO, other reliable witnesses, or by other means

such as an Air Traffic Control or official Club log of takeoffs and landings. This will be compared to the FR landing data.

B2.2. Checking the Installation of the FR.

 As soon as practicable after landing, an OO shall inspect the installation of the FR

in the glider (including any sealing to the glider), so that this can be compared to the check described in para B1.1 above. The
transfer of flight data shall then take place in accordance with B2.3.

B2.3. Transferring the Flight Data.

 If a portable PC is available, the flight data may be transferred at the glider without

disturbing the installation of the FR; if a portable PC is not available, the OO shall check and break any sealing to the glider, and
take the FR to a PC. If the OO is not familiar with the actions required, the pilot or another person may transfer the data while
the OO witnesses the process. Security is maintained by electronic coding embedded in the FR and in the data transferred in the
"High Security" mode which is then independently checked later at the NAC (and at FAI if the claim goes to them).

Method:

 Execute the file DATA-GCS.EXE on either a floppy diskette or on the PC hard disk and check the software version at

the top of the menu (see under "software" on page 1, which gives the relevant versions). You can also find the version by typing
the file name followed by a space and a question mark at the DOS prompt when the appropriate directory is selected. This
programme file executes in the normal way such as 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 executed, select "N" for new FR, make sure
that the PC is connected to the female 9-pin computer port provided on the cable which goes to the FR, and connect the power
supply to the FR. A 10-second count-down will be shown on the LCD immediately after switching on, during which contact should
be made with the PC. If not, disconnect the power from the FR and re-connect with the PC connected and DATA-GCS and "N"
already selected.
For FAI/IGC record and badge flights, the "High Security" transfer option must be used, not the "test" mode which does not have
electronic security to IGC standards (See para 2.4 of the Conditions of Approval). The floppy diskette may be self-booting. This
process will produce an IGC-format flight data file with the file name YMDCXXXF.IGC, where Y=year, M=month, D=day, C=
manufacturer, XXX = FR Serial Number and F = flight number of the day (full key, Appendix 1 to the IGC GNSS FR
Specification). A copy of this IGC-format file shall be retained securely by the OO such as by immediately copying it to a separate
diskette or PC card, or by the use of the OO's own PC. This file shall be retained by the OO in safe keeping for later checking and
analysis under NAC procedures.

Competitions:

 Different rules may apply for competition flights, for which a central data transfer facility may be used, but for

flights to IGC record and badge rules the above must be followed.

B.3. Analysis of Flight Data Files.

A Data Analyst approved by the NAC will then evaluate the flight using an analysis programme approved by the NAC concerned
(list, see the IGC GNSS web site under SOFTWARE). In addition to checking flight data, an authenticated version of the file
VALI-GCS.EXE shall be used by the NAC and by FAI (if the data goes to them) to check the electronic security coding, that the
FR had not been interfered with, and that the flight data in the *.IGC file has not been altered since it was transferred from the FR.
The version number of the VALI file is shown at the top of the page when the file is executed, or by typing the file name followed
by a space and a question mark, at the DOS prompt when the appropriate directory is selected. The latest version of VALI-GCS
should be used and is available from the IGC GNSS site for software: 

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

Method:

 at the appropriate prompt or run function, type VALI-GCS.EXE followed by a space and the full name of the file to be

checked. If the file security is good, the following messages should appear: first "Type of signature in IGC file: High security level
- DSA (asymmetric): suitable for official flight validation", followed, after the whole file has been checked, by "asymmetric file
integrity is OK". The message "File integrity is not OK, file tampered with!!" indicates either that the FR physical security seal
has been broken, the "Test" transfer mode was used instead of the "High Security" transfer, or that the IGC file has been altered
since it was transferred from the FR. It should be noted that GFAC tests include ensuring that the change of a single character in
an otherwise-correct IGC file, cause the VALI program to fail as indicated above.

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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