ZANDER GP 940 Manual Download Page 19

GP940E 01/97

27.02.97

19

2.3

Sealing of data ports:

  no requirement, but no unauthorised data must be passed into the FR during the

time between takeoff and the start of the post-flight transfer of data by an OO. Any abuse of this may lead to a
future requirement to seal the data port.
 
3.

Check of Installation in the Glider.

  Before flight, an Official Observer must check the place of the equip-

ment in the glider concerned and how it is fixed to the glider. Following this examination; EITHER,

3.1.

Continuous Observation.

  The glider must be under

continuous observation by an OO until it takes off

on the claimed flight (so that the FR cannot be transferred to another glider without this being seen); OR,

3.2.

Sealing to the Glider.

  If para 3.1 cannot be met, the FR must be sealed to the glider by the OO so that

it cannot be removed without breaking the seal. The sealing method must be acceptable to the NAC and IGC.
Paper seals must be marked with the glider registration, the date, time and OO's number and signature. A
wire/lead or wax seal with a unique sealing die (imprint pattern) may also be used. Sealing to the glider is allo-
wed to take place at any time or date in advance of the flight. This is because all GNSS fixes have a date/time
content, unlike a drum-type barograph. The use of adhesive plastic tape is not satisfactory for IGC-approved
sealing because it can be peeled off and re-fitted. Gummed paper tape is recommended, as used for sealing
drum-type barographs.

3.3.

Place of Installation in the Glider.

  See para 2.1. Where sealing to the glider is required under para

3.2, the OO must seal the FR unit to glider parts which are part of the minimum standard for flight. It is accep-
ted that such parts can be removed for purposes such as servicing; such parts include the canopy frame, in-
strument panel, and

centre-section bulkhead fittings. If such a part is

transferred between gliders, any FR

seal for the previous glider must be removed. For motor gliders, see para 2.2.

4.

Security Seals, Physical and Electronic.

  The FR unit is physically sealed with adhesive security tape ac-

ross the bottom of the case. An internal electronic security mechanism is also included and its security check
will no longer work is the case is opened. If the FR is found to be unsealed electronically, it must be returned to
the manufacturer or his appointed agent for investigation and resealing, with a statement of how the unit beca-
me unsealed. Whenever any unit is resealed, the manufacturer or agent must carry out positive checks on the
internal programmes and wiring, and ensure that they work normally. If any evidence is found of tampering or
unauthorised modification, a report must be made by the manufacturer or agent to the Chairman of GFAC and
to the NAC of the owner; the IGC approval of that individual unit will be withdrawn until the unit is re-set and
certified to be to the IGC-approved standard.

5

After-Flight Transfer of Flight Data from the FR and conversion to *.IGC File Format.

  Only the IGC-

approved standard of software shall be used. This standard is given on page 1 under `Equipment', and `soft-
ware'.

6

Analysis of Flight Data.

  Analysis of flight data may be through any analysis programme which is approved

by the relevant NAC such as those which use the *.IGC file format. The *.ZAN file which was originally downlo-
aded from the FR must be checked as unaltered by the NAC by the use of an authenticated version of the VA-
LI-ZAN.EXE file (see page 1 under "software"), and the CONV-ZAN.EXE programme then used to derive the
*.IGC file from it; this newly-created *.IGC file must either be used for flight analysis or be checked as being
identical to any earlier version of the *.IGC format which may have been used for preliminary analysis.

7

Manufacturer's Changes.

  Notification of any intended change to hardware, firmware or software must be

made by the manufacturer to the Chairman of GFAC so that a decision can be made on any further testing
which may be required.
 
Ian Strachan
Chairman, IGC GFAC
10 Nov 1996

Annexes:

A. Notes for owners and pilots

B. Notes for Official Observers and NACs

Any Queries to:
Chairman IGC GFAC, Bentworth Hall West, Alton, Hampshire GU34 5LA, England
Tel: +44 1420 564 195; Fax: +44 1420 563 140; email: [email protected]
Annex A to IGC Approval Dated 10 Nov 1996

NOTES FOR OWNERS AND PILOTS -
PART OF IGC APPROVAL FOR ZANDER GP 940 GNSS FR

Summary of Contents for GP 940

Page 1: ...computer SR940 7 7 Preparing waypoints and routes for SR940 GP940 8 8 How to use GP940 10 9 Technical data 13 10 Wiring diagrams 14 11 Pin assignments of connectors 16 12 Calibration chart for altimet...

Page 2: ...ctor signal to GP940 declare and transfer a task from SR940 to GP940 waypoint lists and routes can be entered into recorder and brought to the glider where these informations can be transferred to SR9...

Page 3: ...ng this button must make a connection to minus of supply power If the standard recording rate of 4 seconds per sample is accepted as sufficient the marker button can be left out To make the power supp...

Page 4: ...tion So even without GPS reception information is stored continuously There is no recording during PC operation and during charging with the charger Recording within the GP940 is done in that way that...

Page 5: ...n into the recorder select FDR functions from the ZANxxE EXE main menue then select write personal information The recorder will answer with an audio signal PC operation active Every two seconds the r...

Page 6: ...several pilots sharing a glider may load their own settings before takeoff Important all these inputs to GP940 have no influence to the recorder part of GP940 None of the waypoints or routes entered...

Page 7: ...he in ternal battery is o k If turn off beep is missing recorded flight data are unvalid for FAI use If there is no turn off beep after charging then the internal battery is faulty and must be replace...

Page 8: ...ned off When power is applied again to the recorder the task data entered last are copied into the flight data record just when recording starts A declared task can be changed as desired up to takeoff...

Page 9: ...all routes must use the same turnpoint list At the glider turnpoint list and routes can be trans fered to SR940 by SR940 function read waypoints and routes from FDR If a turnpoint list is un changed...

Page 10: ...le beep no GPS or not yet received 6 uninterrupted GPS fixes If SR940 announces entering the photo sector photo angle less than 40 an automatic mark signal is transmitted to the recorder which has the...

Page 11: ...route flown is written on the flight declaration and it must be marked if that was the declared task The pilot signs this statement Takeof time and landing time are also written to the declaration Th...

Page 12: ...umber of glider Manufacturer and type of flight data recorder ZANDER GP940 Serial number of flight data recorder Geodetic datum used WGS 84 Task Name and coordinates takeoff point departure point turn...

Page 13: ...ignals time barometric altitude GPS position GPS altitude DOP 2D 3D engine running sensor with SR940 indicated airspeed measured wind next WP recording interval 4 seconds 1 second when pressing marker...

Page 14: ...GP940E 01 97 27 02 97 14 10 Wiring diagrams GP940 with SR940 new version...

Page 15: ...GP940E 01 97 27 02 97 15 Wiring diagrams GP940 with SR940 SR820D upgrade version...

Page 16: ...GP940E 01 97 27 02 97 16 11 Pin assignments of connectors...

Page 17: ...x besides the antenna connector see 11 Pin assignments of connectors The GPS antenna is not connected When power is applied the GP940 starts recording Now the ambient pressure is changed in steps from...

Page 18: ...use by OOs on a floppy diskette without the need to access a hard disk These files have unrestricted access and will be placed on the IGC web server Also for the same purposes for Officials familiar w...

Page 19: ...e ac ross the bottom of the case An internal electronic security mechanism is also included and its security check will no longer work is the case is opened If the FR is found to be unsealed electroni...

Page 20: ...hed to a part of the glider structure which is capable of transmitting the vibration caused by the MoP to the case of the FR The FR must be sealed to the glider para 3 2 on page 1 applies unless the F...

Page 21: ...a portable PC is not available the OO shall check and break any sealing to the glider and personally take the main FR module to a PC Connect the PC to the main FR module s 9 pin data port and use eith...

Page 22: ...as if it was flight data see B2 3 above and the calibration data file will then be analysed and a correction table produced of true against indicated altitudes This table can then be used to correct p...

Reviews: