PLANEVIEW® MASTER OPERATING SYSTEM SOFTWARE
Contents
1. the latched display format may be released from the latched condition by depressing the 2 3 display button on the display controller for three 3 seconds A different display format may then be selected If the aircraft is on the ground and a DU or AGM is found to be inoperative the manual DU Control Switches may be positioned to ALT on the ground only in order to configure the operational DUs and AGMs in accordance with the MMEL for dispatch however one DU 3 will then be inoperative The following matrix shows the effect of the ALT position selection Appendix A Page 5 of 5 Operational Information Issues Continued AGM condition switch position DU 1 DU 2 DU 3 DU 4 All AGMs operable NORM AGM 1 AGM 2 AGM 3 AGM 4 AGM 1 FAIL DU 1 ALT AGM 2 AGM 4 X AGM 3 AGM 2 FAIL DU 2 ALT AGM 1 AGM 4 X AGM 3 AGM 3 FAIL DU 3 ALT AGM 1 AGM 2 X AGM 4 AGM 4 FAIL DU 4 ALT AGM 1 AGM 2 X AGM 3 The automatic engagement of autothrottles by the Envelope Protection System is inhibited in Cert C ll The autothrottles will not engage if the aircraft speed approaches Vmax or Vmin All known software conditions that caused DU blanking issues have been resolved in Cert C ll however the AFM and QRH procedures have been updated to provide guidance in dealing with DU blanking caused by faulty Network Interface Controllers NICs and or Advanced Graphic Modules AGMs Issues under2. Aerospace All rights reserved including the right to reproduce this publication No part may be reproduced stored in any retrieval system or transmitted in any part or form or by any means electronic photocopying microfilm microfiche mechanical or otherwise without prior written permission of Gulfstream Aerospace This technical data is controlled under the Export Administration Regulations by General License TSU It may not be transferred to a third party without the prior written approval of the U S Department of Commerce PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE This service change installs the PlaneView Master Operating System MOS software EB7031236 00407 on G450 aircraft Airplane Flight Manual AFM Revision 11 or later approved version will be required as a result of this service change PLEASE RETAIN THIS COPY WITH THE ASC BOOKLET Gulfstream G450 Aircraft Service Change 905 July 26 2006 Page 1 of 6 The design change effected by this document is FAA approved If a compliance time inspection interval or process requires FAA approval such approval will be noted by the affected words appearing with an asterisk or note designating FAA approval The design of this Aircraft Service Change ASC is approved by aircraft type design data for installation on aircraft registered for operation in accordance with applicable regulations of the United States Federal Aviation Administration
3. Investigation If the Preview mode is used to tune an onside ILS on the Progress page and then subsequently switching to the offside Nav or FMS sources and cycling through the offside Nav or FMS sources using the DC the onside Nav previously tuned to the ILS in Preview will revert back to autotune Occasionally on power up or after a power interruption FMS 1 will not accept any input When using the what if initialization mode on the MCDU to review the flight plan at a different Mach speed but not selecting the new speed for use and subsequently making a change to the flight plan e g deleting a waypoint the what if Mach speed is automatically selected and placed in the current performance initialization data on the MCDU Datalink automatic position reporting may fail after 1 to 2 hours of flight or if VHF Datalink is lost Weather Radar status is shown in red on CMC WX Summary page however radar functions normally This is thought to be a CMC interface communication problem If the existing flight plan is replaced by an identical flight plan via datalink all three FMSs may reset Uplink wind information is displayed with a green area shown that does not correspond to any of the wind velocity color cues on the wind speed reference legend Unless the throttles are at idle Flex EPR takeoff cannot be selected Entering a Flight Plan with over 100 waypoints will result in a corrupted Custom Database When the flight plan with 100 way
4. message annunciating the condition is scheduled for Cert Delta Whenever the Checklist Function is selected using the button on the Display Controller the checklist will appear in the lower 1 6 window of Display Unit 3 as the default location of this function The checklist may be positioned to any other location using the appropriate selection on the Display Controller or CCD If selecting menu options on the I NAV display results in only a short menu containing only show info and center map then this indicates that there is a disagreement between the AGM nav database and the FMS nav database This most likely will occur when the FMS database is updated on the regular cycle but the AGM database update is omitted In Cert C ll the automatic Advanced Graphics Module AGM reversion feature has been disabled while in flight If an AGM or Display Unit DU fails while in flight it may not be recovered The Display Unit Control switches that were used to select an alternate AGM for a Display Unit have no effect in the ALT position while airborne However the inflight display format conversion will automatically switch according to the established default settings to ensure the preservation of a PFD display for each pilot and the display of CAS messages and Engine Data If the display format has switched due to a DU or AGM failure that display format is latched If the failed AGM or DU subsequently recovers and is found to be usable
5. of this ASC provides detailed PlaneView software information including known anomalies and planned resolutions operational information issues and issues under investigation Approved Engineering Data The source data for this aircraft service change is 1159ASC47905 Rev Top Drawing Certification Charlie II MOS Gulfstream G450 Aircraft Service Change 905 July 26 2006 Page 2 of 6 Prerequisites G450 ASC 903 or ASC 904 PlaneView Master Operating System Software Update Concurrent Requirements G450 ASC 014A PlaneView Avionics Enhancement must be installed in conjunction with this service change Associated Documents G450 Aircraft Maintenance Manual AMM Chapters 20 31 and 34 Flight Manual Revision Supplement Required Airplane Flight Manual AFM Revision 11 or later approved version will be required as a result of this service change Publications Data Data concerning this service change will be published in a future revision of the affected manual s This booklet will provide technical data until the revision s are published Effectivity This service change is applicable to Gulfstream G450 aircraft serial numbers 4001 4057 This or a similar change will be installed during Initial Phase on Gulfstream G450 aircraft serial number 4058 and subsequent Effect on Spares None Special Equipment Tools Required Aircraft s PC Laptop with Remote Terminal Tool version 16
6. reports at higher latitudes 60 N or higher where the tolerance limits of 3 minutes of longitude equates to 1 5 NM or less Datalink reports passing the position earlier than actual point passage Will be addressed in Cert Delta Flex EPR cannot be selected for takeoff unless a NAV source is selected in the FMS NOTE this applies to G450 G350 aircraft only Will be addressed in Cert Delta FMS predictions of time enroute and fuel consumed for the last flight plan leg prior to top of descent TOD are inaccurate The groundspeed and fuel flows for this leg will be lower than actual thus the FMS predicted time enroute will be longer than actual and actual fuel used will be more than the figure shown on the FMS page The degree of inaccuracy is dependent on the length of the leg that precedes TOD Entering a pilot defined waypoint or route waypoint just prior to TOD will minimize time and fuel inaccuracies Fixed in Cert D Appendix A Page 3 of 5 Operational Information Issues If operating on emergency batteries E batts you don t have to select EMER on ACPs to talk on Radio 1 Selecting EMER on ACPs only bypasses PlaneView avionics interfaces and connects the ACPs directly to Comm 1 Selecting E batts or extending the EMER switch de powers a relay which ties ACP 1 and 2 transmit directly to Comm 1 The Electronic Charts are loaded using the Honeywell blue disk in the DMU The E chart program resides on the AGMs an
7. 0 NOTE Correct setup of the aircraft laptop with the CMC Remote Terminal Tool is critical to the successful loading and operation of all software Follow Data Load Guide procedures CAREFULLY Ensure any firewalls anti virus programs or wireless LAN connections are disabled and the laptop is connected to 60 Hz aircraft power D Load the following software in accordance with GIVX GER 9934 Section 2 0 PlaneView Software Loading 1 PlaneView Master Operating System software Component of Top Level System P N EB7031236 00407 NOTE Testing of this installation and the installations found in G450 ASC 14A should be conducted only after all of the hardware and software installations are completed GIVX SGER 905 is the only required test E Comply with G450 ASC 014A Steps F 1 through 10 F Verify all software loads in accordance with GIVX SGER 9934 Rev F or later Section 6 0 ASC Enter 16 digit INDS serial number recorded in ASC 014A Step A 2 to access charts information as required Gulfstream G450 Aircraft Service Change 905 July 26 2006 Page 4 of 6 NOTE The following changes were incorporated into the base Certification Charlie II LDI for the Central Maintenance Computer CMC AGM reset test is removed AGM Member system status is removed Nuisance AOA maintenance faults reported to the CMC and a blue Check CMC CAS message being displayed has been prevented when the
8. 3 2 or later Refer to Gulfstream PlaneView Maintenance Applications disk version 4 1 or later PN 1159LAP59000 Skill Type Required Knowledge of the Gulfstream G450 PlaneView avionics system will be required for this installation Price Prices are subject to change without notice Installed Price See notes Gulfstream G450 Aircraft Service Change 905 July 26 2006 Page 3 of 6 NOTE This ASC will be installed at no charge for a period of 24 months from the release date noted on the cover of the aircraft service change if installed at Gulfstream Aerospace or a Gulfstream G450 Authorized Warranty Repair Facility All other installations are subject to the prevailing labor rate of the installing agency NOTE This ASC Kit will be provided at no charge for a period of 24 months from the release date noted on the cover of this Aircraft Service Change After the 24 month period has expired this ASC Kit s will be priced and sold NOTE Coverage is granted per the terms and conditions of the Gulfstream Aircraft Sales Agreement to the original purchaser or subsequent owner with appropriate Assignment of Warranties on file with Gulfstream MODIFICATION INSTRUCTIONS A Prepare aircraft for safe maintenance Refer to G450 AMM Chapter 20 20 10 B Ensure Steps A through E of ASC 014A PlaneView Avionics Enhancement have been complied with C Apply electrical power to aircraft Refer to G450 AMM Chapter 20 20 1
9. AOA heaters are selected off G Perform Return to Service RTS Checkout Procedure GIVX SGER 905 provided with this service change H Verify Top Level System software part number on Configuration Management Software CMS screen matches the part number on the CD ROM Refer to Figure 1 I Remove disk from laptop and store in aircraft J Discard previously used version of the PlaneView Master Operating Software CD ROM K Remove electrical power from aircraft Refer to G450 AMM Chapter 20 20 10 L Ensure work area is clean and clear of foreign objects FOD M Document the following information on the attached service reply card and in the aircraft logbook Refer to Figure 1 Top Level System Part Number Media Part Number Media Serial Number N Document the necessary information on the PlaneView Configuration Record located within the MISCELLANEOUS section of the aircraft s permanent maintenance records O Record compliance with this aircraft service change in the aircraft s permanent maintenance records and return aircraft to flight status P Report compliance with this aircraft service change to Gulfstream CMP via electronic transmittal or fill out and fax the attached Service Reply Card Gulfstream G450 Aircraft Service Change 905 July 26 2006 Page 5 of 6 WEIGHT AND BALANCE DATA The weight and balance of the aircraft is not affected by this service change ELECTRICA
10. CHANGE HAS BEEN COMPLIED WITH ASC NUMBER A C AIRCRAFT TYPE COMPLIANCE DATE 979050 G450 AIRCRAFT HOURS AIRCRAFT LANDINGS PREVIOUSLY COMPLIED WITH PCW DATE NOT APPLICABLE DATE DISC INFORMATION MEDIA TITLE TOP LEVEL SYSTEM PART NUMBER MEDIA PART NUMBER MEDIA SERIAL NUMBER CMP CODE TLS MM OFF 319010 319012 MOS ON 319010 319012 SIGNATURE TITLE CERTIFICATE NUMBER COMPANY COMMENTS SUGGESTIONS ACTIONS TAKEN Appendix A Page 1 of 5 APPENDIX A PLANEVIEW SOFTWARE INFORMATION UPDATE updated July 14 2006 Open Issues and Planned Resolutions NOTE THIS INFORMATION IS ADVISORY ONLY This appendix contains neither approved flight procedures nor official guidance Consult the latest guidance in the airplane flight manual AFM or quick reference handbook QRH for flight procedures Updates to this appendix can be found in the Waypoints section of myGulfstream com at the following link https www mygulfstream com portal customer pilots Anomaly Resolution During Radar Altimeter Test the Flight Controls System page weight on wheels indication will amber cross hatch and the ECS load valve will close Corrects with release of Rad Alt test button Resolved in Cert Delta Occasionally pilot and copilot display sensors power up defaulted to ADS 3 and RAD ALT 1 Condition may be associated with a low voltage APU start To resolve the issue select desired sensor
11. Individual approval should be obtained from the appropriate airworthiness agency prior to installation on aircraft registered outside the United States The design of an ASC is configured to a standard greenie production aircraft If spare wires pin connections or locations called out have been used for another modification the installing agency must ensure the development documentation and approval of any required deviations The following instructions in step by step form are written as a guide to perform this ASC Compliance with safe maintenance practices as recommended in the Aircraft Maintenance Manual and FAA regulations is required Gulfstream considers this ASC a means to enhance aircraft capabilities to meet individual operator requirements The modification is not related to any safety or airworthiness condition Subject Indicating Recording Systems ATA 31 PlaneView Master Operating System Software Update Purpose Discussion This service change installs the PlaneView Master Operating System software EB7031236 00407 on G450 aircraft This service change enhances the overall performance and reliability of the PlaneView Avionics System Description Man Hours Required Per Aircraft This service change installs updated Master Operating System software P N EB7031236 00407 This ASC must be installed in conjunction with G450 ASC 014A Approximately 10 man hours will be required for this installation Appendix A
12. L LOAD ANALYSIS DATA The effect of this change on the aircraft s electrical loading will be 0 PARTS REQUIRED PER AIRCRAFT Item Part Number Nomenclature Qty Notes Alt Substitutes 1 EB7031236 00407 Master Operating Software 1 2 GIVX SGER 905 Return to Service Checkout Procedure 1 NOTE All drawings publications and media software will be issued to the latest revision Gulfstream G450 Aircraft Service Change 905 July 26 2006 Page 6 of 6 Figure 1 Top Level System Part Number Media Part Number Media Serial Number Gulfstream G450 Aircraft Service Change 905 July 26 2006 Aircraft Service Change prepared by Gulfstream Aerospace Savannah International Airport PO Box 2206 Savannah Georgia 31402 2206 USA 2006 Gulfstream Aerospace All rights reserved including the right to reproduce this publication No part may be reproduced stored in any retrieval system or transmitted in any part or form or by any means electronic photocopying microfilm microfiche mechanical or otherwise without prior written permission of Gulfstream Aerospace This technical data is controlled under the Export Administration Regulations by General License TSU It may not be transferred to a third party without the prior written approval of the U S Department of Commerce SERVICE REPLY CARD PLEASE FAX THIS PAGE TO GULFSTREAM AEROSPACE CMP FAX 912 965 3598 THE FOLLOWING AIRCRAFT SERVICE
13. NUMBER 905 INDICATING RECORDING ATA 31 PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE July 26 2006 Gulfstream G450 Aircraft Service Change 905 July 26 2006 Aircraft Service Change prepared by Gulfstream Aerospace Savannah International Airport PO Box 2206 Savannah Georgia 31402 2206 USA 2006 Gulfstream Aerospace All rights reserved including the right to reproduce this publication No part may be reproduced stored in any retrieval system or transmitted in any part or form or by any means electronic photocopying microfilm microfiche mechanical or otherwise without prior written permission of Gulfstream Aerospace This technical data is controlled under the Export Administration Regulations by General License TSU It may not be transferred to a third party without the prior written approval of the U S Department of Commerce PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE This service change installs the PlaneView Master Operating System MOS software EB7031236 00407 on G450 aircraft Airplane Flight Manual AFM Revision 11 or later approved version will be required as a result of this service change PLEASE DETACH AND GIVE TO FLIGHT DEPARTMENT PERSONNEL Gulfstream G450 Aircraft Service Change 905 July 26 2006 Aircraft Service Change prepared by Gulfstream Aerospace Savannah International Airport PO Box 2206 Savannah Georgia 31402 2206 USA 2006 Gulfstream
14. To be resolved in Cert Delta NAV 1 and or NAV 2 may power up with DME Hold selected on Must select DME Hold off from the MCDU Nav Radio detail page For consideration in Cert Delta If a step climb is entered in the flight plan and the flight continues past the Bottom of Step Climb point the Vertical Track Change message will be displayed each time the FMS re calculates performance data Frequency of the message display increases during large turns To clear message delete step climb segment from performance init For consideration in post Delta cert VNAV path deviation may not match between pilot and copilot with possible automatic disengagement of VNAV Vertical direct to will re sync the VNAV path deviation Investigation under way to determine cause of problem will correct in Cert Delta if cause is determined Infrequent auto throttle power lever changes for speed control with an active speed target Disconnect auto throttle and re engage to stabilize power lever movement To be resolved in Cert Delta Selection of the DLK key may not always result in display of the Datalink menu page Standby and Misc pages are typically observed Re select DLK key May require as many as 3 attempts To be resolved in Cert Delta Appendix A Page 2 of 5 Anomaly Resolution Uplink weather display does not update the SEND button status in a timely manner if both pilots have been accessing the uplink weather selection t
15. WS callouts may be delayed such that they appear to be inaccurate e g the 40 call at 20 Appendix A Page 4 of 5 Operational Information Issues Continued If operating on battery power only the Horizontal Stabilizer will show failed on the Flight Controls page Once the HMG master is on and up to speed HMG fault light out the stabilizer will work normally Normal operation can be confirmed by going to emergency stabilizer and using trim switch An amber flashing WX will be shown up on the HSI and INAV displays if the radar is transmitting but is not selected for display on either display Also at ranges less than 5 half range WX will not be available and the WX annunciation will flash amber It is normal for the aileron indication to fill completely at approximately 2 3 of full travel on the Flight Controls display If the FMSs experience a power interruption temporary NOTAM information will be lost If an MRC fails the other MRC will take over the Comm Nav and HF tuning and display functions The radio page on the MCDU will remain fully functional except for the loss of the ADF and Transponder in the failed MRC A stuck microphone logic is incorporated in the ACPs After a 30 second mic use period the transmitter will disengage This feature also applies to SATCOM you must release the mic button every 30 seconds in order to keep the transmitter online This operational logic is per design however a new CAS message and MCDU
16. ab To clear exit the Uplink WX dialog and re attempt several minutes later To be resolved in Cert Delta Failure rate of the weather requests was 40 50 From the method of data transmission from the ground and improper construction of the multiple segments which result in marking the data failed Verify request construction and re attempt selection with fewer segments To be resolved in Cert Delta Performance calculations may incorrectly use the approach speed for descent predictions This can occur if the TO waypoint is in the approach procedure or if the TO waypoint is within the approach distance 15nm defined in the PERF INIT DEP APP page This error is the result of direct clearance to the approach waypoint from 1000 miles Avoid direct to selections of waypoints from distances of greater than 1000 nm To be resolved in Cert Delta Single Engine Performance Predictions show speeds that are 100 knots faster than the single engine cruise speeds To be resolved in Cert Delta Autothrottle speed command receives erroneous signal as flaps transit through 2 12 and 22 up or down when the autothrottles are engaged in speed select mode The speed target change may not show on the Flight Guidance Panel The erroneous command will gradually erode at a rate of 1 knot per second to the correct speed target Disengage autothrottles to avoid speed change To be resolved in Cert Delta Datalink sends inaccurate position
17. d the individual approach charts are on the PCMCIA card in the DMU You can do a full load and load both or you can target load just the PCMCIA card If the AGM programs are out of date it will show which AGMs are out of date in amber on the Database page of the CMC If the airport data or AGM programs are out of date when the Electronic Charts are opened there will be an amber note saying the data may be out of date If everything is current then the letters on the Elec Chart open page will be white Select the X in the top right corner of the Elec Chart page to go to the actual program If you experience power up issues and do not want to dispatch with these issues the recommended course of action is to recycle the last power source that was applied i e if problems arise on application of battery power turn battery power off for 30 seconds and then re apply If problems arise after application of external power or APU power then you may be able to regain normal application by cycling those switches only If this doesn t fix the issue then removal of all power and waiting 30 seconds followed by a normal start is the best procedure The datalink interface is now provided by Global Data Center If you re one of their customers you can request the EPIC PlaneView user s manual which has a good description of the operation of the new interface The logic on the EVS cooling valve message has been revised to only annunciate when the cooling valve i
18. points is closed on the FMS the other two FMSs will go to a cold start and the FMS used to enter the Flight Plan will go to single mode with a corrupted Custom Database To view a presentation on how to restore the FMSs to normal operation click here
19. s not in the correct position You ll no longer get the message below 18 000 You must push the engine start switch for one second or more A momentary button press on start switch may not command the start valve to open SVO icon not displayed and you may get a SVO Maint Required amber message like the GV If so you ll need to shutdown and restart to clear the message The small inverse airplane icon on approach and airport electronic charts indicates that the chart is drawn to scale and the spotter should be shown With SIDS STARS and some airports are not to scale and a spotter will not be shown Waypoint list altitudes are predicted altitudes only Check the FMS for the constraints Also you can only get WP list on DU 1 or 4 after selection of an engine page then WP list This is per design All four APMs have to be up and valid to do an EVS raster alignment APM 1 is in NIC 1 which is on MAU 1A APM 2 is on NIC 4 which is on MAU 2B APM 3 is on MRC 1 APM 4 is on MRC 2 In normal operations there s a Master Slave audio warning system Thus you can hear items like the AP and AT disconnect at the same time as Ground Proximity altitude callouts If MW 1 or 2 fails audible warnings are annunciated sequentially and each audible warning has to annunciate completely before the next warning can sound Thus if you disconnect autopilot during landing at say 45 you will hear the autopilot disconnect tones but the 40 and 20 EGP
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