Replacing GTX 1 (GTX 3000) on Citation M2
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- Jeffrey Norris
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1 Replacing GTX 1 (GTX 3000) on Citation M2 Garmin G3000 Software Version 10 Caution: Caution: Caution: Caution: Note: Before starting the software or configuration loading process, certain items may be required to be recorded first, to prevent loss of information or settings. See Section 1 for details. Make certain that all SD cards are available before starting. These are usually located in a blue pouch onboard the aircraft (usually in AFM). Follow all steps in a given section for specific loadings. Failure to do so will result in probable rework. Ensure that power is available through a GPU so that power is not interrupted during the loading process. This document is to supplement, not replace, the Cessna Citation M2 MM, and Garmin G3000 LMM. Note: Reference latest revision of the Garmin G3000 LMM Table of Contents Introduction Section 1 Section 2 Section 3 Section 4 Section 5 Appendix A Appendix B G3000 System Familiarization References Prior to Certain Software and Configuration Loading Software and Configuration Loading Aircraft Configuration Final Verification / Return to Service Troubleshooting Determining Options Installed Configuration ID / CRC Numbers 1
2 Introduction G3000 System Familiarization When in configuration mode, select GDU controls on left side of GTC 1. Ensure that PFD 1 is selected on the screen. The dual concentric knobs on the lower right bezel will be utilized, and throughout this document will be referred to as the FMS small and large knob. The Enter button will be in the lower right part of the screen. As an alternative, you can use the dual concentric knobs (labeled PFD) and Enter button on the GCU-275 controller mounted above PFD 1. 2
3 Section 1 References Prior to Certain Software and Configuration Loading When replacing a GTX 3000 the following steps must be completed first: Note: This is with the G3000 powered up in normal mode. Radar Trim Settings Go into the left GTC: o Use Back button and select Aircraft Systems. o Select Maintenance. o Enter CACCDMS for password. o Select Radar Trim. Record Pitch Trim Value= Record Roll Trim Value= o If the Radar trims were not both at zero originally: Select Restore Defaults. o Select Home. Select Utilities. Select Setup. Select Avionics Status. Select the Airframe Tab on the left side. Record the Config ID now that the radar trims are zero= This is for reference in case it is needed later. 3
4 Section 2 Software and Configuration Loading This section will provide the steps necessary to target load the software and configuration into GTX 1 after replacement. Note: Anytime that software or configurations are being loaded, all three displays, and both touch controllers must be in configuration mode. Note: Ensure that you have completed the steps contained in Section 1. GTX 3000 GTX 1 (Transponder) When GTX 1 is replaced, then software and configuration loading is required. 1) Pull the following circuit breakers: L PFD MFD R PFD L Touch Control R Touch Control 2) Insert the software loader card into the upper slot of PFD 1. 3) Turn on aircraft power. 4) Press and hold the right knob on the left GTC and push the L Touch Control circuit breaker in. Let go when you see initializing. 5) Press and hold the right knob on the right GTC and push the R Touch Control circuit breaker in. Let go when you see initializing. 4
5 6) Press and hold the #12 softkey on the #2 PFD and push the R PFD circuit breaker in. Let go when you see initializing. PFD 2 should come up in configuration mode. SYSTEM STATUS should show at the top of the screen. 7) Press and hold the #12 softkey on the MFD and push the MFD circuit breaker in. Let go when you see initializing. MFD should come up in configuration mode. SYSTEM STATUS should show at the top of the screen. 8) Press and hold the #12 softkey on the #1 PFD and turn on power. Let go when you see initializing. 9) Press the NO softkey at DO YOU WANT TO UPDATE SYSTEM FILES? prompt. 10) Press the NO softkey at DO YOU WANT TO UPDATE THE CUSTOM GRAPHICS FILES (EG, SPLASH SCREEN)? if it appears. 11) PFD 1 should come up in configuration mode. SYSTEM UPLOAD should show at the top of the screen. Clearing Maintenance Log Note: The maintenance log must be cleared before loading the configuration. On the left GTC 570 touch controller: 1) Select GDU Controls. 2) Select MFD on the left side of the screen under GDU block. Rotate the small FMS knob to select the MAINTENANCE LOG on the page. Press the Clear softkey on the MFD. 1) The Erase entire Maintenance Log? prompt will appear. 2) Press Enter. Wait until Clearing Log disappears before continuing. Select PFD 1 on the GTC 570 to switch the display being controlled. 5
6 Loading Software & Configuration 1) Activate the cursor by pushing down on the FMS knob. 2) Rotate the small knob to drop the menu down, and highlight 525 Base Configuration in the GROUP field. 3) Press the Enter key. 4) Rotate the small knob to drop the menu down, and highlight Cessna Model 525 Base Configuration in the ITEM field. 5) Press the Enter key. 6) Select the CLR ALL softkey at the bottom of the display. 7) Using the FMS knob, highlight the following, press Enter for each, which will place a check mark in each box: GTX Software GTX Configuration 8) Select the LOAD softkey at the bottom of the display. 9) A green PASS message is shown beside software and configuration items as they are successfully completed. 10) Acknowledge when Upload and Crossfill Complete is displayed by pressing the Enter key. 11) Push the UPDT CFG softkey to update the system configuration files. 12) Select YES, and press the Enter key. 13) Acknowledge when Update Config Complete is displayed by pressing the Enter key. 6
7 Section 3 Aircraft Configuration Aircraft Configuration Push the FMS knob to deactivate the cursor. Transponder and TCAS Configuration: o Rotate the inner right knob to go to the Aircraft Configuration page. o Push the FMS knob to activate it. o The cursor should be on the Aircraft Registration line. Rotating the small FMS knob provides a single character cursor. Use the small knob to change the value, and the large knob to move to the next character. U.S. registered aircraft: Enter the aircraft tail number using the FMS knob to select characters. The VFR code should be set to Press Enter. Foreign registered aircraft: Note that the Hexadecimal code will need to be entered first. Then the tail number should be entered. Also the VFR code will need to be set to the correct value for the country of registry. Press Enter. Select the softkey labeled SET GTX1 to program #1 GTX Select OK to acknowledge. Select the softkey labeled SET GTX2 to program #2 GTX Select OK to acknowledge. Select the softkey labeled SET GTS to program the GTS Select OK to acknowledge. 7
8 Section 4 Final Verification / Return to Service Note: This is with the G3000 powered up in normal mode. Determine options installed using Appendix A. Select Home on the left GTC controller. o Select Utilities. o Select Setup. o Select Avionics Status. o Select the Airframe tab on the left side. o Verify that the configuration ID (CRC Number) matches the number determined in Appendix B based on the options installed in the aircraft. o Select the LRU Info tab on the left side. Verify that all the LRUs are showing green check mark. o Select the MSG button: Verify there is no DB Mismatch message present. Verify there is no Manifest message present. Verify there is no Config message present. If the initial radar trims were not zero: o Select Home on the left GTC controller. o Select Aircraft Systems. o Select Maintenance. o Enter password CACCDMS. o Select Radar Trim. Enter the Pitch and Roll trims recorded in section 1. Return to Service Testing For testing, complete section in the Garmin G3000 LMM. 8
9 Section 5 Troubleshooting This section will provide corrective actions for issues seen after the software is loaded. Substitute LRU name for ***. *** DB Error or *** DB Mismatch o Ensure that the supplemental SD cards are installed in the lower slots of the displays. o Databases do not match. o Verify which database is not the same, and reload as necessary. *** Manifest Error o Software does not match what the system is expecting. o Check work performed and reload necessary software again. *** Config o Configurations do not match what the system is expecting. o Check work performed and reload necessary configurations again. 9
10 Appendix A Determining Options Installed Note: This is with the G3000 powered up in normal mode. Caution: If any optional radio appears to have an amber X and is grayed out as in this example, then the LRU is not installed, but was previously loaded incorrectly. Determine Options Installed Single GSR56 o On either GTC 570, select the SERVICES / TELEPHONE button, then select Telephone. A single Iridium transceiver is displayed on the left side. Dual GSR56 o On either GTC 570, select the SERVICES / TELEPHONE button, then select Telephone. A double Iridium transceiver is displayed on the left & right side. GDL69 o From the Home screen of either GTC 570, touch the Weather button. Then touch Weather Selection. The option is installed if Sirius XM Settings is displayed. 10
11 Becker ADF o ADF controls are seen on the AUDIO & RADIO screen of either GTC 570. GDR66 o GDR or Datalink controls are seen on the AUDIO & RADIO screen of either GTC 570. Should appear as one of the 2 images below. It may say COM3 or GDR. HF9000 o HF9000 controls are seen on the AUDIO & RADIO screen of either GTC 570. Cabin Briefing o From the Home screen of either GTC 570, select AIRCRAFT SYSTEMS. The option is installed if Cabin Briefing is displayed. 11
12 GSR56 Weather o From the Home screen of either GTC 570, touch the Weather button. Then touch Weather Selection. The option is installed if CONNEXT WEATHER is displayed. Should be if a single or dual GSR 56 is installed. DME 2 o Second DME controls are seen on the AUDIO & RADIO screen of either GTC 570. Synthetic Vision o On the PFD, select PFD Settings, then select Attitude Overlays. Synthetic Terrain is displayed. Also, there should be an unlock SD card present. TAWS Class A o From the Home screen of either GTC 570, select the TAWS button. Then select TAWS Selection button. TAWS A is loaded if there are 6 buttons displayed on the page. Otherwise TAWS B is loaded as default. Also, there should be an unlock SD card present. Note: First image is TAWS B, and second image is TAWS A. 12
13 TCAS II o From the Home screen of either GTC 570, select the transponder button in the upper right part of the screen. TCAS II option is loaded if there are 5 buttons on the left side of the screen. Otherwise, TCAS I is loaded. Also, there should be an unlock SD card present. Note: First image is TCAS I, and second image is TCAS II. Windshear o The Windshear option can be determined by viewing the PFD during power up. During the self test, there should be a WNDSHR TEST white message just to the right of the airspeed tape. Also, there should be an unlock SD card present. Doppler & Turbulence o From the Home screen of either GTC 570, select the Weather button. Then select Weather Selection button. Select the WEATHER RADAR SETTINGS button and the TURBULENCE DETECTION button will be visible. Also, there should be an unlock SD card present. 13
14 CPDLC o The CPDLC button is available on the home screen of either GTC. Also, there should be an unlock SD card present. 14
15 Appendix B Configuration ID / CRC Numbers This section will provide details on determining the correct configuration ID or CRC number for a particular M2 aircraft based on the installed options. Through the rest of this section the number will be referred to as a CRC number for simplification. Note: Radar trims that are not at zero for both pitch and roll will cause the number to be different. Ensure they are at zero before verification. Note: Once the CRC number is verified, then the radar trims can be adjusted to the original values. See section 4 for details. Every combination of options that have been ordered or delivered is listed. If you have an aircraft that has been modified in the field that now has a combination not listed, please contact Team M2 at teamm2@txtav.com. Each option is assigned a letter to ensure accuracy when comparing the combination of options to the final number. Options Single GSR 56 (includes GDL 59) --A-- Dual GSR 56 (includes GDL 59) B GDL 69 C WX-1000 Stormscope D Becker ADF E GDR 66 F HF 9000 G Cabin Briefing H GSR 56 Weather K DME 2 M Unlock Cards Synthetic Vision (SVS) N TAWS Class A P TCAS II R Windshear S Doppler & Turbulence T CPDLC V Example: Aircraft has Single GSR, GDL 69, Becker ADF, GDR 66, GSR 56 Weather, SVS, and TCAS II. Its code should be ACEFKNR. This equates to a CRC number of 450CB
16 Option CRC Number Option CRC Number Option CRC Number AC 8D808EC9 ACKM 002A20B9 CFN 705A67B6 ACEF 461C7003 ACKMNPRST BFB15610 CFNP D6F7CAC3 ACEFK 461D07AD ACKMNPST 56B80596 CFNPT 03F4DB35 ACEFKN DC ACKMP 66C783C6 CFNPTV 7F37E14C ACEFKNPR ABAA1C20 ACKMPS 93C49438 CFNRS 0650C8A2 ACEFKNPV C5F4177B ACKMPST COC1A4AA CFNRV 5496BE47 ACEFKNR 450CB913 ACKN F CFNV EB9D6DCD ACEFKR AF ACM F CFP D7 ACEKNPRS F59FE879 AE 92B25F28 CFR 435D5744 ACF 7087D2E2 AEFK 6D8E9B3B CFRS 705A67B6 ACFGHKN 51452D5C AEFKNPSV 1A62BB7B CH D6C5F524 ACFGKMNPRST 3961C814 AEFKPSV 846C5A8F CHNP D359B91D ACFGKN 6FE619E7 AEFKPV 576F4A1D CHP 3D ACFHK 51E77E01 AEFKV F0D1E710 CM E65FDA0D ACFHKN E7DDDEED AEK 92B2F6D2 CMNPST 3CEDBEEA ACFHKNPV C9BE2507 AEKN 28A957BE CMP 4CFD3D1A ACFHKNS 14DAEF5F B CC8FFABE CMPS 79FA4D8C ACFHKNV 6320C1FA BCEFGHKM 7D407A08 CMPST A6F75DFE ACFHKS 7EE48E73 BCEFGHKMNPRSTV C00AD2CE CN 8B5D429B ACFHKV CD2A610E BCEFGHKMPRSTV 2A147B42 CNPRS 87F10694 ACFK 70886ABC BCEFGHKMPRSV FD176AD0 CNS B85A530D ACFKMNPRST A2B89A29 BCEFGHKMPRV D01A5A5E CPR C4FD9536 ACFKMNPST 39BF49AF BCEFGHKMRV 697CF751 CPRS F1FAA5A8 ACFKMNPT 0CC2392D BCEFGHKMV 0083A6D7 CR 5E ACFKMPT 76CBD851 BCEFGKM 5EE16895 CS 2263F221 ACFKMT 102E7544 BCEFGM 5EE0D08B E 91F92276 ACFKN 067ECB78 BE A22497DF EF 6EDEE5E1 ACFKNPRS 03128F71 BEGM 3DD6B028 EFGM 18B25491 ACFKNPS 9A193EF7 BEM A72D823D F 994A48C0 ACFKNPST C7164F69 C F566E1AF FGN 98A7F81B ACFKNPV E85F349C CEF AFF8A3EB FMT 4D ACFKNV 81C1D18F CEFN 45EF04D7 FN 2F40A9AC ACFKP D725CD99 CEFNV C93250AC FNRV 137D003D ACFKPR 401F1E13 CF DA6406CA FNT 5C3DBA1E ACFKPRS 6D1C2E85 CFGN D9C1B625 FNV AA83AFC3 ACFKPS 0422DE0B CFGNPRSV FT C ACFKPST 311FEE7D CFGNPRV 249B6FC3 G 25CBD3C4 ACFKR D981BB06 CFGNPT 6D5C29A4 GN BBC234B0 ACFMT 102DDD9A CFGNRV BDFE0CB6 M 433D6D9B ACHKN 04D69AD4 CFGNV 5504BC3C N 525AE641 ACHKNP 6B73FDE1 CFHN 51B97B2B NRS E851472D ACHKNPS 987E1053 CFMNPST 21EAE405 R 255DD5CF ACHKNPST C56E1EC5 CFMNPT F4EDD393 V 148D4E7D ACK 8D CFMT F85A0F9A 16
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