Garmin Cirrus Perspective SR20, Line Maintenance Manual

Page 1: ...190 00920 00 September 2009 Revision E CIRRUS PERSPECTIVE LINE MAINTENANCE MANUAL SR20 SR22 SR22TN...

Page 2: ......

Page 3: ...printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision heret...

Page 4: ...____________________________________________________________ Page ii Cirrus Perspective System Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 5: ...n Option to Ice Protection Installation Option D 4 24 09 Cover Added SR20 to title vi Changed GDU software version from 9 01 to 9 14 1 1 1 Added SR20 to opening paragraph 2 2 1 Added SR20 to opening p...

Page 6: ...L group in Table 4 1 4 4 5 Updated figure 4 4 5 Global Changed all references of PFD1 to PFD Removed all references to PFD2 Changed all PFDs to PFD Every table that includes replacing the master confi...

Page 7: ...one 7 7 35 Added SR20 to step one 7 7 43 Removed references placing the PFD in configuration mode in section 7 5 2 1 7 7 46 Added NH and FIKI to step 12 Added step c SR22 only Oil Temperature Sensors...

Page 8: ...nt Content ix GDU software version to 10 0 1 1 1 Page 1 1 changed name of SR22T to SR22 Turbo Normalized 2 2 1 Changed name of SR22T to SR22 Turbo Normalized 4 4 2 Added statement at the end of sectio...

Page 9: ...1 Port Status Tests and added new screen shots to support text 10 Global Changed name of SR22T to SR22 Turbo Normalized 10 25 Added section 10 7 Navigation Databases for GDU 10 0 10 27 Added Pre GDU...

Page 10: ...ev E 190 00920 00 DOCUMENT PAGINATION Section Pages Front Matter I to xviii Section 1 1 1 to 1 2 Section 2 2 1 to 2 10 Section 3 3 1 to 3 6 Section 4 4 1 to 4 8 Section 5 5 1 to 5 118 Section 6 6 1 to...

Page 11: ...etain a charge shall be discharged only when such grounding does not result in equipment damage If a test connection to energized equipment is required make the test equipment ground connection before...

Page 12: ...h a special anti reflective coating which is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the...

Page 13: ...E UNIT 2 4 2 7 GTX 32 33 TRANSPONDERS 2 5 2 7 1 GTX 32 TRANSPONDER 2 5 2 7 2 GTX 33 TRANSPONDER 2 5 2 8 GRS 77 ATTITUDE HEADING AND REFERENCE UNIT AHRS 2 5 2 9 GMU 44 MAGNETOMETER 2 6 2 10 GDL69 69A S...

Page 14: ...AGE GROUPS AND PAGES 4 2 4 4 SECURE DIGITAL SD CARDS 4 4 4 5 SET AND ACTIVE COMMANDS 4 5 4 5 1 SET AND ACTIVE COMMANDS 4 5 4 6 CONFIGURATION STATUS 4 6 4 7 DATA TRANSMISSION INDICATORS 4 6 SECTION 5 T...

Page 15: ...ALERTS 5 72 5 9 3 GMU 44 RELATED ALERTS 5 73 5 10 GDC 74A RELATED ALERTS AND PROBLEMS 5 74 5 10 1 COMMON PROBLEMS 5 74 5 10 2 GDC 74A RELATED ALERTS 5 74 5 11 GDC 74A FIELD CALIBRATION UTILITY 5 75 5...

Page 16: ...CTION 7 LRU SOFTWARE INSTALLATION AND TESTING 7 1 GDU 1240A 7 2 7 1 1 GDU SOFTWARE LOADING 7 2 7 1 2 GDU CONFIGURATION LOADING 7 2 7 1 3 GDU TESTING 7 7 7 2 GMA 347 7 8 7 2 1 GMA SOFTWARE AND CONFIGUR...

Page 17: ...4 4 GRS AHRS TESTING 7 44 7 5 GDC 74A 7 46 7 5 1 GDC SOFTWARE AND CONFIGURATION LOADING 7 46 7 5 2 GDC TESTING 7 47 7 6 GEA 71 7 49 7 6 1 GEA SOFTWARE AND CONFIGURATION LOADING 7 49 7 6 2 GEA TESTING...

Page 18: ...2 8 2 2 DUAL GIA TEST PROCEDURE 8 2 8 3 DISPLAY TESTING 8 3 8 3 1 MFD DISPLAY TEST PROCEDURE 8 3 8 3 2 PFD DISPLAY TEST PROCEDURE 8 3 8 4 GCU 478 TEST PROCEDURE 8 4 8 5 BACKUP PATH TESTS 8 4 8 5 1 PO...

Page 19: ...NAL SYSTEMS ACTIVATION 10 8 10 5 SOFTWARE LOAD CONFIRMATION 10 22 10 6 AIRCRAFT REGISTRATION NUMBER ENTRY GTX33 OPTION ONLY 10 24 10 7 NAVIGATION DATABASES 10 25 10 8 AVIATION DATABASE LOADING PRE GDU...

Page 20: ...____________________________________________________________ Page xviii Cirrus Perspective System Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 21: ...e P N 190 00821 00 1 1 MANUAL ORGANIZATION Section 1 Introduction Section 2 LRU Descriptions Section 3 System Overview Section 4 Configuration Mode Section 5 Troubleshooting Section 6 Replacement Proc...

Page 22: ...tion seven gives details on how to install configure and test software for a replacement LRU Sections eight and nine present return to service tests and periodic maintenance procedures Section 10 desc...

Page 23: ...1040A MFD PFD 10 Display GDC 74A 1 Air Data Computer GDC 74A 2 Air Data Computer OPT GRS 77 1 AHRS GRS 77 2 AHRS OPT GIA 63W 1 GPS Com Nav GIA 63W 2 GPS Com Nav GMA 347 Audio Panel GCU 478 Keypad GTX...

Page 24: ...as the PFD This PFD communicates with the GDU 1240A 20 1040A 20 MFD and with the on side GIA 63W Integrated Avionics Unit through a High Speed Data Bus HSDB connection 2 2 GDU 1240A 20 1040A 20 1 Fig...

Page 25: ...are received through a RS 232 digital interface with the GIA 63W 2 4 GIA 63W INTEGRATED AVIONICS UNIT IAU WAAS Enabled Figure 2 4 GIA 63W Integrated Avionics Unit The GIA 63W is the central Integrate...

Page 26: ...on to the system using data received from the pitot static system and the OAT probe The GDC 74A communicates with the GIA 63Ws GDU 1240As and GRS 77s using an ARINC 429 digital interface 2 6 GEA 71 EN...

Page 27: ...nsponder 2 7 1 GTX 32 Transponder The GTX 32 ATCRBS Transponder provides Mode A and C capabilities for ATC and TCAS I surveillance requirements The GTX 32 interfaces with the No 1 and No 2 GIA 63W LRU...

Page 28: ...ence systems AHRS that provides aircraft attitude roll pitch and heading angular rate and acceleration information to the GIAs and GDU 1240A LRUs 2 9 GMU 44 MAGNETOMETER Figure 2 10 GMU 44 Magnetomete...

Page 29: ...D and PFD inset map The GDL 69A communicates with the MFD through an HSDB connection A subscription to the XM satellite radio service is required before the GDL 69A can be enabled 2 11 GSA 80 81 AFCS...

Page 30: ...ontrol system via cables chains push rods or other means and transmits the power from the motor in the servo actuator to the flight controls when engaged The GSM 85A is a mechanical appliance with no...

Page 31: ...de select keys and a thumbwheel encoder The GMC 705 sends over an RS 232 serial data bus the switch status information to be used elsewhere in the Perspective System The CDU Control Display Unit defin...

Page 32: ...2 16 MISCELLANEOUS LRUs Figure 2 17 GRT 10 Remote Controller and GRC 10 Wireless Transceiver 2 16 1 GRC 10 XM Remote Control The GRC 10 allows a passenger to interface with the GDL XM radio without in...

Page 33: ...ion describes the basic characteristics of the Perspective System Figures 3 1 through 3 3 illustrate system interconnect block diagrams showing single and dual AHRS and ADC configurations Figure 3 1 D...

Page 34: ...____________________________________________________________________ Page 3 2 Cirrus Perspective Line Maintenance Manual Figure 3 2 Dual AHRS Dual ADC Configuration Rev E 190 00920 00...

Page 35: ...____________________________________________________________________ Figure 3 3 GFC 700 System Interface Cirrus Perspective Line Maintenance Manual Page 3 3 190 00920 00 Rev E...

Page 36: ...s If either of these external measurements is unavailable or invalid the GRS 77 uses air data information for attitude determination Four GRS 77 modes of operation are available and depend upon the co...

Page 37: ...rface and the mode selection occurs via the GMC 705 controller 3 3 S TEC 55X 55SR AUTOPILOT The Perspective System can interface with the S TEC 55X 55SR Autopilot to provide the following information...

Page 38: ...TION AND COMMUNICATION SYSTEM The GIAs contain VHF COM VHF NAV and GPS receivers COM and NAV audio is sent via digital audio to the GMA 347 Audio Panel GPS information is sent to the GRS 77 AHRS and b...

Page 39: ...ing documents for detailed information regarding system control and operation Garmin GFC 700 Cirrus SR20 SR22 SR22T Airplane Flight Manual Supplement Garmin Cirrus SR20 SR22 SR22T Cockpit Reference Gu...

Page 40: ...pages have commands or selections that are activated by display softkeys Figure 4 2 If a softkey is associated with a command that command will be displayed directly above the key A grayed out softke...

Page 41: ...tion Maintenance Log GDU RS 232 ARINC 429 Config GDU Status GDU Test Diagnostics Serial Ethernet I O Video Alert Configuration Airframe Configuration TAWS B Setup GIA RS 232 ARINC 429 Config RS 485 Co...

Page 42: ...d manually Be careful when using the card during maintenance The system is designed to immediately initialize the card upon power up Pay attention to all on screen prompts to avoid possible loss of da...

Page 43: ...VE columns during troubleshooting Certain problems can be resolved by pressing the SET ACTV softkey which reloads settings to the specific LRU this can also be accomplished by reloading the configurat...

Page 44: ...ure 4 5 Configuration Confirmation Prompts 4 7 DATA TRANSMISSION INDICATORS Several configuration pages use an indicator light system to show discrete ON OFF data and or hardware component status Unle...

Page 45: ...____________________________________________________________________ Cirrus Perspective Line Maintenance Manual Page 4 7 190 00920 00 Rev E Figure 4 7 Loss of Communication Indication...

Page 46: ...____________________________________________________________________ Page 4 8 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 47: ...TION 5 TROUBLESHOOTING This section provides troubleshooting guidance for failed LRU s 5 1 CIRRUS PERSPECTIVE ALERTING SYSTEM 5 1 1 Display Fields A red X through a display field such as COM frequenci...

Page 48: ...errors before proceeding Swap GIA1 and GIA2 and reconfigure If problem follows GIA1 replace GIA1 Check Ethernet interconnect from GIA1 to PFD and unit connector pins for faults If problem persists re...

Page 49: ...state in the cabin 2 Turn to the MFD AUX GPS STATUS page and check the GPS strength bars on both GPS receivers If the signal strength levels are erratic disappear and reappear rapidly or switch betwe...

Page 50: ...232 interconnect lines Replace the GTX 32 33 AIRSPEED FAIL ALTITUDE FAIL VERT SPEED FAIL GDC 74A 1 or Optional 2 Check PFD Alert Window for PFD MFD or GDC configuration software or failed data path er...

Page 51: ...input Check to see if the GPS has acquired at least four satellites has a 3D navigation solution and a DOP of less than 5 0 Check for metal objects tool boxes power carts nearby large steel structure...

Page 52: ...r after moving aircraft away from metal objects to determine if metal objects were the source of the interference Allow up to five minutes for the heading to reinitialize Is the aircraft stationary if...

Page 53: ...ed engine airframe sensors that receive 5V 10V or 12V power from the GEA tach sensor MAP sensor Fuel Flow sensor oil pressure sensor and pitot heat sensor The configuration and calibration boxes shoul...

Page 54: ...es and annunciations not covered in this Line Maintenance Manual Figure 5 2 Messages Annunciations In normal mode the system displays a variety of system messages and or annunciations System messages...

Page 55: ...AILED PATH message is triggered by a timeout of any digital channel The channels that are checked are displayed on the following pages in configuration mode 1 GDU RS 232 ARINC 429 CONFIG PFD and MFD 2...

Page 56: ...below 5 4 Data Path Indications on the Main and GIA Configuration Pages NOTE Pre GDU 9 11 software uses solid green black and red indicator boxes on the configuration pages Post GDU 9 11 software use...

Page 57: ...a Path Configuration Page displays port status and information The System Data Paths Configuration page Figures 5 4 through 5 7 displays the following data when the A429 CAN RS 232 or RS 485 data path...

Page 58: ...Perspective Line Maintenance Manual Rev E 190 00920 00 A text field indicating the following port status o OK if the port is communicating o FAIL if the port is not communicating o N A if the port is...

Page 59: ...__________________________________________________________________ Cirrus Perspective Line Maintenance Manual Page 5 13 190 00920 00 Rev E Figure 5 5 CAN Data Path Page Figure 5 6 RS 232 Data Path Pag...

Page 60: ...____________________________________________________________________ Page 5 14 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Figure 5 7 RS 485 Data Path Page...

Page 61: ...row ordered from left to right o A text field indicating the LRU name in the column o A drop down selectable field indicating the expected LRU for each HSDB port o A white text field indicating the cu...

Page 62: ...S 232 ARINC 429 Configuration Page PFD1 2 and MFD Figure 5 9 Main RS 232 ARINC 429 Configuration Page The Main RS 232 ARINC 429 Configuration Page Figure 5 9 troubleshooting tables show channel LRU st...

Page 63: ...ap PFD and MFD to see if the problem is in the PFD Replace original PFD if box turns green after swapping displays Replace the GCU PFD GCU 478 data path functionality is unknown Reload PFD configurati...

Page 64: ...r swapping units Swap PFD and MFD to see if the problem is in the PFD Replace original PFD if box turns green after swapping displays Check the PFD GRS 77 1 interconnect wiring and unit connector pins...

Page 65: ...the GCU is powered on by pressing the ANN TEST softkey on the MFD AUX SYSTEM STATUS page to see if the key indicators turn on If GCU will not power on remove unit and make sure power and ground are p...

Page 66: ...powered on by pressing the ANN TEST softkey on the MFD AUX SYSTEM STATUS page to see if the key indicators turn on If GMC will not come on remove unit and make sure power and ground are present at the...

Page 67: ...tatus is OK using the AUX SYSTEM STATUS PAGE on the MFD If there is a red x troubleshoot why the GRS is offline before proceeding Make sure the GRS77 2 connecter is secure and proper wire harness stra...

Page 68: ...oftware error messages Correct any errors before proceeding Make sure the GDC 74 2 status is OK using the System Status Page on the MFD If there is a red x troubleshoot why the GDC is offline before p...

Page 69: ...ore proceeding Make sure the GDC 74 1 status is OK using the AUX SYSTEM STATUS page on the MFD If there is a red x troubleshoot why the GDC is offline before proceeding Swap GIA1 and GIA2 reconfigure...

Page 70: ...GIA1 RDM interconnect wiring and connector pins for faults Replace RDM if problem remains GIA1 RDM output data path is not monitored A black box is normal CHNL 5 GTX 32 33 1 GIA1 GTX 32 33 1 data pat...

Page 71: ...on the MFD If there is a Red X troubleshoot why the GRS is offline before proceeding Make sure the GRS77 1 connecter is secure and proper wire harness strain relief is provided Swap GIA1 and GIA2 rec...

Page 72: ...eding Make sure the GMA 347 status is OK using the AUX SYSTEM STATUS PAGE on the MFD If there is a Red X troubleshoot why the GRS is offline before proceeding Swap GIA1 and GIA2 Reconfigure both GIA s...

Page 73: ...oftware error messages Correct any errors before proceeding Make sure the GDC 74A 1 status is OK using the AUX SYSTEM STATUS page on the MFD If there is a Red X troubleshoot why the GDC is offline bef...

Page 74: ...rect any errors before proceeding Make sure the GDC 74A 1 status is OK using the AUX SYSTEM STATUS page on the MFD If there is a Red X troubleshoot why the GDC is offline before proceeding Swap GIA1 a...

Page 75: ...GE on the MFD If there is a Red X troubleshoot why the GRS is offline before proceeding Make sure the GRS77 1 connecter is secure and proper wire harness strain relief is provided Swap GIA1 and GIA2 R...

Page 76: ...on or software error messages Correct any errors before proceeding Make sure the GDC 74A 2 status is OK using the AUX SYSTEM STATUS page on the MFD If there is a Red X troubleshoot why the GDC is offl...

Page 77: ...X SYSTEM STATUS PAGE on the MFD If there is a Red X troubleshoot why the GRS is offline before proceeding Make sure the GRS77 2 connecter is secure and proper wire harness strain relief is provided Sw...

Page 78: ...eeding Make sure the GDC 74A 2 status is OK using the AUX SYSTEM STATUS page on the MFD If there is a Red X troubleshoot why the GDC is offline before proceeding Swap GIA1 and GIA2 Reconfigure both GI...

Page 79: ...ck PFD Alert Window for GIA configuration or software error messages Correct any errors before proceeding Swap GIA1 and GIA2 Reconfigure both GIA s at their new locations to see if the problem is in t...

Page 80: ...ct wiring and connector pins for faults Troubleshoot detector according to manufacturer s instructions if problem remains GIA2 Guardian data path functionality is unknown Reload GIA2 configuration fil...

Page 81: ...SYSTEM STATUS PAGE on the MFD If there is a Red X troubleshoot why the GRS is offline before proceeding Make sure the GRS77 2 connecter is secure and proper wire harness strain relief is provided Swa...

Page 82: ...ceeding Make sure the GMA 347 status is OK using the AUX SYSTEM STATUS PAGE on the MFD If there is a Red X troubleshoot why the GMA is offline before proceeding Swap GIA1 and GIA2 Reconfigure both GIA...

Page 83: ...Check PFD Alert Window for GIA configuration or software error messages Correct any errors before proceeding Swap GIA1 and GIA2 Reconfigure both GIA s at their new locations to see if the problem is i...

Page 84: ...rect any errors before proceeding Make sure the GDC 74A 1 status is OK using the AUX SYSTEM STATUS page on the MFD If there is a Red X troubleshoot why the GDC is offline before proceeding Swap GIA1 a...

Page 85: ...E on the MFD If there is a Red X troubleshoot why the GRS is offline before proceeding Make sure the GRS77 1 connecter is secure and proper wire harness strain relief is provided Swap GIA1 and GIA2 Re...

Page 86: ...on or software error messages Correct any errors before proceeding Make sure the GDC 74A 2 status is OK using the AUX SYSTEM STATUS page on the MFD If there is a Red X troubleshoot why the GDC is offl...

Page 87: ...PAGE on the MFD If there is a Red X troubleshoot why the GRS is offline before proceeding Make sure the GRS77 2 connecter is secure and proper wire harness strain relief is provided Swap GIA1 and GIA...

Page 88: ...is not functioning correctly Check PFD Alert Window for GIA or GEA configuration or software error messages Correct any errors before proceeding Make sure the GEA status is OK using the AUX SYSTEM STA...

Page 89: ...ake sure all GSA GTA servo statuses are OK using the AUX SYSTEM STATUS PAGE on the MFD If one or all show a Red X troubleshoot why the servos are offline before proceeding Swap GIA1 and GIA2 Reconfigu...

Page 90: ...software error messages Correct any errors before proceeding Make sure the GEA status is OK using the AUX SYSTEM STATUS PAGE on the MFD If there is a Red X troubleshoot why the GEA is offline before p...

Page 91: ...ed on even in a monitoring state in the cabin Cycle power If GDU recovers observe display for yellow text containing error information at the top of the screen If message indicates that software needs...

Page 92: ...l facing to the right do not attempt to remove Return the unit to Garmin for repair A button knob joystick does not appear to function Go to the GDU TEST page in configuration mode and make sure the b...

Page 93: ...ttom slot of the display and insert in the top slot If the problem is resolved the bottom card slot is dirty or has failed Try reinserting the card multiple times in the bottom slot to clean the card...

Page 94: ...if the top slot if unused or replace the display Swap with a supplemental data card from another display in the same system If problem moves to the other display reload the database or replace all th...

Page 95: ...pplemental data card from the bottom slot of the display and insert in the top slot If the problem is resolved the bottom card slot is dirty or has failed Try reinserting the card multiple times in th...

Page 96: ...isplay Reload the Jeppesen ChartView database onto the card MFD1 DB ERR MFD1 Terminal Procs database error exists The MFD has encountered an error in the Terminal Procedures database Make sure the sup...

Page 97: ...Aviation database version mismatch Xtalk is off The system has found the Jeppesen aviation database in the PFD and MFD do not match Load the same cycle of aviation database to all displays DB MISMATCH...

Page 98: ...erent airport terrain database types installed CAS INOP The system has found the PFD and or MFD software versions do not match Reload PFD and MFD software The Aviation databases do not match in both d...

Page 99: ...LING has poor cooling Reducing power usage PFD has exceeded its operating temperature range Check cooling fan and wiring for proper operation Replace cooling fan if unable to determine if operating co...

Page 100: ...ow for database error Messages Correct all errors before proceeding Check display Ethernet interconnect wiring and pins for faults Replace PFD with a known good unit to verify location of problem If p...

Page 101: ...system has determined the MFD needs service Make sure the MFD connector is fully seated and locked If the unit was started in a very dark environment the photocells may not have enough light to initi...

Page 102: ...e enough light to initially raise the CCFT level Go to the GDU STATUS page in configuration mode make sure the CCFT CRNT 1 2 levels are above 50 If the CCFT levels are not above 50 apply light to the...

Page 103: ...r Config service req d The system has detected a PFD configuration mismatch Reload PFD configuration files from SD Loader Card Reload system configuration files by pressing the UPDT CFG softkey on the...

Page 104: ...by pressing the UPDT CFG softkey on the Configuration Upload Page in the System Page Group to load configuration files into the configuration module If message persists check config module wiring for...

Page 105: ...ain Aviation Database or GDU SW mismatch has not occurred If a mismatch has occurred load correct database software files or replace all the supplemental database cards as a set TAWS TEST TAWS system...

Page 106: ...m one electrical system or component refer to the Cirrus airframe maintenance manual Make sure the NAV COM squelch is not open Make sure the ADF and DME audio is not active Make sure the marker beacon...

Page 107: ...transmitters COM bleed over may occur if this option is enabled If the box is black highlight MUTE AUDIO ON TX with the cursor and press the ENT key to turn the box green Speaker Cuts Out Reduce the...

Page 108: ...A 347 needs service Replace the GMA 347 GMA1 FAIL GMA 1 is inoperative The system has detected a failure in GMA 347 Make sure the 347 is receiving power Make sure both GIAs are receiving power Make su...

Page 109: ...box is black highlight MUTE AUDIO ON TX with the cursor and press the ENT key to turn the box green 5 8 1 1 COM Adjustment Procedure The COM Calibration Procedure is not a required procedure and is no...

Page 110: ...he calibration data values and must be accomplished prior to making any changes Failure to do so may allow COM calibration values to be inadvertently stored into incorrect memory locations requiring G...

Page 111: ...ime Setup Page If date and time are incorrect enter the correct date and time Switch GIA1 and GIA2 to verify location of problem If problem follows unit clear the GPS almanac by performing the followi...

Page 112: ...a coupler and cabling for faults 5 8 4 G S Symptom Recommended Action Weak G S receiver Set up a NAV COM Ramp Test Set to radiate a test signal Switch GIA1 and GIA2 to verify location of problem If pr...

Page 113: ...the push to talk switch s again to cycle its operation Check push to talk switch s and wiring Switch GIA2 and GIA1 to verify location of problem If problem follows the unit replace GIA2 Check GIA1 GM...

Page 114: ...S1 needs service Return unit for repair The system has detected a failure in G S1 receiver Replace GIA1 G S2 SERVICE G S2 needs service Return unit for repair The system has detected a failure in G S1...

Page 115: ...replace GIA1 If problem does not follow the unit check GPS1 antenna and cabling GPS2 FAIL GPS2 is inoperative The system has detected a failure in GPS2 receiver Switch GIA1 and GIA2 to verify location...

Page 116: ...tion instructions If problem persists check config module harness for faults and replace if necessary GIA2 CONFIG GIA2 audio config error Config service req d HW MISMATCH GIA hardware mismatch GIA1 co...

Page 117: ...connector for bent pins If no damage can be found replace GRS 77 configuration module If problem persists replace the GRS 77 Attitude appears unstable Make sure a cell phone or a device using cell pho...

Page 118: ...ckup GPS information GRS 77 1 is not receiving backup GPS information from either GIA 63W AHRS1 GPS AHRS operating exclusively in no GPS mode The GRS 77 is operating in the absence of GPS AHRS1 GPS AH...

Page 119: ...model database version mismatch Reference Garmin SB 0533 for update instructions 5 9 3 GMU 44 Related Alerts Message Cause Solutions MANIFEST GMU1 software mismatch Communication Halted The system ha...

Page 120: ...replace Note Both units may individually be in spec but show a difference in altitude Do not return a GDC 74A to Garmin for service if not outside limits If GDC is outside limits recalibration may be...

Page 121: ...ed on the bench not in the aircraft at room temperature The GDC 74 X Field Calibration utility should only be used to correct errors due to altitude drift If the drift is greater than the limits defin...

Page 122: ...file Procedure 1 Connect the GDC 74A to the pressure control system 2 Connect the GDC 74A to the PC serial port using the GDC 74A PC Interface Cable Figure 5 10 3 Connect the GDC 74A PC Interface Cabl...

Page 123: ..._ HHMMSS txt This file can be used by Garmin to restore the unit to the original settings if necessary 10 After the full backup file has been created the Prepare To Take Measurements screen appears wh...

Page 124: ...er the 11 000 feet calibration is complete the Set altitude to 30 000 ft screen appears 18 According to the on screen instructions set the pressure control system to a pressure altitude of 30 000 feet...

Page 125: ...to confirm message Figure 5 16 Field Calibration Result Screen 25 Return the pressure control system to ambient pressure before disconnecting the pitot and static lines from the GDC 74A 26 Click on E...

Page 126: ...o restore to the unit and click Open Figure 5 17 Calibration Files Screen 4 Select the Serial Port on the PC that will be used to communicate with the GDC 74 X and click OK A progress bar screen appea...

Page 127: ...ted in the C Garmin directory or in the same directory where the GDC_FieldCal exe file resides Email copies of these files to avionics garmin com Please enter GDC 74 X Field Calibration Data in the su...

Page 128: ...GEA 71 configuration mismatch See Section 7 for instructions on configuration If problem persists check config module harness for faults and replace if necessary MANIFEST GEA1 software mismatch Commu...

Page 129: ...nsor ALT1 ALT2 and BAT1 shunts in question has been energized at operating voltage but is isolated from current flow both high and low inputs to the GEA should be at the same high voltage On the MFD 1...

Page 130: ...was in normal mode If the channel is calibrated and the calibration setup is correct this parameter should be near zero and fluctuation should be minimal Be sure to take note of the range of fluctuat...

Page 131: ...gure 5 23 is displayed Do not perform any actions until this is complete Figure 5 23 Configuration Verification Processing 10 When the configuration is complete press the ENT key to confirm Figure 5 2...

Page 132: ...a GTX33 make sure the aircraft registration is present in the GTX Configuration page If error is still present reload config files from a loader card See Section 7 MANIFEST GTX1 software mismatch Comm...

Page 133: ...e Make sure unit is active Make sure the signal number is 2 or 3 If it is 0 or 1 check the GDL 69 69A antenna and cabling for faults Reseat the GDL 69 69A to make sure the coax connector is fully seat...

Page 134: ...guration Page in the System Group 3 Turn the Cursor on by pressing the FMS Knob 4 The GDL69 text should be flashing Press the ENT key to turn the GDL 69 off indicated by the green light box changing t...

Page 135: ...d The system has detected a GMC 705 configuration mismatch Load GMC configuration files see Section 7 Replace GMC If problem persists check config module wiring for faults and replace if necessary GMC...

Page 136: ...is encountered during the operation of the GFC 700 the pilot and technician should first evaluate the overall status and condition of the system on the AUX System Status Page MFD Observe any alert me...

Page 137: ...h Trim Axis Failure Roll Axis Failure Elevator Mistrim Down Make sure the GTA 82 is online at the AUX SYSTEM STATUS page Check the GTA 82 and trim motor servo for proper operation by exercising the pi...

Page 138: ...the operation of the system in configuration mode before starting this procedure The GFC Status Page may be used to check the status of the servos as an aid in troubleshooting To access the GIA and GS...

Page 139: ...t failed on the opposite GIA See the GIA pre flight steps for a description of the possible values for STEP on the failed GIA and for corrective actions PFT FAIL STEP Pre flight has failed because the...

Page 140: ...itch MET switch Check the MET trim switches for proper operation GIA Pre Flight Test Steps PFT Step 0 System initializing verify GFC powered This step checks to make sure the GFC is powered up Make su...

Page 141: ...ARINC 485 data lines The cross side GIA must also pass its AHRS monitoring Make sure both GIAs are online and communicating with all servos PFT Step 7 Verify cross GIA initialized This step checks to...

Page 142: ...lot disconnect is connected to all GIAs and servos and is registering 28 volts Make sure the autopilot disconnect switch is not pressed PFT Step 14 Verify servo validity This step checks to make sure...

Page 143: ...g the GSA unit pre flight test PFT If there is a fault during PFT the unit will not be able to transition to normal mode and the only way to clear this state is to cycle unit power The second grouping...

Page 144: ...lowing logs 3 Pitch Servo 5 Roll Servo 7 Yaw Servo 9 Pitch Trim Servo There are two main groupings of faults that can occur in the control processor The first grouping of faults can occur during the G...

Page 145: ...Disconnect power HALL 5 FAIL Check unit power and AP Disconnect power HALL 6 FAIL Check unit power and AP Disconnect power CURR OFFST FAIL Check unit power and AP Disconnect power SVO TYPE FAIL Check...

Page 146: ...ove the cursor to the COMMAND box and select View Maintenance Log in the drop down menu then press the ENT key The error log data will be displayed in the OUTPUT box If you see the more press any key...

Page 147: ...the recording function 11 Wait one minute for the system to save the data to the SD card 12 While you are waiting for the data to be saved to the SD card record the order of the LRU s and or Servos we...

Page 148: ...d the 55x Analog outputs from GIA2 drive the GS deviation GS flag Nav deviation Nav flag to the 55x Pitch and Roll analog steering outputs from the 55x drive the FD bar inputs to GIA2 which in turn ar...

Page 149: ...follow GPS track in GPSS mode Check ARINC 429 GPS steering input to 55x from GIA2 computer Configuration GPSSteering No FD bars shown on PFD Check FD logic output from 55x computer to GIA2 Configurat...

Page 150: ...____________________________________________________ Page 5 104 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 RDY annunciation on PFD during AHRS alignment Normal display prior to AP o...

Page 151: ..._____________________________________________________________ Cirrus Perspective Line Maintenance Manual Page 5 105 190 00920 00 Rev E Autopilot engaged in HDG mode only Autopilot driven failure annun...

Page 152: ..._________ Page 5 106 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Autopilot engaged in heading and altitude hold modes Autopilot engaged in heading and vertical speed modes Note verti...

Page 153: ..._________________ Cirrus Perspective Line Maintenance Manual Page 5 107 190 00920 00 Rev E Autopilot engaged in heading vertical speed and altitude hold armed to capture at 1500 ft Autopilot engaged i...

Page 154: ..._________________________ Page 5 108 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Autopilot has been disengaged but the flight director output from the S TEC computer can still be sel...

Page 155: ..._______________ Cirrus Perspective Line Maintenance Manual Page 5 109 190 00920 00 Rev E Valid RS 485 path used for altitude select data RS 485 path status indicator showing missing data from the 55x...

Page 156: ...erspective Line Maintenance Manual Rev E 190 00920 00 Clock sync and data configuration set to DME KN63 1 Used for mode annunciation data from the 55x computer Status unknown indication for the FD Val...

Page 157: ...output will toggle to L and T when in Localizer or Approach mode Case shown above is in VOR or Enroute mode ANNUN 4 GPS output is shown L and T which enables the S TEC 55x ARINC 429 GPS steering Show...

Page 158: ...______________________________________ Page 5 112 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Shows the analog outputs from GIA2 to the 55x that are required to be turned on Normal d...

Page 159: ...____________________________________________________________________ Cirrus Perspective Line Maintenance Manual Page 5 113 190 00920 00 Rev E Failed 55x computer condition shown...

Page 160: ...5 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26...

Page 161: ...GEA 71 Backshell Connectors 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 6...

Page 162: ...______ Page 5 116 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Figure 5 30 GDU 1240A Backshell Connector P10001 Figure 5 31 GRS 77 Backshell Connector P771 Figure 5 32 GDC 74A Backshe...

Page 163: ...117 190 00920 00 Rev E Figure 5 34 GMC 705 Backshell Connector P7101 Figure 5 35 GCU 478 Backshell Connector P4751 Figure 5 36 GSA 80 81 Backshell Connector P801 Figure 5 37 GTA 82 Backshell Connecto...

Page 164: ...____________________________________________________________________ Page 5 118 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 165: ...n LRU software part number and or version 1 Start the system in configuration mode 2 The System Status Page Figure 6 1 shows a list of LRUs in the LRU window Activate the cursor and use the FMS knob t...

Page 166: ...ve Insert a 3 32 hex drive tool into the access hole on the unit face and rotate counterclockwise until the unit can be freely pulled from the rack To install 1 Inspect connector s for damaged pins 2...

Page 167: ...secure connector in a stationary fashion 3 Fasten unit to the aircraft mounting rack 6 7 GDC 74A To remove 1 Loosen two thumb screws that secure the unit to the mounting rack 2 Disconnect Backshell as...

Page 168: ...TX 33 X body and tighten the Phillips screw 6 10 GDL 69A To remove 1 Loosen the Phillips screw to unlock unit handle 2 Pull the GDL lever up towards the top of the unit This disengages the locking stu...

Page 169: ...ening the mounting bolts or damage will occur to the servo mount requiring replacement To install 1 Inspect the output gear for abnormal wear or the absence of grease If grease is required refer to Se...

Page 170: ...remove 1 Remove the setscrew securing the keypad with a 3 32nd hex tool and carefully remove keypad 2 While supporting the keypad disconnect the connector 3 Remove the unit To install 1 Connect the c...

Page 171: ...osition 3 Insert connector into configuration module item 1 4 If the GRS configuration module is replaced proceed to Section 6 6 5 If the GDC configuration module is replaced proceed to Section 6 5 6...

Page 172: ...er Contact Garmin for assistance in determining which cards will need to be replaced 6 15 GEA BACKSHELL THERMOCOUPLE Figure 6 3 GEA Backshell Thermocouple Item Description Qty Needed Garmin Part Numbe...

Page 173: ...re stripped wire length is 1 8 prior to crimping 2 Insert newly crimped pins and wires into the appropriate connector housing location item 6 3 Place thermocouple body item 1 onto the Backshell boss i...

Page 174: ...__________________________________________________________________________ Page 6 10 Garmin Perspective Line Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 175: ...anty Approved software versions and part numbers can be found in Cirrus documentation Garmin recommends the use of SanDisk brand SD cards to load system software and configuration files If another bra...

Page 176: ...display to reinstall in the new display after loading software 7 1 1 GDU Software Loading 1 Remove the supplemental database card from the bottom slot of each GDU and the Cirrus data card from the top...

Page 177: ...Press the CLR ALL softkey at the bottom of the display ii Use the FMS knob and ENT key to select the MFD Configuration box iii Press the LOAD softkey iv When the upload is complete press the ENT key t...

Page 178: ...MFD replacement i GFC700 w YD MFD Configuration file ii GFC700 w o YD MFD Configuration file 11 Move the curser to the AIRFRAME window turn the small FMS knob to show the list of Airframe choices hig...

Page 179: ...the small FMS knob to turn to the SYSTEM UPLOAD page Activate the cursor turn the small FMS knob to show the list of Airframe choices highlight Configuration Files in the pop up box and press the ENT...

Page 180: ...ENT key to confirm the database update The following prompt is displayed 21 After the update completes the display starts in normal mode Turn off the display and remove the aviation database update SD...

Page 181: ...k the PFD and MFD displays for the following 1 Check in the top corners of the PFD and MFD to see that all COM NAV display fields are valid 2 Check to see that altitude airspeed vertical speed and OAT...

Page 182: ...n to the SYSTEM UPLOAD page 4 Activate the cursor turn the small FMS knob to show the list of airframe choices highlight the airframe model in the pop up box and press the ENT key 5 In the FILE box tu...

Page 183: ...ts and check for proper operation at all headphone locations 7 2 2 2 Transceiver Operational Check Perform a ramp test radio check by operating the installed transceivers microphone microphone key and...

Page 184: ...inner marker signals by following the test equipment manufacturer s instructions Verify that each marker audio signal is present over the headphones and speaker Verify that the outer middle and inner...

Page 185: ...ure the units without using the Cirrus Perspective software loader card 1 Apply system power insuring both MFD and PFD are in Configuration Mode 2 On the PFD use the FMS knob to navigate to the GIA RS...

Page 186: ...he PFD use the small FMS knob to turn to the SYSTEM UPLOAD page 5 Activate the cursor turn the small FMS knob to show the list of airframe choices highlight your airframe model in the pop up box and p...

Page 187: ...d load any of the following files if the aircraft is equipped with the following optional equipment For a GIA1 replacement i Oxygen GIA 1 Configuration file ii Ice Protection NH and FIKI GIA 1 Configu...

Page 188: ...f AHRS and ADC units installed on the aircraft and press the ENT key For a GIA1 replacement i Press the CLR ALL softkey at the bottom of the display ii Use the FMS knob and ENT key to select the GIA 1...

Page 189: ...fer to the WX 500 Installation Manual for troubleshooting Following successful power up verify the following modes Access to both 360 and 120 weather view modes All available ranges can be displayed A...

Page 190: ...om the WX PA mode menu then press MENU ENTER 17 Select the bottom mount antenna configuration on the WX PA keyboard A key Use the F1 and F2 keys to select the 120 NM range and press MENU ENTER to star...

Page 191: ...r of the display over the aircraft symbol 3 Verify that the system comes up in STANDBY indicating proper squat switch interconnect 4 Press the OPERATE softkey and verify that OPERATING is displayed in...

Page 192: ...or with TAS functionality 10 Using the ramp generator simulate a TA and verify the proper target display and associated Traffic Traffic audio alert 11 Provide a valid GPS signal and verify TAS True Ai...

Page 193: ...played use the large FMS knob and highlight the DME field Verify that the NAV1 NAV2 and HOLD modes can be selected by turning the small FMS knob 4 Verify that NAV1 and NAV2 frequencies are set to 108...

Page 194: ...hat the DME distance on the PFD matches the test set 7 3 7 Optional ADF Function Test This check verifies that the ADF to Garmin interface operates correctly This check is only required for SR20 SR22...

Page 195: ...r the cockpit speaker 5 Press the MENU button again and select Inhibit TAWS from the pop up menu and press ENT Verify TAWS INHB is displayed in the lower right hand corner of the PFD 6 Press the MENU...

Page 196: ...4 On the Audio Alert Configuration page use the FMS knob to activate the cursor and scroll through the MSG FIELD audio alert menu When the desired alert is selected press the ENT key on the display T...

Page 197: ...MFD then select DBASE softkey 2 Use the small FMS knob and scroll to CHART 3 Verify FliteCharts is displayed in blue text adjacent to CHART 4 Verify the FliteChart database REGION CYCLE number EFFECT...

Page 198: ...loading or updating the ChartView data via the Jeppesen website NOTE The required ChartView databases are subscription based and are to be procured by the aircraft owner directly from Jeppesen 1 Apply...

Page 199: ...e charts and select a chart for viewing by pressing the GCU ENT key Make sure the appropriate ChartView chart is displayed 7 3 11 SafeTaxi Functional Test Figure 7 6 SAFETAXI Display The maximum map r...

Page 200: ...the range knob select a range of 5000 ft or less Verify SafeTaxi display represents the current aircraft location and the airport layout 7 3 12 GIA Testing The following section applies to both GIA 63...

Page 201: ...14 Transmit for 35 seconds while monitoring GPS1 signal strength levels 15 During the transmit period verify that the GPS DR or LOI flags do not come into view on the PFD HSI and verify on the MFD tha...

Page 202: ...t directions Verify proper response from the VOR2 CDI 7 3 16 Localizer Glideslope Test 1 Simulate a localizer signal on the ramp tester Tune both NAV1 and NAV2 receivers to the ramp test frequency 2 S...

Page 203: ...irector and aircraft controls follow the CDI to the left 6 Press the CDI softkey to select the VOR2 receiver Verify that the green NAV autopilot annunciation flashes yellow then returns to default ROL...

Page 204: ...ew Repaired or Exchange GMU 44 is Installed Load software from the Cirrus Perspective software loader card if the GMU 44 was replaced with a new repaired or exchanged unit 7 4 1 GRS Software Loading a...

Page 205: ...ompt 4 After the SYSTEM STATUS page appears use the small FMS knob to turn to the SYSTEM UPLOAD page 5 Activate the cursor 6 Turn the small FMS knob to display the list of airframe choices 7 Highlight...

Page 206: ...is less than 30 knots the aircraft is considered not moving and attitude heading will become valid 3 If both 3D GPS and true airspeed are unavailable attitude heading will not become valid No configu...

Page 207: ...sening mounting rack bolts None Required Continue to Test Section Replaced the GRS 77 and loosened mounting rack bolts X X X Replaced the GRS 77 Configuration Module X X X Replaced the GMU 44 X GMU 44...

Page 208: ...ord to perform the calibration Press the following softkeys in sequence i softkey 9 ii softkey 10 iii softkey 11 iv softkey 12 c Ensure that the No 1 GRS 77 is selected d Select PITCH ROLL OFFSET then...

Page 209: ...tion procedure The magnetometer calibration procedure itself contains the logic to simultaneously survey the location for magnetic cleanliness while it is computing the magnetometer calibration parame...

Page 210: ...FMS 2 After aircraft engine startup taxi the aircraft to a properly calibrated compass rose or magnetically clean location determined previously 3 At the compass rose align the aircraft to a heading o...

Page 211: ...in the SELECT GRS UNIT window Move the cursor to the SELECT PROCEDURE window and use the FMS knob and ENT key to select MAGNETOMETER Perform the following steps on the PFD and MFD at the same time 9 U...

Page 212: ...e the PFD restarts the 18 second countdown without full completion of the previous countdown If this occurs more than once for a given station begin turning to the next station approximately 30 A mini...

Page 213: ...dvise the control tower or ground control you may temporarily not be able to receive or transmit on your COM radios during this procedure before restarting the system in config mode 2 Restart the PFD...

Page 214: ...mplete 10 The PFD informs the operator if the installation has passed or failed the vibration test If the test fails the specific measurements causing the failure are identified and associated numeric...

Page 215: ...ropriate to start the engine and turn the alternator on and then off during a portion of the test Procedures A1 B C and D are not required before performing this test Figure 7 11 Magnetometer Interfer...

Page 216: ...Sequence Elapsed Time Since Start of Test min secs Action 0 00 Test begins 0 10 Aileron full right 0 20 Aileron full left 0 30 Aileron level 0 40 Flaps down 0 50 Flaps up 1 00 Navigation lights on 1...

Page 217: ...is test 12 If the test fails the installation should be considered unreliable until the source of magnetic interference is identified and remedied When the magnetometer interference test fails record...

Page 218: ...hin 1 minute of power up as shown in Figure 7 13 provided both GPS receivers have a valid position If GPS is unavailable AHRS initialization may take as long as 2 minutes the aircraft must remain stat...

Page 219: ...___________________________________ Cirrus Perspective Line Maintenance Manual Page 7 45 190 00920 00 Rev E 7 4 4 1 Optional Second AHRS Test Press the SENSOR softkey on the PFD then select AHRS2 Figu...

Page 220: ...onfiguration Loading 1 Insert the Cirrus Perspective software loader card into top slot of the PFD 2 Apply system power insuring both MFD and PFD are in Configuration Mode 3 On the PFD press the NO so...

Page 221: ...ent to the altitude that will be displayed to the pilot on the altitude display B ALT will be used for all CFR Part 43 Appendix E tests for system altitude 3 Push the red reversionary button located b...

Page 222: ...rtical speed field on the PFD is within the tolerances specified in the table below Vertical Speed feet minute Allowed tolerance feet minute 2000 100 0 45 2000 100 4 Press the SENSOR PFD softkey and t...

Page 223: ...he MFD and PFD are in Configuration Mode 3 On the PFD press the NO softkey at DO YOU WANT TO UPDATE SYSTEM FILES prompt 4 After the SYSTEM STATUS page appears on the PFD use the small FMS knob to turn...

Page 224: ...The following tests are recommended if the unit is removed or replaced 1 Each GEA 71 sensor input must be checked with the aircraft engine off Make sure all engine information systems are valid on the...

Page 225: ...7 7 1 GTX32 33 Software and Configuration Loading 1 Insert the Cirrus Perspective software loader card into top slot of the PFD 2 Apply system power insuring both MFD and PFD are in Configuration Mod...

Page 226: ...ransponder altitude reporting system must be verified in accordance with Title 14 of the Code of Federal Regulations CFR 91 411 and 91 413 2 For the GTX 33 transponder make sure the aircraft registrat...

Page 227: ...rus Perspective software loader card into top slot of the PFD 2 Apply system power insuring both MFD and PFD are in Configuration Mode 3 On the PFD press the NO softkey at DO YOU WANT TO UPDATE SYSTEM...

Page 228: ...e channel control located in the cabin verify that you can select and deselect channels the white arrow to the left of the channel list indicates the currently selected channel Select channel 1 when c...

Page 229: ...D and PFD are in Configuration Mode 3 On the PFD press the NO softkey at DO YOU WANT TO UPDATE SYSTEM FILES prompt 4 After the SYSTEM STATUS page appears on the PFD use the small FMS knob to turn to t...

Page 230: ...n the PFD press the NO softkey at DO YOU WANT TO UPDATE SYSTEM FILES prompt 4 After the SYSTEM STATUS page appears on the PFD use the small FMS knob to turn to the SYSTEM UPLOAD page 5 Activate the cu...

Page 231: ...D and PFD are in Configuration Mode 3 On the PFD press the NO softkey at DO YOU WANT TO UPDATE SYSTEM FILES prompt 4 After the SYSTEM STATUS page appears on the PFD use the small FMS knob to turn to t...

Page 232: ...nciation is displayed in the upper left side of the PFD until the attitude comes up 3 Verify that a white PFT annunciation is displayed on the PFD after the attitude comes up as shown in Figure 7 16 N...

Page 233: ...rcuit breaker The Autopilot should disengage with abnormal disconnect alerting consisting of a continuous disconnect tone and a flashing red white AP annunciation No AFCS annunciations e g AFCS PFT an...

Page 234: ...key on the GMC 705 The command bars should be level and the control stick should be stationary very slow movement is acceptable due to the aircraft not being perfectly level 4 Turn the HDG knob to the...

Page 235: ...to disconnect the Autopilot then re engage by pressing the AP and YD keys on YD equipped aircraft 12 Externally push the tail of the aircraft to the left and observe the rudder deflection Rudder move...

Page 236: ...__________________________________________________________________ Page 7 62 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 237: ...AUX page 3 Remove the shroud 3 The following shall remain valid on the PFD Attitude and Heading from AHRS Airspeed Altitude Vertical Speed and OAT from Air Data Computer GPS Course Deviation Indicato...

Page 238: ...1 failure only the following shall flag invalid COM1 NAV1 field PFD MFD NAV1 CDI loses deviation bar PFD only AHRS1 using backup GPS alert given 6 For a GIA2 failure only the following shall flag inva...

Page 239: ...oes not disconnect if equipped Attitude and Heading remain valid from AHRS Airspeed Altitude Vertical Speed and OAT remain valid from Air Data Computer Valid Engine Instrumentation appears on PFD XPDR...

Page 240: ...akers and remove power from both displays before performing these tests Reboot the PFD and MFD by pressing and holding the 12th softkey on the MFD until the words INITIALIZING SYSTEM appear 1 Go to th...

Page 241: ...p Select the RS 232 ARINC 429 CONFIG page 9 Verify that GIA1 is selected in the SELECT UNIT field 10 View the data indicators for all configured RS 232 and ARINC 429 channels except GIA DEBUG includin...

Page 242: ...S 485 CONFIGURATION page in the GIA Page Group 15 Verify that GIA1 is selected in the SELECT UNIT field 16 Observe the data indicators for all configured RS 485 channels 17 Make sure all DATA indicato...

Page 243: ...__________________________________________________________________ Cirrus Perspective Line Maintenance Manual Page 8 7 190 00920 00 Rev E Figure 8 4 CAN RS 485 Config Page GIA2 Data Indicators...

Page 244: ...eft to right A text field indicating the LRU name in the column A text field indicating the channel name A status indicator showing o An N A indication if the monitor is on and data path status is not...

Page 245: ...__________________________________________________________________ Cirrus Perspective Line Maintenance Manual Page 8 9 190 00920 00 Rev E Figure 8 5 A429 Data Path Page Figure 8 6 CAN Data Path Page...

Page 246: ...________________________________________________________________ Page 8 10 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Figure 8 7 RS 232 Data Path Page Figure 8 8 RS 485 Data Path Pa...

Page 247: ...ow ordered from left to right o A text field indicating the LRU name in the column o A drop down selectable field indicating the expected LRU for each HSDB port o A white text field indicating the cur...

Page 248: ...__________________________________________________________________ Page 8 12 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 249: ...or Mode S transponder equipped aircraft Air Data Test Set ADTS capable of simulating altitude up to the aircraft s service ceiling GPS Indoor Repeater if outside GPS signals cannot be acquired Headset...

Page 250: ...efer to aircraft specific documentation as appropriate 9 4 GFC 700 VISUAL INSPECTION PROCEDURE 1 Remove the access panels according to Cirrus maintenance documentation 2 Inspect the servos connectors...

Page 251: ...rfaces through their range of motion to ensure freedom of movement 9 6 GDC RVSM ALTITUDE INSPECTION Operation with the GDC at RVSM altitudes requires an accuracy inspection every 12 months Refer to th...

Page 252: ...__________________________________________________________________ Page 9 4 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 253: ...solution to a problem System reconfiguration is a last resort when all other troubleshooting efforts have been exhausted 10 1 DATA CARDS Garmin recommends using SanDisk cards to load system software...

Page 254: ...hat are defined on the card Should software part numbers or versions change a new loader card part number is issued Cirrus drawings show all available combinations of hardware and loader cards for the...

Page 255: ...ONFIGURATION PROCEDURE The Perspective system is not airworthy unless software loading and configuration procedures are accomplished successfully as described in the following procedures The following...

Page 256: ...INITIALIZING SYSTEM appear in the upper left corner of the MFD release the key 5 Press the rightmost softkey on the MFD to acknowledge the prompt to load new software An Updating System Files screen...

Page 257: ...will be loaded 4 Once an airframe type is selected the cursor moves to the FILE window Turn the small FMS knob to active the drop down menu Move the cursor to highlight the appropriate aircraft model...

Page 258: ...ftware and configuration load to a new installation 6 After making sure the desired software and configuration files are checked press the LOAD softkey The system automatically begins loading software...

Page 259: ...__________________________________________________________________ Cirrus Perspective Line Maintenance Manual Page 10 7 190 00920 00 Rev E Figure 10 3 Upload Complete Window...

Page 260: ...ently loaded for a system that is NOT installed the aircraft configuration files must be reloaded For example if the ADF option is loaded and the aircraft is not equipped with an ADF the default confi...

Page 261: ...n the upload is finished press ENT to acknowledge 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes C ADF Option Follow this procedur...

Page 262: ...is finished press ENT to acknowledge 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes E SR22 TN DIN IEC 751 Oil Temperature Sensor...

Page 263: ...he status of the upload When the upload is finished press ENT to acknowledge 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes G Oxyg...

Page 264: ...the upload When the upload is finished press ENT to acknowledge 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes I S TEC 55X 55SR F...

Page 265: ...pload is finished press ENT to acknowledge 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes K Carbon Monoxide Detection Option NOTE...

Page 266: ...e 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes M Disable GDU Fan Monitoring NOTE Always load this option to deactivate the fan m...

Page 267: ...is finished press ENT to acknowledge 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes O Ice Protection Installation Option Flight In...

Page 268: ...hen the upload is finished press ENT to acknowledge 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes Q GFC 700 Option with and witho...

Page 269: ...When the upload is finished press ENT to acknowledge 6 View the SUMMARY field and ensure that all items are complete Verify that PASS appears in green at the check boxes S Single AHRS Single ADC Opti...

Page 270: ...equipped with this option 1 Activate the cursor and rotate the FMS knob once to activate the AIRFRAME menu on the System Upload page 2 Select Options from the AIRFRAME window and press ENT 3 Select Du...

Page 271: ...D 3 While holding the ENT key on the PFD and MFD restore power to the displays 4 When the words INITIALIZING SYSTEM appear in the upper left corner of both displays release the ENT keys 5 On the PFD g...

Page 272: ...t of the PFD 3 While holding the ENT key on the PFD and MFD restore power to the displays 4 When the words INITIALIZING SYSTEM appear in the upper left corner of both displays release the ENT keys 5 O...

Page 273: ...Insert this card in the upper slot of the PFD 3 While holding the ENT key on the PFD and MFD restore power to both displays by closing the PFD and MFD circuit breakers 4 When the words INITIALIZING S...

Page 274: ...o the LRU window 2 Highlight each of the following item in the LRU window and verify that the software part number and version matches the information in the appropriate Cirrus drawing use the followi...

Page 275: ..._______ GRS2 __________ _ GFC CERT GIA2 ___________ GRS2 FPGA __________ _ GFC CERT P C ___________ GSA PTCH CTL __________ _ GFC CERT P M ___________ GSA PTCH MON __________ _ GFC CERT PT ___________...

Page 276: ...under the SET and ACTIVE columns 3 Activate the cursor and highlight the ADDRESS field Use the small large FMS knobs to enter the aircraft registration number Once the correct registration number is e...

Page 277: ...SD cards to load the Navigation Database into the GDUs Do not copy the navigation database not including Chartview onto 010 00330 42 or 43 supplemental data cards to load into the GDUs Doing so may co...

Page 278: ...g prompt is displayed in the upper left corner of PFD2 3 Press the ENT key to confirm the database update The following screen is displayed 4 After the update completes the MFD starts in normal mode R...

Page 279: ...slot of the PFD 2 Apply power to the PFD The following prompt is displayed in the upper left corner of the PFD 3 Press the ENT key to confirm the database update The following prompt is displayed 4 Af...

Page 280: ...ert two Terrain Obstacle SafeTaxi FliteChart database cards into the bottom slots of the MFD and PFD respectively Refer to the appropriate Cirrus drawing for correct database card part numbers 4 Conti...

Page 281: ...that LRU part number is compatible with software version and Card Loader Refer to the General Arrangement Drawing and to Section TBD of this document Restart MFD PFD in Configuration Mode and retry s...

Page 282: ...still does not operate reference optional equipment documentation for further troubleshooting SYN VIS softkey does not appear on PFD softkey tier Verify that the PFD and MFD software versions are show...

Page 283: ...essage Cause Solution SVS SVS DISABLED Out of available terrain region SVS is disabled because the aircraft exceeded the boundaries of the loaded terrain database Ensure that operations are within the...

Page 284: ...__________________________________________________________________ Page 10 32 Cirrus Perspective Line Maintenance Manual Rev E 190 00920 00 Blank Page...

Page 285: ...COM MIC KEY In 5 INTERCOM MIC IN HI In 6 INTERCOM MIC IN LO GROUND 7 COM MIC AUDIO IN HI In 8 COM MIC AUDIO IN LO GROUND 9 COM 500 AUDIO OUT HI Out 10 COM 500 AUDIO OUT LO GROUND 11 TRANSMIT INTERLOC...

Page 286: ...31 POWER GROUND 32 COM RS 232 OUT 1 Out 33 COM RS 232 IN 1 In 34 COM REMOTE TUNE ENABLE In 35 COM AUDIO IN HI In 36 COM AUDIO IN LO GROUND 37 VOR LOC AUDIO IN HI In 38 VOR LOC AUDIO IN LO GROUND 39 A...

Page 287: ...1 VOR OBS STATOR E VOR LOC COMMON 12 VOR OBS STATOR F In 13 VOR OBS STATOR D In 14 VOR OBS STATOR G VOR LOC COMMON 15 VOR LOC SUPERFLAG Out 16 VOR LOC 500 AUDIO OUT HI Out 17 VOR LOC 500 AUDIO OUT LO...

Page 288: ...42 PARALLEL DME 100 KHZ D Out 43 PARALLEL DME 50 KHZ Out 44 SPARE 45 PARALLEL DME 1 MHZ A Out 46 PARALLEL DME 1 MHZ B Out 47 PARALLEL DME 1 MHZ C Out 48 RESERVED 49 SIGNAL GROUND 50 RESERVED 51 SPARE...

Page 289: ...29 IN 3 B In 10 MAIN ARINC 429 IN 4 A In 11 MAIN ARINC 429 IN 4 B In 12 MAIN ARINC 429 IN 5 A In 13 MAIN ARINC 429 IN 5 B In 14 MAIN ARINC 429 IN 6 A In 15 MAIN ARINC 429 IN 6 B In 16 MAIN ARINC 429 I...

Page 290: ...ut 50 MAIN RS 232 IN 4 In 51 SIGNAL GROUND 52 MAIN RS 232 OUT 4 Out 53 MAIN RS 232 IN 5 In 54 SIGNAL GROUND 55 MAIN RS 232 OUT 5 Out 56 MAIN RS 232 IN 6 In 57 SIGNAL GROUND 58 MAIN RS 232 OUT 6 Out 59...

Page 291: ...DISCRETE IN 3 In 10 DISCRETE IN 15 In 11 AP DISCONNECT IN In 12 DISCRETE IN 4 In 13 DISCRETE IN 5 In 14 DISCRETE IN 6 In 15 DISCRETE IN 16 In 16 DISCRETE IN 17 In 17 DISCRETE IN 7 In 18 DISCRETE IN 8...

Page 292: ..._____________ Page A 8 Cirrus Perspective Line Maintenance Manual Rev D 190 00920 00 37 ANNUNCIATE 14 Out 38 ANNUNCIATE 15 Out 39 ANNUNCIATE 16 Out 40 ANNUNCIATE 17 Out 41 ANNUNCIATE 18 Out 42 ANNUNCI...

Page 293: ...DIRECTOR ROLL LEFT In 12 DISCRETE IN 19A In 13 POTENTIOMETER SIGNAL IN In 14 POTENTIOMETER REF IN HI In 15 POTENTIOMETER REF IN LO In 16 DISCRETE IN 20A In 17 MAIN LATERAL DEVIATION LEFT Out 18 MAIN L...

Page 294: ...TE IN 11A In 50 DISCRETE IN 21A In 51 DISCRETE IN 22A In 52 DISCRETE IN 12A In 53 DISCRETE IN 13A In 54 DISCRETE IN 14A In 55 DISCRETE IN 15A In 56 OUTER MARKER LAMP IN In 57 MIDDLE MARKER LAMP IN In...

Page 295: ...AFCS REF HI In 6 26 VAC AFCS REF LO In 7 DIRECTIONAL GYRO MOTOR A In 8 DIRECTIONAL GYRO MOTOR B In 9 SIGNAL GROUND 10 ADF X COS In 11 ADF Y SIN In 12 ADF Z GROUND In 13 SIGNAL GROUND 14 HEADING X In...

Page 296: ...SE DATUM LO GROUND Out 50 SIGNAL GROUND 51 26 VAC DIRECTIONAL GYRO REF HI In 52 26 VAC DIRECTIONAL GYRO REF LO In 53 REMOTE ANNUNCIATE CLOCK In 54 REMOTE ANNUNCIATE DATA In 55 REMOTE ANNUNCIATE SYNC I...

Page 297: ...ETHERNET OUT 2 B Out 8 ETHERNET IN 2 A In 9 ETHERNET IN 2 B In 10 ETHERNET OUT 3 A Out 11 ETHERNET OUT 3 B Out 12 ETHERNET IN 3 A In 13 ETHERNET IN 3 B In 14 FAN MONITOR VALID In 15 REVERSIONARY MODE...

Page 298: ...OWER 2 In 42 SIGNAL GROUND 43 CONFIG MODULE CLOCK Out 44 RS 232 OUT 1 Out 45 RS 232 IN 1 In 46 RS 232 OUT 2 Out 47 RS 232 IN 2 In 48 ETHERNET OUT 4A Out 49 ETHERNET OUT 4 B Out 50 ETHERNET IN 4 A In 5...

Page 299: ...TER RS 232 OUT Out 11 GPS 1 RS 232 IN In 12 ARINC 429 OUT 3 A Out 13 ARINC 429 OUT 2 A Out 14 ARINC 429 OUT 1 A Out 15 ARINC 429 IN 1 A In 16 CONFIG MODULE DATA I O 17 CONFIG MODULE POWER OUT Out 18 A...

Page 300: ...GROUND 39 MAGNETOMETER RS 485 IN B In 40 MAGNETOMETER GROUND 41 SIGNAL GROUND 42 SIGNAL GROUND 43 SIGNAL GROUND 44 SIGNAL GROUND A 9 GMU 44 P441 View of J441 connector looking at pigtail Pin Pin Name...

Page 301: ...YSTEM ID PROGRAM 1 In 7 SIGNAL GROUND 8 DISCRETE IN 6 In 9 SIGNAL GROUND 10 RS 232 IN 1 In 11 RS 232 OUT 1 Out 12 SIGNAL GROUND 13 RS 232 IN 2 In 14 RS 232 OUT 2 Out 15 SIGNAL GROUND 16 RESERVED 17 PO...

Page 302: ...3 A Out 48 ARINC 429 OUT 3 B Out 49 SIGNAL GROUND 50 DISCRETE IN 7 In 51 SIGNAL GROUND 52 DISCRETE IN 8 In 53 SIGNAL GROUND 54 SPARE 55 AIRCRAFT POWER 1 In 56 SPARE 57 SPARE 58 AIRCRAFT POWER 2 In 59...

Page 303: ...O GROUND 13 TRANSDUCER POWER OUT LO GROUND 14 10 VDC TRANSDUCER POWER OUT Out 15 5 VDC TRANSDUCER POWER OUT Out 16 12 VDC TRANSDUCER POWER OUT Out 17 ENGINE TEMP ANALOG IN 6 HI In 18 ENGINE TEMP ANALO...

Page 304: ...LO In 52 ENGINE TEMP ANALOG IN 9 HI In 53 ENGINE TEMP ANALOG IN 9 LO In 54 ENGINE TEMP ANALOG IN 10 HI In 55 ENGINE TEMP ANALOG IN 10 LO In 56 ENGINE TEMP ANALOG IN 11 HI In 57 ENGINE TEMP ANALOG IN 1...

Page 305: ...10A Out 11 TRANSDUCER POWER OUT LO GROUND 12 TRANSDUCER POWER OUT LO GROUND 13 TRANSDUCER POWER OUT LO GROUND 14 10 VDC TRANSDUCER POWER OUT A Out 15 5 VDC TRANSDUCER POWER OUT A Out 16 12 VDC TRANSDU...

Page 306: ...CURRENT MONITOR IN 3A LO In 50 ANALOG CURRENT MONITOR IN 4A HI In 51 ANALOG CURRENT MONITOR IN 4A LO In 52 ANALOG IN 1A HI In 53 ANALOG IN 1A LO In 54 ANALOG IN 2A HI In 55 ANALOG IN 2A LO In 56 ANAL...

Page 307: ...29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 2...

Page 308: ...3 CROSS SIDE COM AUDIO LO I O 14 CROSS SIDE NAV AUDIO IN HI In 15 DME AUDIO IN HI In 16 DME AUDIO IN LO In 17 MUSIC IN 1 LEFT In 18 MUSIC IN 1 RIGHT In 19 UNSWITCHED AUDIO IN 1 HI In 20 UNSWITCHED AUD...

Page 309: ...PILOT ICS KEY In 53 RESERVED 54 ALTITUDE WARN AUDIO IN HI In 55 ALTITUDE WARN AUDIO IN LO In 56 MUSIC IN 2 LEFT In 57 MUSIC IN 2 RIGHT In 58 COM 3 AUDIO IN HI In 59 COM 3 AUDIO LO I O 60 RESERVED 61 R...

Page 310: ...ESERVED 11 PROGRAM GROUND 12 RESERVED 13 RESERVED 14 POWER GROUND 15 RESERVED 16 POWER GROUND 17 COM SWAP In 18 PROGRAM GROUND 19 RESERVED 20 RESERVED 21 CONFIG MODULE POWER OUT Out 22 RESERVED 23 PRO...

Page 311: ...50 RESERVED 51 14 V LIGHTING HI In 52 28 V LIGHTING HI In 53 AIRCRAFT POWER 1 In 54 RESERVED 55 AIRCRAFT POWER 1 In 56 RESERVED 57 GROUND RETURN 58 RESERVED 59 MARKER ANTENNA LO In 60 CONFIG MODULE C...

Page 312: ...n 8 ALTITUDE C1 In 9 ALTITUDE B2 In 10 ALTITUDE B4 In 11 ALTITUDE D4 In 12 EXTERNAL IDENT SELECT In 13 EXTERNAL STANDBY SELECT In 14 NOT USED In 15 AUDIO OUT HI Out 16 AUDIO OUT LO Out 17 SQUAT SWITCH...

Page 313: ...POWER 1 In 43 POWER GROUND 44 CURRENT TEMPERATURE PROBE IN In 45 NOT USED In 46 TIS CONNECT SELECT In 47 AUDIO MUTE SELECT In 48 ARINC 429 IN 4 A In 49 ARINC 429 IN 4 B In 50 ALTITUDE COMMON GROUND I...

Page 314: ...GROUND 5 RS 232 IN 2 In 6 RS 232 IN 3 In 7 RS 232 IN 1 In 8 RS 232 OUT 1 Out 9 DATA LINK SYSTEM ID PROGRAM 1 In 10 DATA LINK SYSTEM ID PROGRAM 2 In 11 SIGNAL GROUND 12 SPARE 13 SIGNAL GROUND 14 SPARE...

Page 315: ...55 SPARE 56 ETHERNET IN 4 B In 57 ETHERNET IN 4 A In 58 ETHERNET OUT 4 B Out 59 ETHERNET OUT 4 A Out 60 CONFIG MODULE CLOCK Out 61 AUDIO MUTE SELECT 1 In 62 AUDIO MUTE SELECT 2 In 63 AUDIO MUTE SELEC...

Page 316: ...101 connector looking at unit Pin Pin Name I O 1 RS 232 OUT 1 Out 2 RS 232 IN 1 In 3 RS 232 OUT 2 Out 4 RS 232 IN 2 In 5 POWER GROUND 6 SIGNAL GROUND 7 AIRCRAFT POWER 1 In 8 SIGNAL GROUND 9 AIRCRAFT P...