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____________________________________________________________ 

 

Page xiv 

 

Cirrus Perspective™ System Maintenance Manual 

Rev. E 

 

190-00920-00 

SECTION

 

6—LRU

 

REPLACEMENT

 

PROCEDURES

 

 

6.1

 

ACCESSING

 

LRUS

 

............................................................................................

 

6

‐

1

 

6.2

 

GDUS

 

..............................................................................................................

 

6

‐

2

 

6.3

 

GMA

 

347

 

........................................................................................................

 

6

‐

2

 

6.4

 

GIA

 

63W

 

.........................................................................................................

 

6

‐

2

 

6.5

 

GRS

 

77

 

............................................................................................................

 

6

‐

3

 

6.6

 

GMU

 

44

 

..........................................................................................................

 

6

‐

3

 

6.7

 

GDC

 

74A

 

.........................................................................................................

 

6

‐

3

 

6.8

 

GEA

 

71

 

............................................................................................................

 

6

‐

3

 

6.9

 

GTX

 

32/33

 

......................................................................................................

 

6

‐

4

 

6.10

 

GDL

 

69A

 

..........................................................................................................

 

6

‐

4

 

6.11

 

GSA

 

80/81

 

SERVO

 

ACTUATOR

 

........................................................................

 

6

‐

4

 

6.12

 

GTA

 

82

 

PITCH

 

TRIM

 

ADAPTER

 

........................................................................

 

6

‐

5

 

6.13

 

GCU

 

478

 

KEYPAD

 

............................................................................................

 

6

‐

6

 

6.14

 

CONFIGURATION

 

MODULE

 

............................................................................

 

6

‐

7

 

6.15

 

GEA

 

BACKSHELL

 

THERMOCOUPLE

 

.................................................................

 

6

‐

8

 

 

SECTION

 

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

 

CONFIGURATION

 

LOADING

 

.......................................

 

7

‐

8

 

7.2.2

 

GMA

 

TESTING

 

.................................................................................................

 

7

‐

9

 

7.3

 

GIA

 

63W

 

.......................................................................................................

 

7

‐

11

 

7.3.1

 

GIA

 

SOFTWARE

 

AND

 

CONFIGURATION

 

LOADING

 

.......................................

 

7

‐

12

 

7.3.2

 

GIA

 

OPTIONAL

 

EQUIPMENT

 

CONFIGURATION

 

LOADING

 

............................

 

7

‐

13

 

7.3.3

 

GIA

 

OPTIONS

 

INTERFACE

 

TESTING

 

...............................................................

 

7

‐

15

 

7.3.4

 

OPTIONAL

 

STORMSCOPE

 

FUNCTIONAL

 

TEST

 

..............................................

 

7

‐

15

 

7.3.5

 

OPTIONAL

 

SKYWATCH

 

FUNCTIONAL

 

TEST

 

...................................................

 

7

‐

17

 

7.3.6

 

OPTIONAL

 

DME

 

FUNCTION

 

TEST

 

.................................................................

 

7

‐

19

 

7.3.7

 

OPTIONAL

 

ADF

 

TEST

 

.....................................................................................

 

7

‐

20

 

7.3.8

 

TAWS

 

FUNCTIONAL

 

TEST

 

.............................................................................

 

7

‐

21

 

7.3.9

 

GARMIN

 

FLITE

 

CHART

 

FUNCTIONAL

 

TEST

 

...................................................

 

7

‐

23

 

7.3.10

 

JEPP

 

CHART

 

VIEW

 

DATABASE

 

LOCATION

 

AND

 

TEST

 

....................................

 

7

‐

24

 

Содержание Cirrus Perspective SR20

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

Страница 2: ......

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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