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Sandel SG102 Series Скачать руководство пользователя страница 26

Setup Procedures

82011-IM, REV J

Sandel SG102 & MT102 Installation Manual

Page 6-1

6

Setup Procedures

6.1

Software Configuration

6.1.1 SG102 Maintenance Adapter (USB) p/n 81032

The Sandel 81032 SG102 Maintenance Adapter is available to allow USB communication
between the setup PC and the SG102 in order to operate the Installation-Calibration software.

See the Maintenance Adapter User Guide for instructions for use.

6.1.2 SG102 Installation-Calibration Utility Software

Sandel 82011-ICU Installation-Calibration Utility software is used in conjunction with the
81032 SG102 Maintenance Adapter to support the following functions:

•

View the serial number and software version of the SG102 and MT102.

•

Selecting the default SG102 mount orientation.

•

Compass calibration.

•

Selecting Arinc 429 enhanced maintenance labels.

•

Selecting Arinc 429 Hi/Low Speed. For SG102 (MOD 2) and SG102/D

See 82011-ICUG (SG102 Installation Calibration Utility User Guide) for use of this software.

Any time changes are made to the SG102 setup or calibration, an entry must be made in the
aircraft maintenance logs by an appropriately rated person stating the action taken.

6.1.3 Mounting Orientation Select

The 82011-ICU Installation-Calibration Utility software is used to select the mounting
orientation. Follow the instructions in the User Guide.

NOTE: If the correct software orientation selection is not made the SG102 will appear to
operate properly on the ground but will malfunction during flight.

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Содержание SG102 Series

Страница 1: ...em Including SG102 D Digital SG102 MOD 2 with High Speed ARINC 429 and Reduced Initialization Time MT102 Magnetic Transducer Accessory Sandel Avionics Inc 2401 Dogwood Way Vista CA 92081 Phone 760 727...

Страница 2: ...82011 IM REV J Sandel SG102 MT102 Installation Manual Page ii This page intentionally left blank...

Страница 3: ...erational Specifications SG102 MOD 2 SG102 D 2 5 2 5 4 Operational Specifications 2 5 2 5 5 Arinc 429 Labels SG102 MOD 1 2 6 2 5 6 Arinc 429 Labels SG102 MOD 2 SG102 D 2 6 3 Installation 3 1 3 1 Unpac...

Страница 4: ...Error Codes 7 2 8 Instructions for Continued Airworthiness 8 1 9 Appendix A Post Installation Procedures 9 1 10 Appendix B Environmental Qualification 10 1 11 Appendix C Sample FAA Form 337 11 1 12 Ap...

Страница 5: ...3 2 SG102 0xx w MOD 1 1xx 2xx 3xx installed in Mounting Base Assembly 3 6 Figure 3 3 SG102 XXX w MOD 2 installed in Mounting Base Assembly 3 6 Figure 3 4 SG102 X5X SG102 D installed in Mounting Base A...

Страница 6: ...lity Images updated to include SG102 D Updated for SG102 D Updated for effectivity Updated for SG102 D Typo corrected LED Error Code table updated Updated for SG102 D List of effective drawings update...

Страница 7: ...ironmental Qualification Forms Removed aerobatic limitation mod1 E 11 FEB 2009 1 212 Update limitation note Limitation modified for reversionary or backup display D 06 NOV 2008 7 1 12 Changed initiali...

Страница 8: ...s technical characteristics components approval procedures installation considerations setup procedures checkout procedures and instructions for continued airworthiness for the SG102 This revision of...

Страница 9: ...d stay level during most flight maneuvers This means that a mechanical DG installed non level will work properly however installing with the SG102 without checking the mechanical alignment will not wo...

Страница 10: ...allation approval procedures is provided for filing with authorities 2 2 MOD Levels The SG102 models covered in this Installation Manual have been produced in several variations over time As indicated...

Страница 11: ...is accessed by the Installation Calibration Software See section 6 2 3 2 Install Kit 2 3 3 Bill of Materials SG102 Install Kit Description SPN Fixed Wing Piston Aircraft MT102 000 Fixed Wing Turbine...

Страница 12: ...3 or the applicable airworthiness requirements 2 4 4 Installation and Operational Approval Procedures For the purpose of seeking installation approval declarations should be made in the Description of...

Страница 13: ...ht 2 53 in 6 4 cm Length 6 3 in 16 0 cm excluding mating connector Weight 1 65 lbs 75 kg including connector CG 2 54 from forward face 1 1 from bottom of mounting surface SG102 MOD 2 Item Dimension Wi...

Страница 14: ...te Limits 250 sec Initialization Time Approximately 1 Minute Standard day ARINC 429 Low or High Speed Item Spec Static Pitch and Roll Accuracy 35 typical initial 2 typical after 10 minutes Dynamic Pit...

Страница 15: ...d 30 Hz min 320 Magnetic Heading 30 Hz min 324 Pitch Attitude 30 Hz min 325 Roll Attitude 30 Hz min 332 Body Lateral Acceleration 30 Hz min 350 Maintenance 1 Hz 351 Maintenance 1 Hz 352 Maintenance 1...

Страница 16: ...ed connectors and associated installation hardware are supplied by Sandel in the Installation Kit 3 2 2 Mounting Orientation The SG102 supports various mounting orientations See section 3 4 below Thes...

Страница 17: ...installation from a KG102 to an SG102 interfaced to either a Sandel SN3500 or SN4500 you must remove connections between the c j and n pins 3 3 Installation Considerations 3 3 1 General The SG102 inst...

Страница 18: ...e without the MT102 connected Any application which requires operation without a magnetic reference will not work with the SG102 Note The SG102 will not initialize unless it has communication with the...

Страница 19: ...of three feet from high noise sources and not routed with cables from high power sources D The pinout descriptions will assist you in determining installation requirements Adhere to all notes within t...

Страница 20: ...the SG102 mounting base to reproduce the same pitch and roll tilt angle as the airframe Tighten the base mounting screws friction tight Step 5 Adjust the longitudinal axis of the mounting base so that...

Страница 21: ...D installed in Mounting Base Assembly 3 8 Post Installation Summary Prior to installing the SG102 a point to point continuity check of the wiring harness should be accomplished to verify proper wiring...

Страница 22: ...Connect 4 n c Do Not Connect 22 26VAC Inverter Out Out 26VAC out 14 Hdg X Out Out Arinc 407 Out Z GND 5 Hdg Y out Out Arinc 407 Out Z GND 23 Gnd Out Shield Signal Gnd 15 Valid Gnd Out Open Collector...

Страница 23: ...used e Aircraft Power In F 15 VDC f Unused H 15 VDC h Unused J Unused j CW Sw In K 15 VDC k Slaving Meter Out L Stepper C GND OPEN M Unused m Unused N Stepper D GND OPEN n CCW Sw In P Stepper A GND OP...

Страница 24: ...power This simplifies installation in retrofit applications It is often the case that the original fluxgate wiring is routed to an existing HSI and not to the existing Gyro In this case the MT102 wiri...

Страница 25: ...ealed CPC connector which adds to the water proofness of the installation Use care when crimping and sealing the mating connector as if this is done incorrectly it will be the weak point in the instal...

Страница 26: ...the serial number and software version of the SG102 and MT102 Selecting the default SG102 mount orientation Compass calibration Selecting Arinc 429 enhanced maintenance labels Selecting Arinc 429 Hi L...

Страница 27: ...Setup Procedures 82011 IM REV J Sandel SG102 MT102 Installation Manual Page 6 2 Figure 6 1 SG102 mounting orientations...

Страница 28: ...with the Sandel SN3500 EHSI the labels are recorded by the SN3500 Data Recording function and the resulting data files can be used by the Factory to diagnose intermittent or installation related probl...

Страница 29: ...nce of primary power Absence of primary power VALID ON Flash OFF Initialized and ready for operation outputs unflagged Operating in Slaving Off mode or fast slaving Not initialized outputs flagged MAG...

Страница 30: ...r during startup when it flashes continuously If an internal failure does occur the ERROR led will flash with a number of consecutive flashes followed by a pause The flashes will continue to repeat as...

Страница 31: ...the Instructions for Continued Airworthiness prepared under the guidelines of FAA Advisory Circulars 23 1309 1 C and 25 1309 1 A which identifies potential failure modes of the Sandel Avionics Model...

Страница 32: ...MT102 Installation Manual Page 9 1 9 Appendix A Post Installation Procedures After all wiring has been verified and the SG102 has been installed into the mounting base the included software must be us...

Страница 33: ...3 1 B PASS Operational Shock and Crash Safety 7 0 B PASS Vibration 8 0 S LM H R PASS 160E Section 8 5 1 Standard Vib Cat S Curves L and M 160E Section 8 6 HLSD Curve R SAE AS396B Zone 1 Fuselage Max...

Страница 34: ...Shock and Crash Safety 7 0 B PASS Vibration 8 0 H R R BB1C C1 PASS 160E Section 8 6 HLSD Curve R 160E Section 8 7 2 Robust Curves B B1 C C1 SAE AS396B Zone 1 Fuselage Max Accel 5g 5 500Hz RESONANT FRE...

Страница 35: ...60E Section 8 8 1 SoR Curve G 160E Section 8 8 3 Rondom unknown freq Curves F F1 SAE AS396B Zone 1 Fuselage Max Accel 5g 5 500Hz RESONANT FREQUENCIES Curve G Section 8 8 1 3 Step a and e Pre Scan X 19...

Страница 36: ...ature Variation 5 0 B PASS Humidity 6 3 1 B PASS Operational Shock and Crash Safety 7 0 B PASS Vibration 8 0 H RP R BB1 CC1EE1GJ U2 FF1 PASS 160E Section 8 6 HLSD Curves R and P 160E Section 8 7 2 Rob...

Страница 37: ...SG102 AHRS or as appropriate B The Sandel Avionics SG102 is interfaced to the following equipment 1 SN4500 Primary Navigation Display By example state the following functional interface properties C...

Страница 38: ...nt This text must be modified by the installation facility to be compatible with the installed equipment SECTION I GENERAL The Sandel Avionics SG102 Attitude Heading Reference System is a compact soli...

Страница 39: ...ally be operated in the slaved mode If it is desired to operate in the unslaved mode select the Slaving Off position on the mode selector switch Adjust the heading clockwise or counter clockwise as ne...

Страница 40: ...nstalled in the aircraft maintenance records A copy must also be forwarded to Sandel Avionics Inc along with the Warranty Registration Form Part Number 82011 0137 which should be mailed after operatio...

Страница 41: ...Installation Manual Page 13 2 COMPANY NAME COMPANY ADDRESS TELEPHONE FAX Ground Test Procedures Report for Sandel Avionics SG102 and MT102 Installed in Aircraft make and model Registration No ________...

Страница 42: ...p free re settable circuit breaker labeled AHRS is clearly visible Completed _______ Comment __________________________________ Install the SG102 into the mounting base and verify that the unit instal...

Страница 43: ..._____________ Verify that during the initialization period the MAG LED is illuminated Completed _______ Comment __________________________________ Verify that during the initialization period the ERRO...

Страница 44: ..._____ Comment __________________________________ 13 2 EMI RFI Test Procedures 13 2 1 NAV COM Testing Apply power to the avionics bus and ensure that all electrical equipment including the SG102 and MT...

Страница 45: ...______________________________ 13 2 2 General Testing Observe any unusual interaction between the transponder DME ADF or Marker Beacon receivers and the SG102 when switching power to any equipment Com...

Страница 46: ...dated note 4 82011 10 2 B Sandel SN3500 4500 Data Outputs ARINC 407 schematic updated for applicability 82011 10 3 B Bendix King KG102 Replacement MT102 Installation Block Diagram Added note 3 for app...

Страница 47: ...ed to connect to a laptop PC during final installation calibration of the SG102 During calibration the MAINT pin must be grounded The DB9 may be remotely mounted in the cockpit if desired NOTE The DB...

Страница 48: ...429 data may be routed to other equipment in the aircraft as needed The ARINC 407 heading output supports a maximum of 2 CT loads 5 The SG102 inverter output is limited to 5VA maximum load ARINC 429...

Страница 49: ...l SG102 KI525 KI525A MT 102 Fluxgate XYZ NEW DC POWER 2 Wire Retained CT 2 Wire retained DATA 3 Wire Re Routed BEFORE AFTER Note 1 For detail MT102 connection see sheet 1 2 Other wiring from KG102 sys...

Страница 50: ...ERWISE SPECIFIED 1 This drawing is for reference to existing KCS 55 wiring when replacing a KG102 with an SG102 For additional KCS 55 55A information consult original manufactures installation manual...

Страница 51: ...ginal manufactures installation manual 2 If a KI525 indicator is not installed this wiring is not required See sheet 1 3 The KMT112 fluxgate is removed The circled items are re routed wires 4 A 5 amp...

Страница 52: ...D ON NEXT ASSY 1 2 3 4 5 6 7 8 8 7 6 5 4 3 2 1 REVISIONS REV DESCRIPTION APPROVED VISTA CA A 82012 M Wiley DWG NO 3T1Z4 NOTES ASME Y14 5M 1994 APPLIES 1 INSTALL UNIT IN MAGNETICALLY REMOTE MAGNETICALL...

Страница 53: ...CORDING OR IN CONNECTION WITH ANY INFORMATION STORAGE OR RETRIEVAL SYSTEM WITHOUT THE PERMISSION IN WRITING FROM SANDEL AVIONICS COPYRIGHT AN UNPUBLISHED WORK SANDEL AVIONICS CAD FILE INITIAL RELEASE...

Страница 54: ...5 00 2 68 FRONT VIEW TOP VIEW SG102 XXX MOD 1 D C B A A B C D SCALE 1 2 NOTED SIZE CAGE CODE B REV 21 22 23 24 25 26 27 28 28 27 26 25 24 23 22 21 VISTA CA 90171 C DWG NO 3T1Z4 SHEET 2 OF 4 CAD FILE...

Страница 55: ...00 2 40 2 53 FRONT VIEW TOP VIEW SG102 XXX MOD 2 D C B A A B C D SCALE 1 2 NOTED SIZE CAGE CODE B REV 31 32 33 34 35 36 37 38 38 37 36 35 34 33 32 31 VISTA CA 90171 C DWG NO 3T1Z4 SHEET 3 OF 4 CAD FI...

Страница 56: ...5 00 2 40 2 53 FRONT VIEW TOP VIEW SG102 D XXX D C B A A B C D SCALE 1 2 NOTED SIZE CAGE CODE B REV 41 42 43 44 45 46 47 48 48 47 46 45 44 43 42 41 VISTA CA 90171 C DWG NO 3T1Z4 SHEET 4 OF 4 CAD FILE...

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