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Garmin GIA 63 Installation Manual

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GIA 63
Installation Manual
190-00303-05
November, 2010
Revision T

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  • Page 1 GIA 63 Installation Manual 190-00303-05 November, 2010 Revision T...
  • Page 2 Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express prior written consent of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic...
  • Page 3 Page Section Revision Description of Change Number(s) Number Added reference to GIA 63H and note regarding GIA 63(X) v, vi Updated mod level tables Updated to GIA 63(X) where applicable, added GIA 63 H 1-1–1-32 info and references throughout 1.4.2 Corrected weight info, added GIA 63H info 1.4.6...
  • Page 4 This manual reflects the operation of main software version 5.31 for the GIA 63 and main software version 6.00 for the GIA 63W and GIA 63H. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.

  • Page 5: Table Of Contents

    2.2 Installation Considerations ........................2-5 2.3 Rack Considerations ..........................2-9 2.4 Cabling and Wiring..........................2-10 2.5 Cooling Air ............................2-10 2.6 GIA 63 Minimum Installation Requirements ..................2-11 2.7 GIA 63W and GIA 63H Minimum Installation Requirements............2-12 2.8 Mounting Requirements ........................2-13 INSTALLATION PROCEDURE......................3-1 3.1 Unpacking Unit..........................3-1 3.2 Wiring Harness Installation .......................3-1...
  • Page 6 PARAGRAPH PAGE APPENDIX A GIA 63 MAIN BOOT BLOCK UPLOADING INSTRUCTIONS......... A-1 A.1 Introduction............................A-1 A.2 Determining Current Boot Block...................... A-1 A.3 Loading Boot Block Version 4.01 ....................A-2 A.4 Loading GIA Main Software (only if GIA main software was cancelled in Section A.2) ....A-3 APPENDIX B OUTINE &...
  • Page 7 GIA 63 HARDWARE MOD LEVEL HISTORY The following table identifies hardware modification (Mod) Levels for the GIA 63. Mod Levels are listed with the associated service bulletin number, service bulletin date, and the purpose of the modification. The table is current at the time of publication of this manual (see date on front cover) and is subject to change without notice.
  • Page 8 The table is current at the time of publication of this manual (see date on front cover) and is subject to change without notice. Authorized Garmin Sales and Service Centers are encouraged to access the most up-to-date bulletin and advisory information on the Garmin Dealer Resource web site at www.garmin.com using their Garmin-provided user name and password.

  • Page 9: General Description

    This manual presents mechanical and electrical installation requirements for installing the GIA 63(X) as part of a Garmin Integrated Flight Deck. The GIA 63(X) can be integrated into a variety of airframes under an appropriate TC or STC. Each airframe installation may vary. Use only approved (type or supplemental type) data for specific installation instructions in a particular aircraft.

  • Page 10: Interface Summary

    1.3 Interface Summary 1.3.1 Primary Interfaces The GIA 63(X) is designed as an open architecture system that provides the following interfaces: • 1 dedicated Ethernet High-Speed Data Bus (HSDB) input/output channel • 2 Controller Area Network (CAN) I/O channels •...

  • Page 11: Technical Specifications

    1.4 Technical Specifications 1.4.1 Environmental Qualification Form It is the responsibility of the installing agency to obtain the latest revision of the GIA 63(X) Environmental Qualification Form. These forms are available directly from Garmin under the following part numbers: GIA 63 Environmental Qualification Form, Garmin part number 005-00148-02 GIA 63W Environmental Qualification Form, Garmin part number 005-00235-00 The GIA 63H and the GIA 63W are included in the 005-00235-00.
  • Page 12 1.4.4 GPS Specifications (GIA 63 only) Characteristics Specifications Acquisition Time a) Search-the-Sky (without almanac, without initial position or time): 5 minutes b) AutoLocate ™ (with almanac, without initial position or time): 5 minutes c) Cold Start (position known to 300 nm, time known to 10...
  • Page 13 70 mVrms to 3.0 Vrms analog microphone input signal applied to the transmitter. When a digital audio microphone signal is provided by a compatible Garmin audio panel, the modulation capability specification can be met with a minimum 70 mVrms microphone input signal applied to the audio panel.
  • Page 14 20 dB. Audio Distortion The distortion in the receiver audio output shall not exceed 10% at all levels up to 100 mW. Selectivity 6 dB BW is greater than 16.5 kHz. Page 1-6 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 15 1020 Hz shall be attenuated at least 20 dB. Audio Distortion The distortion in the receiver audio output shall not exceed 10% at all levels up to 100 mW. GIA 63 Installation Manual Page 1-7 190-00303-05 Revision T...
  • Page 16 (see Sections 4.7.2.1 and 4.10.7) (Main 2 Connector) Power Requirements for P605 1.0 A max @ 27.5 Vdc (Without Superflags Active) (Main 2 Connector) 2.0 A max @ 13.75 Vdc (Without Superflags Active) Page 1-8 GIA 63 Installation Manual Revision T 190-00303-05...

  • Page 17: License Requirements

    Radio Station License. The FCC also has a fax-on-demand service to provide forms by fax. The GIA 63(X) owner accepts all responsibility for obtaining the proper licensing before using the transmitter. International transmitter license procedures vary by country. Contact the local spectrum agency for license requirements.

  • Page 18: Certification

    The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements. At the time of publication, installations of this TSO approved article are only approved when installed in an aircraft as part of a Garmin Integrated Flight Deck.
  • Page 19 1.6.1 GIA 63 TSO/ETSO Compliance Applicable LRU SW Part Applicable CLD Function TSO/ETSO Category Numbers Part Numbers 006-C0046-() 006-B0190-() 006-C0044-() TSO-C9c except Automatic Pilots ETSO-C9c 006-B0190-00 006-C0047-() through 006-C0039-01 006-B0190-19 006-C0046-() 006-B0190-() 006-C0044-() Glideslope TSO-C34e except 006-B0083-01 Receiver ETSO-2C34f 006-B0190-00...
  • Page 20 3. Garmin was granted a deviation from TSO-C9c subpart A (c), which requires marking the weight of the unit on the unit. Garmin will provide this information in the installation manual in lieu of marking on the serial tag. Garmin does not currently list the weight on other avionics units.
  • Page 21 For abnormal operating conditions power input tests, satellite acquisition time of 5 minutes applies. TSO-C151b 1. Garmin was granted a deviation from TSO-C151b 4.a. to mark the unit with the serial number instead of the date of manufacture. GIA 63 Installation Manual...
  • Page 22 006-C0072-0() 006-B0544-1() through 006-C0085-0() 006-B0544-3() 006-B0082-0() and all except TSO-C36e 006-C0039-0() Localizer Receiver Class A ETSO-2C36f 006-B0544-B() 006-B0082-00 except except through 006-C0039-00 006-B0544-BA 006-B0082-02 through through 006-C0039-02 006-B0544-BB 006-C0053-0() except 006-C0053-00 Page 1-14 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 23 Augmented by the except through Wide Area 006-B0544-BA 006-B0339-03 006-C0085-0() Augmentation through System* 006-B0544-BB GIA63W ARINC output labels 310 and 311 are not to be used as navigation data per RTCA/DO-229c. GIA 63 Installation Manual Page 1-15 190-00303-05 Revision T...
  • Page 24 Equivalent to Communications – (transmitter) and all except 006-C0085-0() ETSO-2C37e Transceiver Class C and 006-B0544-B() 006-B0081-00 & Equipment except through 006-C0039-0() ETSO-2C38e (receiver) 006-B0544-BA 006-B0081-04 except through 006-C0039-00 006-B0544-BB through 006-C0039-02 Page 1-16 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 25 3. Garmin was granted a deviation from TSO-C9c subpart A (c), which requires marking the weight of the unit on the unit. Garmin will provide this information in the installation manual in lieu of marking on the serial tag. Garmin does not currently list the weight on other avionics units.
  • Page 26 TSO-C151b 1. Garmin was granted a deviation from TSO-C151b to use DO-160E instead of DO-160D. 2. Garmin was granted a deviation from TSO-C151b 4.a. to mark the unit with the serial number instead of the date of manufacture. ETSO-C151a 1. Garmin was granted a deviation from ETSO-C151a to use DO-160E instead of DO- 160D.
  • Page 27 2. Garmin was granted a deviation to TSO-C169, paragraph 4.d requirement to mark the installation procedures drawing number on the equipment. Garmin will mark as follows, which Garmin believes meets the intent of the requirement. The Install Manual is part of the furnished data package.
  • Page 28 006-B0544-B() 006-B0082-10 except 006-C0124-0() 006-B0544-BA through 006-B0544-BD 006-B0544-3() 006-C0084-0() except except 006-B0544-30 006-C0084-00 through 006-C0072-0() Flight Director 006-B0544-34 TSO-C52b Equipment and all 006-B0544-B() except 006-C0085-0() 006-B0544-BA through 006-B0544-BD Page 1-20 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 29 Class C and and all Equipment 006-B0544-B() (receiver) except 006-C0085-0() 006-B0544-BA through 006-B0544-BD GIA 63W ARINC output labels 310 and 311 are not to be used as navigation data per RTCA/DO-229c. GIA 63 Installation Manual Page 1-21 190-00303-05 Revision T...
  • Page 30 3. Garmin was granted a deviation from TSO-C9c subpart A (c), which requires marking the weight of the unit on the unit. Garmin will provide this information in the installation manual in lieu of marking on the serial tag. Garmin does not currently list the weight on other avionics units.
  • Page 31 GIA 63W or GIA 63H equipment. 4. When flight planning an LNAV/VNAV or LPV approach, operators should use the Garmin Prediction Program 006-A0154-01 with the <insert installed antenna part number> antenna selection in addition to any NOTAMs issued for the approach.
  • Page 32 GARMIN GNSS (GPS/SBAS) NAVIGATION SYSTEM EQUIPMENT APPROVALS The Garmin GNSS navigation system installed in this aircraft is a GPS system with a Satellite Based Augmentation System (SBAS) comprised of [two TSO-C145a Class 3 approved Garmin GIA 63W or GIA 63H units, TSO-C146a Class 3 approved Garmin GDU 1XXX Display Units, Garmin GA 36 and GA 37 antennas, and GPS software version 3.2 or later approved version].
  • Page 33 The GNSS navigation system has [two ETSO-145 / TSO-C145a Class 3 approved Garmin GIA 63W and GIA 63H units, and ETSO-146 / TSO-C146a Class 3 approved Garmin GDU 1XXX Display Units]. The Garmin GNSS navigation system as installed in this aircraft complies with the equipment requirements for PRNAV and BRNAV operations in accordance with AC 90-96A and JAA TGL-10 Rev 1.
  • Page 34 The navigation equipment required to join and fly an instrument approach procedure is indicated by the title of the procedure and notes on the IAP chart. Use of the Garmin GPS/SBAS receivers to provide navigation guidance during the final approach segment of an ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for “or GPS”...
  • Page 35 Navigation information is referenced to WGS-84 reference system, and should only be used where the Aeronautical Information Publication (including electronic data and aeronautical charts) conform to WGS-84 or equivalent. 1.6.8 Other Regulatory Criteria (GIA 63) RTCA/DO-178B Level B, C, D (Software)

  • Page 36: Referenced Documents

    1.7 Referenced Documents The following publications are sources of additional information for installing the GIA 63(X). Before installing the GIA 63(X), the technician should read all referenced materials along with this manual. Part Number Document 190-00303-00 G1000 System Installation Manual...

  • Page 37: Limited Warranty

    (iv) damage caused by service performed by anyone who is not an authorized service provider of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin.
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  • Page 39: Installation Overview

    This section provides hardware equipment information for installing the GIA 63(X), related hardware, and antennas. Installation of the GIA 63(X) should follow the aircraft TC or STC requirements. Cabling is fabricated by the installing agency to fit each particular aircraft. The guidance of FAA advisory circulars AC 43.13-1B and AC 43.13-2B, where applicable, may be found useful for making retro-fit...
  • Page 40 2.1.2 Required Accessories Each of the following accessories is provided separately from the GIA 63(X). Either rack (modular, standalone, or helicopter) and remainder of the accessories are required for installation. Item Garmin P/N GIA 63(W) Modular Install Rack 115-00426-00 GIA 63(W) Standalone Install Rack...
  • Page 41 (which is about 16dB at 1.5 GHz for antennas produced by Garmin) is offset by added attenuation in-line with the GIA 63 (non-WAAS). If an in-line attenuator is used, it must pass DC current (40 mA max at 4.6 VDC) which is provided from the GPS receiver to the antenna pre-amplifier.
  • Page 42 [5] The WAAS GPS antenna connector (and XM antenna connector where applicable) is TNC type. The VHF COM antenna connector is BNC type. [6] Not approved for use with the GIA 63 (non-WAAS) since max DC current specification exceeds 40 mA.

  • Page 43: Installation Considerations

    2.2 Installation Considerations The GIA 63(X) interfaces with the G1000 system and with various avionics equipment. Fabrication of a wiring harness is required. Sound mechanical and electrical methods and practices are required for installation of the GIA 63(X). 2.2.1 Antenna Considerations...
  • Page 44 (re-radiating) ELT transmitter. Note: The separation requirement does not apply to GPS and COM combination antennas, provided the antenna model is TSO authorized and has been tested to meet Garmin’s minimum performance standards. The separating requirement includes the combination with an XM antenna element as well.
  • Page 45 Figure 2-1 shows the recommended placement of antennas. Figure 2-1. GPS Antenna Considerations GIA 63 Installation Manual Page 2-7 190-00303-05 Revision T...
  • Page 46 (18 inches square, minimum). The antenna should be mounted a minimum of six feet from any DME or other COM antennas, four feet from any ADF sense antennas, and three feet from the GIA 63(X) and its GPS antenna.

  • Page 47: Rack Considerations

    COM transceiver and COM antenna (including the GIA 63(X) COM antenna), ELT antenna, and DF receiver antenna is critical. Use the following guidelines, in addition to others in this document, when locating the GIA 63(X) and its antennas.

  • Page 48: Cabling And Wiring

    1 CFM (cubic foot per minute) at a pressure equivalent to 0.1 inches of water. Potential damage to your GIA 63(X) may occur by using outside forced air to cool the equipment. Therefore, it is recommended that an electric forced air fan be installed, of the indicated rating, to cool this equipment.

  • Page 49: Gia 63 Minimum Installation Requirements

    Air Data Computer. Manual Course Device This device delivers the manual course select to the GIA 63, which is required for the VOR receiver, and optional for the GPS receiver. Course information can come from an analog resolver, or from the GDU PFD/MFD via Ethernet HSDB.

  • Page 50: Gia 63W And Gia 63H Minimum Installation Requirements

    In addition it provides manual course selection to the GIA, which is required for the VOR receiver and optional for the GPS receiver. Qualified GPS Antenna Refer to Section 2.1.3.2 for a list of approved antennas. Page 2-12 GIA 63 Installation Manual Revision T 190-00303-05...

  • Page 51: Mounting Requirements

    The unit may also be mounted outside of the G1000 system rack. The number and positions of screws noted in Figure B-2 are to be used when mounting the GIA 63(W) modular rack outside of the G1000 system rack. Aircraft manufacturer must fabricate any additional mounting equipment needed, use outline and installation drawings in Appendix B for reference.

  • Page 52: Gia 63(W) Standalone Rack

    #8-32 pan head screws (MS35206, AN526, or other approved fastener). It can also be mounted horizontally using four #6-32 100° counter-sunk flathead screws (MS24693, AN507R, or other approved fastener). Ensure that the GIA 63(W) chassis has a ground path to the airframe by having at least one mounting screw in contact with the airframe.

  • Page 53: Gia 63H Standalone Rack

    Figure 2-4 GIA 63H Standalone Rack GIA 63 Installation Manual Page 2-15 190-00303-05 Revision T...

  • Page 54: Gia 63(W) Standalone Rack, Suggested Mounting Locations

    Figure 2-5 GIA 63(W) Standalone Rack, Suggested Mounting Locations Page 2-16 GIA 63 Installation Manual Revision T 190-00303-05...

  • Page 55: Installation Procedure

    If the unit is damaged, notify the carrier and file a claim. To justify a claim, save the original shipping container and all packing materials. Do not return the unit to Garmin until the carrier has authorized the claim.

  • Page 56: Antenna Installation

    NOTES 1. Non-Garmin part numbers shown are not maintained by Garmin and consequently are subject to change without notice. 2. Extraction of 16 and 18 AWG contacts requires cutting off the wire barrel from the contact. It may also be necessary to push the pin out from the face of the connector when using an extractor.

  • Page 57: Backshell Assembly

    If there is excessive resistance, do not force the unit. 7. Lock the handle into the GIA 63(W) body and tighten the Phillips screw (or push in the D-Ring and twist clockwise 90°, for units with a D-Ring).

  • Page 58: Post Installation Configuration & Checkout

    3.7 Post Installation Configuration & Checkout All configuration and checkout procedures take place upon completion of the installation of the Garmin Integrated Flight Deck. The GDU serves as the graphics user interface to the installer configuring the system.

  • Page 59: Continued Airworthiness

    3.8 Continued Airworthiness Maintenance of the GIA 63(X) is “on condition” for all units installed in airframes that require power interrupt Category B (50mS). For airframes that require the GIA 63(X) to comply with RTCA/DO-160D power interrupt Category A (200mS), one of the following two actions must be taken to ensure backup time is adequate: •...

  • Page 60: Gia Status Page

    Category A Long Term Power Interrupt Annual Inspection NOTE In order to comply with this procedure GIA 63 main software version must be 5.30 or later, GIA 63W main software version must be 5.21 or later, and GDU main software version must be 7.10 or later.

  • Page 61: System Interconnects

    AIRCRAFT POWER 1 SPARE AIRCRAFT POWER 2 SPARE AIRCRAFT POWER 2 SPARE AIRCRAFT POWER 2 RESERVED RESERVED POWER GROUND POWER GROUND RESERVED RESERVED RESERVED * Indicates Active Low † Pin not currently supported GIA 63 Installation Manual Page 4-1 190-00303-05 Revision T...
  • Page 62 Connector P601, continued Pin Name RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED POWER GROUND POWER GROUND * Indicates Active Low † Pin not currently supported Page 4-2 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 63 ILS ENERGIZE* RESERVED RESERVED GLIDESLOPE +FLAG PARALLEL DME 1 MHZ-D GLIDESLOPE +UP VOR/ILS ARINC 429 IN B VOR/ILS ARINC 429 IN A * Indicates Active Low † Pin not currently supported GIA 63 Installation Manual Page 4-3 190-00303-05 Revision T...
  • Page 64 PARALLEL DME 1MHZ-E RESERVED SPARE GLIDESLOPE COMPOSITE OUT (011-01105-20 AND 011-01105-30 ONLY) VOR/LOC DIGITAL AUDIO OUT SIGNAL GROUND POWER GROUND POWER GROUND * Indicates Active Low † Pin not currently supported Page 4-4 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 65 CAN BUS 2 HI MAIN ARINC 429 IN 2 A CAN BUS 1 TERMINATION MAIN ARINC 429 IN 2 B RS-485 5 A/RS-422 OUT A * Indicates Active Low † Pin not currently supported GIA 63 Installation Manual Page 4-5 190-00303-05 Revision T...
  • Page 66 MAIN ARINC 429 OUT 2 A MAIN ARINC 429 OUT 3 B MAIN ARINC 429 OUT 3 A ETHERNET IN A ETHERNET IN B RESERVED * Indicates Active Low † Pin not currently supported Page 4-6 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 67 ANNUNCIATE* 6 ANNUNCIATE* 7 ANNUNCIATE* 8 ANNUNCIATE* 9 ANNUNCIATE* 10 ANNUNCIATE* 11 ANNUNCIATE* 12 ANNUNCIATE* 13 ANNUNCIATE* 14 ANNUNCIATE* 15 ANNUNCIATE* 16 * Indicates Active Low † Pin not currently supported GIA 63 Installation Manual Page 4-7 190-00303-05 Revision T...
  • Page 68 Connector P604, continued Pin Name ANNUNCIATE* 17 ANNUNCIATE* 18 ANNUNCIATE* 19 ANNUNCIATE* 20 ANNUNCIATE* 21 * Indicates Active Low † Pin not currently supported Page 4-8 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 69 AIRCRAFT POWER 1 POTENTIOMETER REF OUT HI† AIRCRAFT POWER 2 POTENTIOMETER REF OUT LO (GROUND)† AIRCRAFT POWER 2 GIA REMOTE POWER OFF * Indicates Active Low † Pin not currently supported GIA 63 Installation Manual Page 4-9 190-00303-05 Revision T...
  • Page 70 DISCRETE OUT* 3A DISCRETE OUT* 4A ANNUNCIATE* 1A ANNUNCIATE* 2A DISCRETE IN* 17A DISCRETE IN 24A SUPERFLAG 2A POWER GROUND SUPERFLAG 3A POWER GROUND * Indicates Active Low † Pin not currently supported Page 4-10 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 71 SPARE SPARE SPARE RESERVED SIGNAL GROUND RESERVED ADF DC REF IN RESERVED ANALOG ROLL STEERING HI RESERVED ANALOG ROLL STEERING LO (GROUND) * Indicates Active Low † Pin not currently supported GIA 63 Installation Manual Page 4-11 190-00303-05 Revision T...
  • Page 72 DISCRETE OUT* 4B DISCRETE OUT* 5B DISCRETE OUT* 6B DISCRETE OUT* 7B DISCRETE OUT* 8B DISCRETE OUT* 9B RESERVED DISCRETE OUT* 10B RESERVED * Indicates Active Low † Pin not currently supported Page 4-12 GIA 63 Installation Manual Revision T 190-00303-05...

  • Page 73: Power And Antennas

    ACTIVE: 10 ≤  V in ≤  3 3VDC with ≥  7 5 uA source current Source current is internally limited to 1.5 mA max for a 10-33VDC input 4.2.1.3 Antennas Pin Name Connector GPS ANTENNA P611 COM ANTENNA P612 VOR/LOC ANTENNA P613 GLIDESLOPE ANTENNA P614 GIA 63 Installation Manual Page 4-13 190-00303-05 Revision T...

  • Page 74: Gia System Id Program

    4.3 GIA System ID Program The GIA 63(X) utilizes a hard strapping method to assign a unit ID to a unit. Unit ID’s identify a unit as a #1, #2, #3, or #4 GIA. GIA SYSTEM ID PROGRAM* GIA SYSTEM ID PROGRAM*...
  • Page 75 RS-485 4 B P603 The GIA 63(X) contains a total of 5 channels of RS-485 serial data communications. Any two of these channels can also be configured as one RS-422 channel to allow for system flexibility. These data busses conform to EIA standard RS-485, or RS-422, depending on which mode they are currently operating in.
  • Page 76 ETHERNET IN B P603 This Ethernet based high speed data bus (HSDB) provides communications capability with the GDU. HSDB meets the hardware aspects of IEEE standard 802.3 for 10 base T Ethernet communications. Page 4-16 GIA 63 Installation Manual Revision T 190-00303-05...

  • Page 77: Discrete I/O

    Leakage current in the INACTIVE state is typically ≤ 250 uA to ground ACTIVE: Vout ≤ 0.5VDC with ≤  5 00 mA sink current Sink current must be externally limited to 500 mA max GIA 63 Installation Manual Page 4-17 190-00303-05...

  • Page 78: Com/Vor/Ils/Digital Audio

    121.50 MHz. Once the emergency frequency is activated through COM REMOTE TRANSFER*, the GIA 63(X) ignores inputs from the front panel controls for COM selections only. The pilot may exit this independent mode—restoring COM selection control to the front panel knobs and buttons—by momentarily depressing the COM REMOTE TRANSFER* switch.
  • Page 79 COM REMOTE TRANSFER* and VOR/ILS REMOTE TRANSFER* are momentary inputs. 4.6.2.6 Marker Beacon Pin Name Connector OUTER MARKER LAMP IN P605 MIDDLE MARKER LAMP IN P605 AIRWAY/INNER MARKER LAMP IN P605 Active high inputs used for outer/middle/inner marker lamp inputs. GIA 63 Installation Manual Page 4-19 190-00303-05 Revision T...

  • Page 80: Vor/Ils Indicator

    The deviation outputs are each capable of driving up to three 1000 Ω meter loads with ±150 mV ±10% with respect to 2.5V Common for full-scale deflection. The drive circuit provides for more than full-scale ±10%. deflection with a maximum course deviation output voltage of ±300 mV Page 4-20 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 81 OBS STATOR D and VOR OBS STATOR F are each phase and amplitude shifted version of the VOR ROTOR C output. Each pair is intended to read one of the two windings of the indicator’s OBS stator. GIA 63 Installation Manual Page 4-21...
  • Page 82 Leakage current in the INACTIVE state is typically ≤ 10 uA to ground ACTIVE: Vout ≤ 0.5VDC with ≤  2 0 mA sink current Sink current must be externally limited to 20 mA max Page 4-22 GIA 63 Installation Manual Revision T 190-00303-05...

  • Page 83: Rmi/Obi

    Leakage current in the INACTIVE state is typically ≤ 10 uA to ground ACTIVE: Vout ≤ 0.5VDC with ≤  2 0 mA sink current Sink current must be externally limited to 20 mA max GIA 63 Installation Manual Page 4-23 190-00303-05...

  • Page 84: Dme Tuning And Adf

    4.9.1 DME Tuning Function The GIA 63(X) can channel a DME based on the tuned VLOC frequency. The GIA 63(X) outputs 2 of 5, BCD or Slip parallel DME and King Serial DME channeling format. When DME COMMON is held low, the GIA 63(X) actively tunes the DME.
  • Page 85 MAIN KING SERIAL DME CLOCK P606 MAIN KING SERIAL DME REQUEST P606 These pins are used when the GIA 63(X) is configured for King Serial DME tuning. Input logic levels are: High 6.5 Vdc or greater 3.5 Vdc or less 4.9.2.3 Automatic Direction Finder Inputs...

  • Page 86: Auto Pilot

    PITCH +DOWN. Otherwise the input voltage is negative. The input voltage is positive if FLIGHT DIRECTOR ROLL +RIGHT is greater than FLIGHT DIRECTOR ROLL +LEFT. Otherwise the input voltage is negative. Page 4-26 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 87 Amplitude: -15 to +15 Vdc Load Impedance: > 5 kΩ Scaling: 0.21 Vdc per degree of course error Range: 0 ± 71 degrees Resolution: ± 0.15° or better Accuracy: ± 1° GIA 63 Installation Manual Page 4-27 190-00303-05 Revision T...
  • Page 88 (AIRCRAFT POWER –2.0 V ) when the flag is to be OUT OF VIEW. The output voltage with respect to ground is less than 0.25 V when the flag is to be IN VIEW. Page 4-28 GIA 63 Installation Manual Revision T 190-00303-05...
  • Page 89 These inputs read the remote annunciate data bus that the autopilot uses to tell its remote annunciator panel what mode it is operating in. The GIA 63 requires 4.7 kΩ pull-up resistors to +28 V in the aircraft harness for each of these inputs.
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  • Page 91: Appendix A Gia 63 Main Boot Block Uploading Instructions

    APPENDIX A GIA 63 MAIN BOOT BLOCK UPLOADING INSTRUCTIONS NOTE This appendix applies to the GIA 63 only, and does not apply to the GIA 63W or GIA 63H. Introduction This appendix contains instructions on how to upgrade main boot block software for the GIA 63. Boot block version 4.01 is required for GIA Main Software Version 4.00 or later.

  • Page 92: Loading Boot Block Version 4.01

    If power is removed from the entire G1000 system GIA 2 may appear as GIA 1. 2. Insert the GIA 63 boot block version 4.01 loader card into the top slot of the PFD. 3. While holding the ENT key on the PFD, restore power to the PFD.

  • Page 93: Loading Gia Main Software (Only If Gia Main Software Was Cancelled In Section

    14. Verify ‘G1000 GIA 6X SYS’ is being reported in the description field. 15. Power down the G1000. 16. Remove the GIA 63 boot block version 4.01 loader card form the PFD. 17. Continue to Section A.4. A.4 Loading GIA Main Software (only if GIA main software was cancelled in Section A.2)
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