Garmin Part 23 Stc Sa01692Se Instruction Manual 190 00607 00_0A_GMX 200_ICA.Doc
2015-05-27
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GMX 200 Instructions for Continued Airworthiness FAA STC Project No. ST9731SE-A Document Number 190-00607-00 Rev. A Garmin Ltd. Or its subsidiaries c/o Garmin International, Inc. 1200 E. 151st Street Olathe, Kansas 66062 USA Confidential This drawing and the specifications contained herein are the property of Garmin Ltd. or its subsidiaries and may not be reproduced or used in whole or in part as the basis for manufacture or sale of products without written permission. Record of Revision Rev. Date Description of Change 1 6/02/06 Initial Release A 6/19/06 Production Release 1. INTRODUCTION................................................................................................................... 3 1.1 PURPOSE ............................................................................................................ 3 1.2 Scope.................................................................................................................... 3 1.3 Document Control................................................................................................. 3 1.4 Airworthiness Limitations Section......................................................................... 3 1.5 Permission to Use Certain Documents................................................................. 3 1.6 Definitions ............................................................................................................. 3 2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS .................................................... 4 2.1 Introduction ........................................................................................................... 4 2.2 Description of Alteration........................................................................................ 4 2.3 Control, Operating Information ............................................................................. 4 2.4 Servicing Information ............................................................................................ 4 2.5 Periodic Maintenance Instructions........................................................................ 5 2.6 Troubleshooting Information ................................................................................. 5 2.7 Removal and Replacement Information ............................................................... 5 2.8 Diagrams............................................................................................................... 6 2.9 Special Inspection Requirements ......................................................................... 6 2.10 Application of Protective Treatments.................................................................... 6 2.11 Data Relative to Structural Fasteners................................................................... 6 2.12 Special Tools ........................................................................................................ 6 2.13 Additional Instructions for Aircraft Operating under FAR 121/135 ....................... 6 2.14 Overhaul Period.................................................................................................... 6 2.15 ICA Revision and Distribution ............................................................................... 6 2.16 Assistance............................................................................................................. 7 2.17 Implementation and Record Keeping ................................................................... 7 GMX 200 Instructions for Continued Airworthiness P/N 190-00607-00 Rev.A Page 2 of 7 1. INTRODUCTION 1.1 PURPOSE This document is designed for use by the installing agency of the Garmin GMX 200 as Instructions for Continued Airworthiness in response to Federal Aviation regulation (FAR) Part 23.1529, and Part 23 Appendix G. They include information required by the operator to adequately maintain the Garmin GMX 200. 1.2 Scope This document identifies the Instruction for Continued Airworthiness for modification of the aircraft for installation of the Garmin GMX 200. 1.3 Document Control This document shall be released, archived, and controlled in accordance with the Garmin document control system. When this document is revised, refer to Section 2.15 for information on how to gain FAA acceptance or approval and how to notify customers of changes. 1.4 Airworthiness Limitations Section There are no additional Airworthiness Limitations as defined in 14 CFR § 23, Appendix G. G23.4 that result from this modification. The Airworthiness Limitations section is FAA approved and specifies maintenance required under §§43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA approved. 1.5 Permission to Use Certain Documents Permission is granted to any corporation or person applying for approval of a Garmin GMX 200 to use and reference appropriate STC documents to accomplish the Instructions for Continued Airworthiness and show compliance with STC engineering data. This permission does not construe suitability of the documents. It is the responsibility of the applicant to determine the suitability of the documents for the ICA. 1.6 Definitions The following terminology is used within this document: 1) 2) 3) 4) 5) 6) 7) 8) AC: Advisory Circular ACO: Aircraft Certification Office AEG: Aircraft Evaluation Group CFR: Code of Federal Regulations DER: Designated Engineering Representative FAA: Federal Aviation Administration IAW: In Accordance With ICA: Instructions for Continued Airworthiness GMX 200 Instructions for Continued Airworthiness P/N 190-00607-00 Rev.A Page 3 of 7 9) 10) 11) 12) 13) 14) MFD: Multi-Function Display unit PMI: Primary Manufacturing Inspector POI: Primary Operations Inspector STC: Supplemental Type Certificate TC: Type Certification or Type Certificate TSO: Technical Standard Order 2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 2.1 Introduction Content, Scope, Purpose and Arrangement: This document identifies the Instructions for Continued Airworthiness for the modification of the aircraft by installation of the Garmin GMX 200. Applicability: Applies to aircraft altered by installation of the Garmin GMX 200. Definition of Abbreviations: See Section 1.6 Precautions: None Units of measurement: None Referenced publications: 190-00607-04 Rev. B GMX 200 Installation Manual (or later FAA approved revisions) 005-C0315-00 Rev. A GMX 200 STC Master Data List Retention: 2.2 This document, or the information contained within, will be retained in the aircraft’s permanent records. Description of Alteration Installation of the Garmin GMX 200 and other system interfaces. The GMX 200 consists of a LCD display, keypads, keyboard and rotary knob. 2.3 Control, Operating Information See the GMX 200 Installation Manual, listed under the reference documentation in paragraph 2.1 of this document, for system operation and self-test information. 2.4 Servicing Information None. In the event of system failure, return the unit to the manufacturer or an approved Garmin repair station. GMX 200 Instructions for Continued Airworthiness P/N 190-00607-00 Rev.A Page 4 of 7 2.5 Periodic Maintenance Instructions The GMX 200 is designed to detect internal failure. A thorough self-test is executed automatically upon application of power to the units, and built-in test is continuously executed. Detected errors are indicated on the equipment via failure annunciations and maintenance is on-condition. Operation of the GMX 200 is not permitted unless an inspection as described in this section has been completed within the preceding 12 calendar months. Conduct a visual inspection on the unit and its wire harness to insure continued installation integrity: 1. Inspect the unit for security of attachment. 2. Inspect all knobs and buttons for legibility. 3. Inspect condition of wiring, routing, and attachment/clamping. 2.5.1 Cleaning the Front Panel The front bezel, keypad, and display can be cleaned with a soft cotton cloth dampened with clean water. DO NOT use any chemical-cleaning agents. Care should be taken to avoid scratching the surface of the display. 2.5.2 Display Backlight The display backlight is rated by the manufacturer as having a usable life of 50,000 hours. This life may be more or less than the rated time depending on the operation conditions of the GMX 200 unit. Over time, the backlight may dim and the display may not perform as well in direct sunlight conditions. The user must determine by observation when the display brightness is not suitable for its intended use. Contact the Garmin factory repair station when the backlight requires service. 2.5.3 Altitude Encoder In this VFR non-essential system, it is recommended that any interfaced pressure altitude source be calibrated every 24 months. Refer to the manufacturer’s installation and calibration manual. 2.6 Troubleshooting Information If error indications are displayed on the GMX 200 unit, consult the Troubleshooting section contained in the GMX 200 Installation Manual, listed under reference documentation in paragraph 2.1 of this document. The ‘GMX 200 Post-Installation Checkout Log’ in the aircraft permanent records includes the configuration information for the installation. (See Table 5-3 in the GMX 200 Installation Manual for a sample Log). 2.7 Removal and Replacement Information If the GMX 200 unit is removed and reinstalled, verify that the unit power-up self-test sequence is successfully completed and no failure messages are annunciated. If the GMX 200 unit is removed for repair and reinstalled, or if the unit is removed and replaced with a different unit, then follow ‘Post Installation Configuration & Checkout Procedures’ procedures contained in the GMX 200 Installation Manual listed in paragraph 2.1 of this document, and verify the unit power-up self-test sequence is successfully completed and no failure messages are annunciated. GMX 200 Instructions for Continued Airworthiness P/N 190-00607-00 Rev.A Page 5 of 7 2.8 Diagrams Refer to the GMX 200 Installation Manual (listed under reference documentation in section 2.1 of this document) for drawings applicable to this installation. Wiring diagrams are in Appendix E of the GMX 200 Installation Manual. 2.9 Special Inspection Requirements None, N/A. 2.10 Application of Protective Treatments None, N/A. 2.11 Data Relative to Structural Fasteners None, N/A. 2.12 Special Tools No special tools are required for system checkout. See GMX 200 Installation Manual listed in reference documentation in section 2.1 of this document. 2.13 Additional Instructions for Aircraft Operating under FAR 121/135 1. Aircraft Electrical Loads: Perform aircraft electrical system load analysis. See GMX 200 Installation Manual listed in reference documentation in section 2.1 of this document. 2. Methods of balancing flight controls: N/A. 3. Special Repair Methods applicable to the airplane: See certificate holder’s General Maintenance Manual for instructions. 2.14 Overhaul Period The system does not require overhaul at a specific time period. Power on self-test and continuous BIT will monitor the health of the GMX 200 unit. If the unit indicates an internal failure, the unit may be removed and replaced. See troubleshooting section contained in the GMX 200 Installation Manual, listed under reference documentation in paragraph 2.1 of this document. 2.15 ICA Revision and Distribution To revise this ICA, a letter must be submitted to the ACO along with the revised ICA. The ACO will obtain AEG acceptance, and approve any revision to the Airworthiness Limitations Section 1.4. After FAA acceptance/approval, Garmin will release the revised ICA for customer use, and provide any required notification of the revision. The latest revision of this document will be available on the Garmin website (garmin.com). A Garmin Service Letter, describing ICA revision, will be sent to dealers and GMX 200 owners of record if revision is determined to be significant. GMX 200 Instructions for Continued Airworthiness P/N 190-00607-00 Rev.A Page 6 of 7 2.16 Assistance Flight Standards Inspectors or the certificate holder’s PMI have the required resources to respond to questions regarding this ICA. In addition, the customer may refer questions regarding this equipment and its installation to the manufacturer, Garmin AT. Garmin AT customer assistance may be contacted during normal business hours via telephone 800-525-6726 or email from the Garmin web site at support.salem@garmin.com. 2.17 Implementation and Record Keeping Modification of an aircraft by this Supplemental Type Certificate obligates the aircraft operator to include the maintenance information provided by this document in the operator’s aircraft maintenance manual and/or the operator’s aircraft scheduled maintenance program. GMX 200 Instructions for Continued Airworthiness P/N 190-00607-00 Rev.A Page 7 of 7
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