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Garmin 500W Series Instructions Manual

Continued airworthiness
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Instructions for Continued Airworthiness
Rev.
Date
1
10-19-06
A
11-03-06
B
07-30-09
C
02-28-13
D
11-20-14
500W Series
Document Number 190-00357-65 Rev. D
Garmin International, Inc.
1200 E. 151st Street
Olathe, Kansas 66062 USA
Record of Revision
Initial Release
Revision for STC Issuance
Add the "-D" to STC number when reissued under ODA
Revise to support software version 5.02. Clarify inspections. Add
electrical bonding check.
Revise to support software version 5.20 with Flight Stream 210
Description of Change

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Summary of Contents for Garmin 500W Series

  • Page 1 500W Series Instructions for Continued Airworthiness Document Number 190-00357-65 Rev. D Garmin International, Inc. 1200 E. 151st Street Olathe, Kansas 66062 USA Record of Revision Rev. Date Description of Change 10-19-06 Initial Release 11-03-06 Revision for STC Issuance 07-30-09 Add the “-D” to STC number when reissued under ODA 02-28-13 Revise to support software version 5.02.

  • Page 2: Table Of Contents

    Overhaul Period ....................11     2.15 ICA Revision and Distribution ................11     2.16 Assistance......................11     2.17 Implementation and Record Keeping ..............11 500W Series 190-00357-65 Rev. D Instructions for Continued Airworthiness Page 2 of 12...

  • Page 4: Introduction

    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 Models 500W series GPS/WAAS NAV/COM. Applicability: Applies to aircraft altered by installation of the Garmin Models 500W series GPS/WAAS NAV/COM.

  • Page 5: Description Of Alteration

    2.2 Description of Alteration The Garmin Model 500W Series GPS/WAAS Nav/Com unit is a 6 ¼ inch wide panel mounted unit with all the interface connections behind the instrument panel. Installation of the Garmin Model 500W series GPS/WAAS Nav/Com system interfaces, specific for the aircraft installation, is documented in the GNS 500W Series Post-Installation Checkout Log that is retained as part of the aircraft’s permanent...
  • Page 6 The display backlight lamp is rated by the manufacturer as having a usable life of 20,000 hours. This life may be more or less than the rated time depending on the operating conditions of the 500W series unit. Over time, the backlight lamp may dim and the display may not perform as well in direct sunlight conditions.

  • Page 7: Troubleshooting Information

    If the 500W series unit is removed for repair and reinstalled, or if the 500W unit is removed and replaced with a different 500W series unit, then follow ‘Post Installation Configuration & Checkout Procedures’...
  • Page 8 4. Attach the connector, tightening the two jackscrews. 5. Close the BT Link circuit breaker. 6. Complete the interface checkout procedures contained in Section 5.5.8 of the 500W Series Installation Manual. Figure 1. Flight Stream 210 Assembly Overview (Bonding Strap Not Shown) 500W Series 190-00357-65 Rev.
  • Page 9 Re-install the bonding strap and perform the electrical bonding test in accordance with Section 2.5.4. 5. Replace any damaged hardware, otherwise hardware may be reused. 500W Series 190-00357-65 Rev. D Instructions for Continued Airworthiness...

  • Page 10: Diagrams

    The antenna cables are routed between the 500W series unit and the antenna with disconnects at each unit. The antenna cable typically is routed behind interior panels in the fuselage.

  • Page 11: Special Tools

    The system does not require overhaul at a specific time period. Power on self-test and continuous BIT will monitor the health of the 500W series unit. If the unit indicates an internal failure, the unit may be removed and replaced. See troubleshooting section contained in the 500W Series Installation Manual, listed under reference documentation in section 2.1 of this document.

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