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Garmin 500W Series Supplemental Flight Manual

Garmin gps navigation system user manual
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  • Page 3: Table Of Contents

    Garmin International 1200 E. 151 Street, Olathe, KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for a Garmin 500W Series Navigation System Table of Contents SECTION Section 1. GENERAL Garmin 500W Series GPS/WAAS Nav Com...

  • Page 4: Section 1. General

    GPS/WAAS receiver for GPS approved primary navigation under TSO C146a, (plus optional VHF Com and VHF Nav radios) in an integrated unit with a moving map and color display. The 500W Series unit features a graphical display which may also be used to depict traffic, weather, or terrain data.

  • Page 5: Operation

    500W Series unit annunciates OCN. This provides an alarm limit of four NMI and a mask angle of five degrees. The 500W series unit also has the ability to predict RAIM availability at any waypoint in the database or if WAAS corrections are expected to be absent or disabled.

  • Page 6: Section 2. Limitations

    The GARMIN 500W Series Pilot’s Guide, part number and revision listed below (or later applicable revisions), must be immediately available for the flight crew whenever navigation is predicated on the use of the 500W Series unit. 500W Series Pilot’s Guide & Reference P/N 190-00357-00 Rev E...

  • Page 7: Navigation Database

    GPS instrument approaches using the 500W Series units are prohibited, unless the 500W Series unit’s approach data is verified by the pilot or crew to be current. Instrument approaches must be accomplished in accordance with an approved instrument approach procedure that is loaded from the 500W Series unit database.

  • Page 8: Navigation

    Except in emergency conditions, IFR approaches are prohibited whenever any physical or visual obstruction (such as a throw-over yoke) restricts pilot view or access to the 500W Series unit or the affected CDI. 190-00357-03 Rev. B Page 8 of 17...

  • Page 9: Autopilot Coupling

    Garmin 500W Series Navigation System Autopilot Coupling IFR installations of a Garmin 500W Series unit allow the operator to fly all phases of flight based on the navigation information presented to the pilot; however, not all modes may be coupled to the autopilot. All autopilots may be coupled in Oceanic (OCN), Enroute (ENR), and Terminal (TERM) modes;...

  • Page 10: 2.10 Vnav

    2.11 Weather Display If an optional weather receiver is interfaced to the 500W Series unit, the weather information displayed is limited to supplemental use only and may not be used in lieu of an official weather data source.

  • Page 11: Section 3. Emergency Procedures

    Emergency Procedures No change. Abnormal Procedures a) If the Garmin 500W Series unit GPS navigation information is not available, or is invalid, utilize other remaining operational navigation equipment installed in the airplane as appropriate. If the 500W Series unit loses GPS position and reverts to Dead Reckoning mode (indicated by the annunciation of “DR”...
  • Page 12 During any GPS approach in which precision and non-precision alarm limits are exceeded, the 500W Series unit will flag the lateral guidance and generate a system message “ABORT APPROACH loss of navigation”. Immediately upon viewing the message the unit will revert to Terminal alarm limits.

  • Page 13: Section 4. Normal Procedures

    Garmin 500W Series Navigation System Section 4. NORMAL PROCEDURES Refer to the 500W Series unit Pilot’s Guide defined in paragraph 2.1 on page 6 of this document for normal operating procedures. This includes all GPS operations, VHF COM and NAV, and Multi-Function Display information.

  • Page 14: Lp Approaches

    Pilot’s Guide. Autopilot Operation The Garmin 500W Series may be coupled to an optional autopilot if installed in the aircraft when operating as prescribed in the LIMITATIONS section of this manual. For lateral guidance, some installations may utilize GPSS or GPS Roll Steering in lieu of the analog deviation information.

  • Page 15: Taws Cautions And Warning [If Installed]

    AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for a Garmin 500W Series Navigation System the unit will be configured to PROMPT the pilot to “Enable the autopilot approach outputs” in order to prevent the autopilot from entering ROLL mode without the pilot being aware of the transition.

  • Page 16: Wfde Prediction Program

    Program is required for Remote/Oceanic operations. The Prediction Program should be used in conjunction with the Garmin 400W/500W Simulator. After entering the intended route of flight in the Simulator flight plan the pilot selects the FDE Prediction Program under the Options menu of the Simulator program.

  • Page 17: Section 5. Performance

    No change. Section 6. WEIGHT AND BALANCE See current weight and balance data. Section 7. SYSTEM DESCRIPTIONS See Garmin 500W Series unit Pilot’s Guide for a complete description of the 500W Series unit. 190-00357-03 Rev. B Page 17 of 17...

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