Garmin 400W Series Supplemental Flight Manual
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Garmin 400W Series Supplemental Flight Manual

Garmin 400W Series Supplemental Flight Manual

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

    Emergency Procedures Abnormal Procedures Section 4. NORMAL PROCEDURES Approaches with Vertical Guidance Approaches without Vertical Guidance For additional information on LP approaches refer to the 400W Series unit Pilot’s Guide. Autopilot Operation Coupling the Autopilot during approaches WFDE Prediction Program Section 5.

  • 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 400W Series unit features a graphical display which may also be used to depict traffic, weather, or terrain data.

  • Page 5: Operation

    400W Series unit annunciates OCN. This provides an alarm limit of four NMI and a mask angle of five degrees. The 400W 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 400W 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 400W Series unit. 400W Series Pilot’s Guide & Reference P/N 190-00356-00 Rev E...

  • Page 7: Navigation Database

    GPS instrument approaches using the 400W Series units are prohibited, unless the 400W 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 400W 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 400W Series unit or the affected CDI. 190-00356-03 Rev. B Page 8 of 16...

  • Page 9: Autopilot Coupling

    Garmin 400W Series Navigation System Autopilot Coupling IFR installations of a Garmin 400W 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: 2.11 Traffic Display

    SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for a Garmin 400W Series Navigation System If an optional weather receiver is interfaced to the 400W 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 400W 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 400W 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 400W 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 400W Series Navigation System Section 4. NORMAL PROCEDURES Refer to the 400W 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: Approaches Without Vertical Guidance

    Pilot’s Guide. Autopilot Operation The Garmin 400W 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 AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for a Garmin 400W 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

    No change. Section 6. WEIGHT AND BALANCE See current weight and balance data. Section 7. SYSTEM DESCRIPTIONS See Garmin 400W Series unit Pilot’s Guide for a complete description of the 400W Series unit. 190-00356-03 Rev. B Page 16 of 16...

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