Garmin GNS 5XXW, Manual

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Page 2: ...type David G Armstrong ODA STC Unit Administrator ODA 240087 CE Garmin International Inc C All 03 21 13 Complete Rewrite Michael Warren ODA STC Unit Administrator ODA 240087 CE Garmin International Inc D 10 14 01 27 14 Added LP V approach type Michael Warren ODA STC Unit Administrator ODA 240087 CE Garmin International Inc E 8 9 11 14 15 22 23 11 20 14 Updated document revisions and added Flight S...

Page 3: ...uipped Units 12 2 10 VNAV Vertical Navigation Calculation Page 12 2 11 Weather Display Optional 12 2 12 Traffic Display Optional 12 2 13 Manual GTN Crossfill 12 2 14 Flight Stream 210 Optional 13 Section 3 EMERGENCY PROCEDURES 14 3 1 Emergency Procedures 14 3 2 Abnormal Procedures 14 Section 4 NORMAL PROCEDURES 17 4 1 Unit Power On 17 4 2 Before Takeoff 17 4 3 HSI and EHSI Operation 18 4 4 Autopil...

Page 4: ...l concentric rotary knob along the bottom and right side of the display Optional VHF Com and VHF Nav radio functions are controlled via dedicated buttons and knobs on the left side of the display and adjacent to frequencies they are controlling Figure 1 530W Series Control and Display Layout OBS Key Terrain Annunciator Power and Com Volume Squelch Photocell for Auto Dimming Graphic Moving Map Disp...

Page 5: ...hout vertical guidance including LP and LNAV within the U S National Airspace System The Garmin GNSS navigation system complies with the equipment requirements of AC 90 105 and meets the equipment performance and functional requirements to conduct RNP terminal departure and arrival procedures and RNP approach procedures without RF radius to fix legs Part 91 subpart K 121 125 129 and 135 operators ...

Page 6: ...contains the minimum system functions required for P RNAV operations in accordance with JAA Administrative Guidance Material Section One General Part 3 Temporary Guidance Leaflets Leaflet No 10 JAA TGL 10 Rev 1 The GNSS navigation system has one or more TSO C146a Class 3 approved Garmin GNS Navigation Systems The Garmin GNSS navigation system complies with the accuracy integrity and continuity of ...

Page 7: ...GTX 330 330D TIS Garmin TAWS GPS 500WT GNS 530WT GTS 8XX Series TAS Flight Stream 210 400W 500W Series Optional Displays P N 190 00356 30 Rev L The Pilot s Guide Addendum part number and revision listed below or later applicable revision must be immediately available for the flight crew whenever one or more of the following units are installed and utilized with the 5XXW Series unit Stormscope Ligh...

Page 8: ...s the flight crew verifies and uses the current navigation database GPS based instrument approaches must be flown in accordance with an approved instrument approach procedure that is loaded from the navigation database Discrepancies that invalidate a procedure should be reported to Garmin International The affected procedure is prohibited from being flown using data from the navigation database un...

Page 9: ...med for the intended route of flight In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended route of flight the flight shall be delayed canceled or rerouted on a track where RAIM requirements can be met The flight may also be re planned using non GPS based navigational capabilities For flight planning purposes for operations within European B RNA...

Page 10: ...hibited It is not acceptable to flight plan a required alternate airport based on RNAV GPS LP LPV or LNAV VNAV approach minimums The required alternate airport must be flight planned using an LNAV approach minimums or available ground based approach aid Navigation information is referenced to the WGS 84 reference system and should only be used where the Aeronautical Information Publication includi...

Page 11: ...dure and that approach procedure must be loaded from the navigation database into the GNS system flight plan by its name Users are prohibited from flying any approach path that contains manually entered waypoints IFR approaches are prohibited whenever any physical or visual obstruction such as a throw over yoke restricts pilot view or access to the GNS and or the CDI 2 7 Autopilot Coupling IFR ins...

Page 12: ...ather products from SiriusXM via a GDL 69 69A or FIS B via a GDL 88 Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information provided by data link weather products may not accurately depict current weather conditions Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link ...

Page 13: ...ght Stream 210 provides the ability for the crew to import flight plans from a portable electronic device to the GNS The crew must verify all flight plan and waypoint information imported from a portable electronic device prior to use on the GNS See section 7 3 for additional information 2 15 Portable Electronic Devices This STC does not relieve the operator from complying with the requirements of...

Page 14: ...1 LOSS OF GPS SBAS NAVIGATION DATA When the GPS SBAS receiver is inoperative or GPS navigation information is not available or invalid the GNS will enter one of two modes Dead Reckoning mode DR or Loss Of Integrity mode LOI The mode is indicated on the GNS by an amber DR or INTEG If the Loss Of Integrity annunciation is displayed revert to an alternate means of navigation appropriate to the route ...

Page 15: ...equirements cannot be met by the GPS receiver prior to the Final Approach Fix the GNS will downgrade the approach The downgrade will remove vertical deviation indication from the VDI and change the approach annunciation accordingly from LPV L VNAV LP V or LNAV V to LNAV The approach may be continued using the LNAV only minimums After the Final Approach Fix has been passed the approach will be abor...

Page 16: ...ke corrective action until the alert ceases Stop descending or initiate either a climb or a turn or both as necessary based on analysis of all available instruments and information 3 2 5 TAWS INHIBIT The TAWS Forward Looking Terrain Avoidance FLTA and Premature Descent Alerts PDA functions may be inhibited to prevent alerting if desired Refer to GNS 400W 500W Optional Displays Addendum for additio...

Page 17: ...oming too engrossed at the expense of basic instrument flying in IMC and basic see and avoid in VMC Pilot workload will be higher for pilots with limited familiarity in using the unit in an IFR environment particularly without the autopilot engaged Garmin provides training tools with the Pilot s Guide and PC based simulator Pilots should take full advantage of these training tools to enhance syste...

Page 18: ...hat system CAUTION The pilot must verify the active course and waypoint for each flight plan leg The pilot must verify proper course selection each time the CDI source is changed from GPS to VLOC 4 4 Autopilot Operation The GNS may be coupled to an optional autopilot if installed in the aircraft when operating as prescribed in the LIMITATIONS section of this manual Autopilots coupled to the GNS sy...

Page 19: ... with the following message APR Guidance Available Use PROC before A P APR PROC Button PRESS Enable A P APR Outputs SELECT ENT Button PRESS If coupled Autopilot will revert to ROL mode at this time Autopilot ENGAGE APPROACH MODE This installation supports coupling to the autopilot in approach mode once vertical guidance is available To couple an approach Once established on the final approach cour...

Page 20: ...s is accomplished by pressing the cursor knob while on the dedicated traffic page to enter exit the traffic device menu It is important to note that while the traffic device menu is active the current state of the traffic system is not displayed The state of the traffic device is only displayed once the traffic device menu is exited Section 5 PERFORMANCE No change Section 6 WEIGHT AND BALANCE See ...

Page 21: ...oes not support The GNS typically skips over these leg types and provides no guidance Guidance may be available on the GTN but not on the GNS in these cases The GNS will sequence the procedure as it normally would if Crossfill were not active Once a leg type is reached that is supported on both the GTN and GNS systems the systems will automatically sync to the same leg If the GNS is interfaced wit...

Page 22: ...tion and GPS sensor data to a PED Personal Electronic Device from the GNS For details on the operation and features of the Flight Stream 210 please refer to the GNS 400W 500W Series Optional Displays P N 190 00356 30 Rev J For additional details about the Garmin supported devices and apps for use with the Flight Stream 210 please visit http garmin com connext supported_devices ...