Garmin SA01933LA_D Airplane Flight Manual Supplement
Contents
1. 14 3 1 Emergency Procedures 14 3 2 Abnormal Procedures 14 Section 4 NORMAL PROCEDURES 16 4 1 Unit Power On 16 4 2 Before Takeoff 16 4 3 HSI and EHSI Operation 17 4 4 Autopilot Operation 17 4 5 Coupling the Autopilot during approaches 18 4 6 Traffic Mode Selection Optional 19 Section 5 PERFORMANCE 19 Section 6 WEIGHT AND BALANCE 19 Section 7 SYSTEM DESCRIPTIONS 20 7 1 Pilot s Guide 20 7 2 Manual GTN Crossfill 20 7 3 Flight Stream 210 20 AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 3 of 21 Section 1 GENERAL 1 1 Garmin 4XXW Series GPS WAAS Nav Com The Garmin GNS Series GPS WAAS Navigator is a panel mounted product that contains a 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 4X XW Series unit features a graphical display which may also be used to depict traffic weather or terrain data The navigation functions are operated by dedicated keys and graphical menus which are controlled by the buttons and the dual 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 Photocell for Auto sinned Com Freq Graphic Moving Gomm Freq Window Map Display and Direct To2. to provide Temporary Flight Restriction TFR or Notice to Airmen NOTAM information Not all TFRs and NOTAMS can be depicted on the GNS 2 11 Traffic Display Optional Traffic may be displayed on the GNS when connected to an approved optional TCAS I TAS TIS or ADS B traffic device These systems are capable of providing traffic monitoring and alerting to the flight crew Traffic shown on the display may or may not have traffic alerting available The display of traffic is an aid to visual acquisition and may not be utilized for aircraft maneuvering 2 12 Manual GTN Crossfill When Manual GTN Crossfill is in use the crew must verify each flight plan leg prior to using the GNS to navigate See section 7 2 for additional information 2 13 Flight Stream 210 Optional The Flight 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 14 Portable Electronic Devices 190 00356 03 Rev E AFMS Garmin GNS 4XXW GPS SBAS System Page 12 of 21 FAA APPROVED This STC does not relieve the operator from complying with the requirements of 91 23 or any other operational regulation regarding portable electronic devices AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 13 of 21 Section
3. 3 EMERGENCY PROCEDURES 3 1 Emergency Procedures No change 3 2 Abnormal Procedures 3 2 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 and phase of flight If the Dead Reckoning annunciation is displayed the map will continue to be displayed with an amber ownship icon Course guidance will be removed on the CDI Aircraft position will be based upon the last valid GPS position then estimated by Dead Reckoning methods Changes in true airspeed altitude heading or winds aloft can affect the estimated position substantially Dead Reckoning is only available in Enroute and Oceanic modes Terminal and Approach modes do not support Dead Reckoning If Alternate Navigation Sources ILS LOC VOR DME ADF Are Available Navigation enigen i USE ALTERNATE SOURCES If No Alternate Navigation Sources Are Available DEAD RECKONING DR MODE Navigatie hdd eee E a E E i E S USE GNS NOTE All information normally derived from GPS will become less accurate over time 190 00356 03 Rev E AFMS Garmin GNS 4XXW GPS SBAS System Page 14 of 21 FAA APPROVED LOSS OF INTEGRI
4. Garmin International Inc 1200 E 151 Street Olathe Kansas 66062 U S A FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for the Garmin GNS 400W 420W 420A W 430W or 430A W GPS SBAS Navigation System as installed in Make and Model Airplane Registration Number Serial Number This document serves as an Airplane Flight Manual Supplement or as a Supplemental Airplane Flight Manual when the aircraft is equipped with the Garmin GNS 400W 420W 420AW 430W or 430AW GPS SBAS Navigation System This document must be carried in the airplane at all times when the Garmin GNS unit is installed in accordance with STC SA01933LA D This document must be incorporated into the FAA Approved Airplane Flight Manual or provided as an FAA Approved Supplemental Airplane Flight Manual The information contained herein supplements the information in the FAA Approved Airplane Flight Manual For limitations procedures loading and performance information not contained in this document refer to the FAA Approved Airplane Flight Manual markings or placards FAA Approved By P Michael Warren ODA STC Unit Administrator Garmin International Inc ODA 240087 CE Date RO NYY 201 AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page of 22 LOG OF REVISIONS Page Rev No No Date Description FAA Approved A All 11 20 07 Comple
5. Key Flip Flop Nav Freq aon at Window Navigation Info Range Keys Menu Key Power and Com Volume Squelch Clear Key Data Enter Key AN Fir Function and Nav Radio r 3 valine J Si i lt Page Number Nav Radio Large Knob Flip Flop Large Knob Small Knob Com VLOC Cursor Press Freq MHz Terrain Flight to activate Small Knob Phase and Com VLOC GPS Integrity i Freq kHz Annunciator Mounting Screw Procedure Key Key Message K Navigation oy Source GPS VLOC or GPS PTK Figure 1 430W Series Control and Display Layout 190 00356 03 Rev E AFMS Garmin GNS 4XXW GPS SBAS System Page 4 of 21 FAA APPROVED 1 2 GPS SBAS TSO C146a Class 3 Operation The GNS complies with AC 20 138A and has airworthiness approval for navigation using GPS and SBAS within the coverage of a Satellite Based Augmentation System complying with ICAO Annex 10 for IFR en route terminal area and non precision approach operations including those approaches titled GPS or GPS and RNAV GPS approaches The Garmin GNSS navigation system is composed of the GNS navigator and antenna and is approved for approach procedures with vertical guidance including LPV and LNAV VNAV and without 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 performa
6. TY LOI MODE Navigation eee FLY TOWARDS KNOWN VISUAL CONDITIONS NOTE All information derived from GPS will be removed NOTE The airplane symbol is removed from all maps The map will remain centered at the last known position No GPS Position will be annunciated in the center of the map 3 2 2 GPS APPROACH DOWNGRADE During a GPS LPV LNAV VNAV LP V or LNAV V approach if GPS accuracy requirements 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 aborted using the indications described below During a GPS approach in which GPS accuracy requirements cannot be met by the GPS receiver for any GPS approach type the GNS will flag all CDI guidance and display a system message ABORT APPROACH Loss of Navigation Immediately upon viewing the message the unit will revert to Terminal navigation mode alarm limits If the position integrity is within these limits lateral guidance will be restored and the GPS may be used to execute the missed approach otherwise alternate means of navigation must be utilized 3 2 3 LOSS OF COM RADIO TUNING FUNCTIONS If alternate COM is available Communi
7. Whenever possible RNP and RNAV routes including Standard Instrument Departures SIDs and Standard Terminal Arrival STAR routes should be loaded into the flight plan from the database in their entirety rather than loading route waypoints from the database into the flight plan individually Selecting and inserting individual named fixes from the database is permitted provided all fixes along the published route to be flown are inserted Manual entry of waypoints using latitude longitude or place bearing is prohibited NOTE If flight plan information is imported from a portable electronic device utilizing the Flight Stream 210 all waypoints and flight plan information must be verified by the crew 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 including electronic data and aeronautical charts conform to WGS 84 or equivalent 2 6 Approaches e Instrument approaches using GPS guidance may only be conducted when the GNS is operating in the approach mode LNAV LNAV V L VNAV LPV LP or LP V NOTE Advisory vertical guidance deviation is provided when the GNS annunciates LNAV V or LP V The control
8. ational The affected procedure is prohibited from being flown using data from the navigation database until a new navigation database is installed in the aircraft and verified that the discrepancy has been corrected Navigation database discrepancies can be reported at FlyGarmin com by selecting Aviation Data Error Report Flight crew and operators can view navigation database alerts at FlyGarmin com then select NavData Alerts If the navigation database cycle will change during flight the flight crew must ensure the accuracy of navigation data including suitability of navigation facilities used to define the routes and procedures for flight If an amended chart affecting navigation data is published for the procedure the database must not be used to conduct the procedure 190 00356 03 Rev E AFMS Garmin GNS 4XXW GPS SBAS System Page 8 of 21 FAA APPROVED 2 5 Flight Planning For flight planning purposes in areas where SBAS coverage is not available the flight crew must check RAIM availability e Within the United States RAIM availability can be determined using the Garmin WFDE Prediction program Garmin part number 006 A0154 04 software version 3 00 or later approved version with Garmin approved antennas or the FAA s enroute and terminal RAIM prediction website www raimprediction net or by contacting a Flight Service Station e Within Europe RAIM availability can be determined using the Garmin WFDE Prediction program
9. cations 20 0 cece eee ccccccccccccecececeesesesescececeeeseeees USE ALTERNATE COM If no alternate COM is available COM RMT XFR key if installed PRESS AND HOLD FOR 2 SECONDS NOTE This procedure will tune the active COM radio the emergency frequency 121 5 regardless of what frequency is displayed on the GNS Certain failures of the tuning system will automatically tune 121 5 without flight crew action AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 15 of 21 Section 4 NORMAL PROCEDURES Refer to the 4X XW Series unit Quick Reference Guide defined in paragraph 2 1 on page 7 of this document for normal operating procedures This includes all GPS operations VHF COM and NAV and Multi Function Display information For information on TIS traffic or data linked weather see the Pilot s Guide addendum for optional displays For information on active traffic device or Stormscope operation and displays see the Pilot s Guide addendum for display interfaces The 4XXW Series unit requires a reasonable degree of familiarity to prevent operations without becoming 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 a
10. dvantage of these training tools to enhance system familiarization 4 1 Unit Power On Database 3 323 Gesei BA GRR ies REVIEW EFFECTIVE DATES Self Pests vince as VERIFY OUTPUTS TO NAV INDICATORS Self Test GPS Remote Annunciator If Installed NAL O EASE EEE hes es sects eh eos east E RI ILLUMINATED GPS ARREN E EAE AE eee bai oat ae ead ILLUMINATED TINE Gia scat Seal oes ee eee eae eR a es ILLUMINATED TERM sates Seas ces snvovs hase ag cad he era eee eee eS ILLUMINATED WPT ioe eles evel cepseteten Sere eed OA an E tae ee ILLUMINATED PR sabes a Sosa Cab saveve he dave gee E bed A ewe ewes ILLUMINATED MSG rrenen ces cetean tere aad A ee epee ees ILLUMINATED SUSPB is kek ee eee a eM A ees ILLUMINATED 4 2 Before Takeoff System Messages and Annunciators 0 cece eee esse cee cseecneeeneeees CONSIDERED 190 00356 03 Rev E AFMS Garmin GNS 4XXW GPS SBAS System Page 16 of 21 FAA APPROVED 4 3 HSI and EHSI Operation If an HSI is used to display navigation data from the GNS the pilot should rotate the course pointer as prompted on the GNS If an EHSI is used to display navigation data from the GNS the course pointer may autoslew to the correct course when using GPS navigation When using VLOC navigation the course pointer will not autoslew and must be rotated to the correct course by the pilot For detailed information about the functionality of the EHSI system refer to the FAA approved Flight Manual or Flight Manual Suppleme
11. ems Additional equipment may be required to obtain operational approval to utilize RNP 4 performance This does not constitute an operational approval The Garmin GNSS navigation system complies with the accuracy integrity and continuity of function and contains the minimum system functions required for P RNAV operations in accordance with JAA Administrative amp Guidance Material Section One General Part 3 Temporary Guidance Leaflets Leaflet No 10 SAA 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 function and contains the minimum system functions required for B RNAV operations in accordance with EASA AMC 20 4 The Garmin GNSS navigation system complies with the equipment requirements for P RNAV and B RNAV RNAV 5 operations in accordance with AC 90 96A CHG 1 This does not constitute an operational approval Garmin International holds an FAA Type 2 Letter of Acceptance LOA in accordance with AC 20 153 for database integrity quality and database management practices for the navigation database Flight crew and operators can view the LOA status at FlyGarmin com then select Type 2 LOA Status Navigation information is referenced to the WGS 84 reference system Note that for some types of aircraft operation and for operation in non U S airspace separate operational appr
12. for IFR operations to aircraft limited to VFR operations Additional aircraft systems may be required for IFR operational approval Systems limited to VFR shall be placarded in close proximity to the 4XXW Series unit GPS LIMITED TO VFR USE ONLY AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 7 of 21 2 3 System Software This AFMS AFM is applicable to the software versions shown in Table 1 The Main and GPS software versions are displayed on the start up page immediately after power on Approved Software Version Software Item or later FAA approved versions for this STC SW version As displayed on unit Main SW Version GPS SW Version Flight Stream 210 2 Ti 2 11 a on GNS Table 1 Required Equipment 2 4 Navigation database GPS SBAS based IFR enroute oceanic and terminal navigation is prohibited unless the flight crew verifies and uses a valid compatible and current navigation database or verifies each waypoint for accuracy by reference to current approved data GPS or GPS and RNAV GPS instrument approaches using the Garmin navigation system are prohibited unless 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 Intern
13. in com connext supported_devices AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E Page 21 of 21
14. l be delayed canceled or rerouted on a track where RAIM requirements can be met Applicable to dual installations consisting of two Garmin GNSS units For flight planning purposes for operations where the route requires Class II navigation the aircraft s operator or flight crew must use the Garmin WFDE Prediction program to demonstrate that there are no outages on the specified route that would prevent the Garmin GNSS navigation system to provide GPS Class II navigation in oceanic and remote areas of operation that requires RNP 10 or RNP 4 capability If the Garmin WFDE Prediction program indicates fault exclusion FDE will be unavailable for more than 34 minutes in accordance with FAA Order 8400 12A for RNP 10 requirements or 25 minutes in accordance with FAA Order 8400 33 for RNP 4 requirements then the operation must be rescheduled when FDE is available AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 9 of 21 Both Garmin GPS navigation receivers must be operating and providing GPS navigation guidance for operations requiring RNP 4 performance North Atlantic NAT Minimum Navigational Performance Specifications MNPS Airspace operations per AC 91 49 and AC 120 33 require both GPS SBAS receivers to be operating and receiving usable signals except for routes requiring only one Long Range Navigation sensor Each display computes an independent navigation solution based on its internal GPS receiver
15. ling minimums remain LNAV or LP even when advisory vertical guidance is provided Advisory vertical guidance information displayed on the VDI in this mode is only an aid to help flight crews comply with altitude restrictions When using advisory vertical guidance the flight crew must use the primary barometric altimeter to ensure compliance with all altitude restrictions in 190 00356 03 Rev E AFMS Garmin GNS 4XXW GPS SBAS System Page 10 of 21 FAA APPROVED accordance with the LNAV or LP approach procedure e When conducting instrument approaches referenced to true North the NAV Angle on the AUX Units Position page must be set to True e The navigation equipment required to join and fly an instrument approach procedure is indicated by the title of the procedure and notes on the JAP chart Navigating the final approach segment that segment from the final approach fix to the missed approach point of an ILS LOC LOC BC LDA SDF MLS VOR TACAN approach or any other type of approach not approved for GPS is not authorized with GPS navigation guidance GPS guidance can only be used for approach procedures with GPS or RNAV in the procedure title When using the Garmin VOR LOC GS receivers to fly the final approach segment VOR LOC GS navigation data must be selected and presented on the CDI of the pilot flying e Not all published Instrument Approach Procedures IAP are in the navigation database Flight crews planning to fly an RNAV i
16. nal approach fix as the active waypoint the GNS will issue a flashing message indication with the following message APR Guidance Available Use PROC before A P APR PROE Button viz cia dia niki Gun a O A EA PRESS Enable A P APR Outputs oo esceeeseseseeceseceseseceeeneneeeees SELECT ENT Buttons inir nd aate diss te eis E e EEO A EERTE PRESS If coupled Autopilot will revert to ROL mode at this time AUtOpilt noes creeeeeeeeeeeeeeeeees ENGAGE APPROACH MODE O 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 course with the final approach fix as the active waypoint the GNS will enable vertical guidance Vertical Guidance cccccccccccecececeeeeeeeeees CONFIRM AVAILABLE AUtOpilOt 0 2 eceeeececeseeseeeeeeseeeeeeenees ENGAGE APPROACH MODE O The autopilot does not support any vertical capture or tracking in this installation Analog only autopilots should use APR mode for coupling to LNAV approaches Autopilots which support digital roll steering commands GPSS may utilize NAV mode and take advantage of the digital tracking during LNAV only approaches 190 00356 03 Rev E AFMS Garmin GNS 4XXW GPS SBAS System Page 18 of 21 FAA APPROVED 4 6 Traffic Mode Selection Optional If the GNS is interfaced to a traffic device the GNS can be used to control the mode of the traffic system This i
17. nce 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 require operational approval from the FAA The Garmin GNSS navigation system complies with the equipment requirements of AC 90 100A for RNAV 2 and RNAV 1 operations In accordance with AC 90 100A Part 91 operators except subpart K following the aircraft and training guidance in AC 90 100A are authorized to fly RNAV 2 and RNAV 1 procedures Part 91 subpart K 121 125 129 and 135 operators require operational approval from the FAA AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 5 of 21 Applicable to dual installations consisting of two Garmin GNSS units The Garmin GNSS navigation system has been found to comply with the requirements for GPS Class II oceanic and remote navigation RNP 10 without time limitations in accordance with AC 20 138A and FAA Order 8400 12A The Garmin GNSS navigation system can be used without reliance on other long range navigation systems This does not constitute an operational approval The Garmin GNSS navigation system has been found to comply with the navigation requirements for GPS Class II oceanic and remote navigation RNP 4 in accordance with AC 20 138A and FAA Order 8400 33 The Garmin GNSS navigation system can be used without reliance on other long range navigation syst
18. nly and is not equivalent to warnings provided by TAWS AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 11 of 21 The terrain display is intended to serve as a situational awareness tool only By itself it may not provide either the accuracy or the fidelity on which to base decisions and plan maneuvers to avoid terrain or obstacles 2 9 VNAV Vertical Navigation Calculation Page VNAV information accessible by pressing the VNAV button may be utilized for advisory information only Use of VNAV information for Instrument Approach Procedures does not guarantee Step Down Fix altitude protection or arrival at approach minimums in a normal position to land 2 10 Weather Display Optional This limitation applies to data linked weather 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 weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather product may be significantly older than the indicated weather product age Do not rely solely upon data link services
19. 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 with a GTN and the GTN Crossfill feature is enabled on the GNS then auto switching from GPS to VLOC guidance on the CDI for ILS LOC approaches will be disabled on the GNS If the flight plan on an interfaced GTN is altered while in a hold the GNS will reinitiate guidance to the holding waypoint and sequence into the hold upon crossing the waypoint If the Missed Approach is activated on the GTN prior to reaching the Missed Approach Point the GTN will automatically resume leg sequencing upon reaching the Missed Approach Point The GNS will remain suspended upon reaching the Missed Approach Point and leg sequencing must be manually resumed 190 00356 03 Rev E AFMS Garmin GNS GPS SBAS System Page 20 of 21 7 3 Flight Stream 210 The Flight Stream 210 provides wireless communication of specific flight plan information 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 S500W 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 garm
20. nstrument approach must ensure that the navigation database contains the planned RNAV Instrument Approach Procedure 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 e 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 installations of a Garmin 4X XW 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 however the FAA requires that vertical coupling of an autopilot for approaches be demonstrated to meet their intended function and provide safe and proper operation to published minimums This installation is limited to O Lateral coupling only for GPS approaches Coupling to the vertical path for GPS approaches is not authorized 2 8 Terrain Proximity Function Terrain and obstacle information appears on the map and terrain display pages as red and yellow tiles or towers and is depicted for advisory use only Aircraft maneuvers and navigation must not be predicated upon the use of the terrain display Terrain and obstacle information is advisory o
21. nt for that 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 system in an analog NAV mode will follow GPS or VHF navigation guidance as they would with existing VOR receivers Autopilots that support GPSS or GPS Roll Steering in addition to the analog course guidance will lead course changes fly arcing procedures procedure turns and holding patterns if coupled in GPSS mode For autopilot operating instructions refer to the FAA approved Flight Manual or Flight Manual Supplement for the autopilot AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 17 of 21 4 5 Coupling the Autopilot during approaches CAUTION When the CDI source is changed on the GNS autopilot mode may change Confirm autopilot mode selection after CDI source change on the GNS Refer to the FAA approved Flight Manual or Flight Manual Supplement for the autopilot O This installation prompts the flight crew and requires the pilot to enable the approach outputs just prior to engaging the autopilot in APR mode To couple an approach Once established on the final approach course with the fi
22. or Europe s AUGER GPS RAIM Prediction Tool at http augur ecacnav com augur app home e For other areas use the Garmin WFDE Prediction program This RAIM availability requirement is not necessary if SBAS coverage is confirmed to be available along the entire route of flight The route planning and WEDE prediction program may be downloaded from the Garmin website on the internet For information on using the WFDE Prediction Program refer to Garmin WAAS FDE Prediction Program part number 190 00643 01 WFDE Prediction Program Instructions For flight planning purposes for operations within the U S National Airspace System on RNP and RNAV procedures when SBAS signals are not available the availability of GPS RAIM shall be confirmed 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 RNAV RNAV 5 and P RNAV airspace if more than one satellite is scheduled to be out of service then the availability of GPS RAIM shall be confirmed for the intended flight route and time In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended flight the flight shal
23. oval s may be required in addition to equipment installation and airworthiness approval 190 00356 03 Rev E AFMS Garmin GNS 4XXW GPS SBAS System Page 6 of 21 FAA APPROVED Section 2 LIMITATIONS 2 1 Pilot s Guide The Quick Reference 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 4X XW Series unit e 400W Series Quick Reference Guide P N 190 00356 01 Rev J 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 4X XW Series unit GDL 69 69A XM Satellite Data link GDL 88 ADS B Transceiver GTX 330 330D TIS GTS 8XX Series TAS Flight Stream 210 e 400W S00W 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 4X XW Series unit Stormscope Lightning Detection System Skywatch Traffic Advisory System Bendix King Traffic Advisory System Avidyne Ryan TCAD Traffic System e 400W S00W Series Display Interfaces P N 190 00356 31 Rev D 2 2 Kinds of Operation This AFM supplement does not grant approval
24. s 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 current weight and balance data AFMS Garmin GNS 4XXW GPS SBAS System 190 00356 03 Rev E FAA APPROVED Page 19 of 21 Section 7 SYSTEM DESCRIPTIONS 7 1 Pilot s Guide See Garmin 4XXW Series unit Pilot s Guide for a complete description of the 4XXW Series unit 7 2 Manual GTN Crossfill Manual GTN Crossfill is a feature that will keep the GNS system in sync with a flight plan that is being used on the GTN system The GTN will not automatically keep its flight plan in sync with changes made on the GNS system Manual crossfill feature is one way from the GTN to the GNS The GTN systems support a variety of procedure leg types that the GNS systems do not support As such it is normal and expected that the flight plan leg that is displayed on the GNS system will not always match the flight plan leg on the GTN system Departure arrival and approach procedures contain leg types that the GNS does not support The GNS typically skips over these leg types and provides no guidance Guidance may be available on the GTN but
25. te Seyed Youssef Hashemi cae Supplement Mer Flt Test Br ANM 160L 8 FAA Los Angeles ACO Transport Airplane Directorate Date Nov 20 2007 B All 07 31 09 Added D to STC number David G Armstrong added LP approach type 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 20 2014 Updated See Page 1 document revisions and added Flight Stream 210 11 Added note for Flight Stream 210 13 14 Added sections 2 14 and 2 15 21 Updated GTN Crossfill section 22 Added Section 7 3 190 00356 03 Rev E Page 2 of 21 AFMS Garmin GNS 4XXW GPS SBAS System FAA APPROVED Table of Contents SECTION PAGE Section 1 GENERAL 4 1 1 Garmin 4XXW Series GPS WAAS Nav Com 4 1 2 GPS SBAS TSO C146a Class 3 Operation 5 Section 2 LIMITATIONS 7 2 1 Pilot s Guide 7 2 2 Kinds of Operation 7 2 3 System Software 8 2 4 Navigation database 8 2 5 Flight Planning 9 2 6 Approaches 10 2 7 Autopilot Coupling 11 2 8 Terrain Proximity Function 11 2 9 VNAV Vertical Navigation Calculation Page 12 2 10 Weather Display Optional 12 2 11 Traffic Display Optional 12 2 12 Manual GTN Crossfill 12 2 13 Flight Stream 210 Optional 12 Section 3 EMERGENCY PROCEDURES
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