Garmin SR02080SE Airplane Flight Manual Supplement
Contents
1. and current The software automatically precludes invalid databases for use by the 400W Database cycle information is displayed at power up on the screen but more detailed information is available on the AUX UTILITY page a Installations with dual 400W 500W Series units will only crossfill between units when they contain the same database cycle Updating of each database must be accomplished on the ground prior to flight 1 4 Terrain Database The 400W Series unit supports Terrain Proximity or HTAWS and requires a Terrain database card to be installed in order for the feature to operate Database cycle information is displayed at power up on the screen but more detailed information is available on the AUX UTILITY page Terrain database cards contain the following data a Due to the terrain resolution used in this system the terrain database is divided into six regions Americas North Americas South Atlantic North Atlantic South Pacific North Pacific South Use of the proper database region must be verified b The Obstacle Database has an area of coverage that includes the United States and Europe and is updated as frequently as every 56 days NOTE The area of coverage may be modified as additional terrain data sources become available 1 5 Navigation No navigation is authorized north of 89 degrees north latitude or south of 89 degrees south latitude FAA APPROVED 90 01226 0 ral meen DATE SEP 27 2012. if the system fails the test HTAWS System Failure is played HTAWS test is only available while on the ground Voice callouts VCOs provide voice annunciation of the aircraft height above terrain when that threshold is crossed VCOs may be enabled by the pilot in 100ft increments from 500 feet above ground level to the surface Enabling VCOs is accomplished using Voice Callout selection in the AUX pages FAA APPROVED 190 01226 06 Rev 1 Page 10 of 14 DATE SEP 2 7 2010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B 3 4 HTAWS Alerts HTAWS visual and aural alerts provided by the Garmin 400W Series GPS WAAS Navigator are shown in the table below ee HTAWS System Failure HTAWS has failed HTAWS has been inhibited by the crew or the aircraft groundspeed has fallen below 30 knots automatic inhi biting HTAWS Not Available HTAWS not available CAUTION TERRAIN Caution Terrain Terrain Forward Looking Terrain Avoidance Caution for Terrain WARNING TERRAIN Waming Terrain Terrain Forward Looking Terrain Avoidance Warning for Terrain CAUTION OBSTACLE Caution Obstacle Obstacle Forward Looking Terrain Avoidance Caution for Obstacle WARNING OBSTACLE Warning Obstacle Obstacle Forward Looking Terrain Avoidance Warning for
3. 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 amp Ref P N 190 00356 00 Rev G 400W 500W Series Optional Displays P N 190 00356 30 Rev H This model helicopter when equipped with the G400W is limited to VFR ONLY operations in accordance with 14 Code of Federal Regulations Part 91 and Part 135 The placard listed below shall be located in close proximity to the 400W Series unit APPROVED FOR DAY NIGHT VFR 1 2 System Software The system must utilize the Main and GPS software versions listed below or later FAA approved versions for this STC The software versions are displayed on the self test page immediately after turn on for approximately 5 seconds or they can be accessed in the AUX pages Subsequent software versions may support different functions Check the 400W Series Pilot s Guide for further information Table 1 Approved Software Versions Approved Software Version or later FAA approved versions for this STC As displayed on unit Main SW Version GPS SW Version Software Item FAA APPROVED 190 01226 06 Rev 1 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B 1 3 Navigation Database The 400W Series unit database cards must be installed
4. the Garmin 400W Series navigator are inhibited below 30 knots groundspeed Display of the terrain and obstacles is supplemental data only Maneuvering solely by reference to the terrain and obstacle display is not authorized NOTE The Terrain and Obstacle Display is intended to serve as a terrain and obstacle awareness tool only The Display and database may not provide the accuracy or fidelity on which to base routine navigation decisions and plan routes to avoid terrain or obstacles FAA APPROVED 190 01226 06 Rev 1 Page 6 of 14 DATE SEP 2 7 2010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B The Obstacle Database does not contain the location of power line poles or wires Also the Obstacle Database contains only KNOWN obstacles and does not contain ALL existing obstacles When alerting is inhibited all Forward Looking Terrain Alerting aural and visual alerting is suppressed HTAWS should be only inhibited when in visual contact with terrain and when the pilot can be assured of maintaining clearance from terrain and obstacles 1 8 HTAWS Annunciations on the PFD Units with HTAWS HTAWS Terrain Awareness and Warning System visual annunciations from the GNS 400W series unit are displayed on the G500H PFD The required HTAWS annunciations appear in the upper right of the PFD Thes
5. visual contact with terrain and when the pilot can be assured of maintaining clearance from terrain and obstacles Use the Enable HTA WS to un inhibit the unit The Mute Active Caution menu selection is used to mute an HTAWS caution that is presently active When the caution is resolved the next caution will be heard It does not mute warnings only cautions The Unmute Active Caution is used to cancel the mute An optional MUTE external switch installation on the cyclic stick is allowed to mute the caution that is presently active in the same manner as using the Page Menu selection The Reduce Protection menu selection is used to activate the Reduce Protection RP functionality RP Mode reduces alerting thresholds and suppresses aural and visual cautions to allow operation in closer proximity to terrain and obstacles while continuing to provide protection from terrain and obstacles The Enable Full Protection menu selection is used to select full protection functionality again An optional RP MODE external switch installation on the cyclic stick is allowed to toggle Reduce Protection and Enable Full Protection in the same manner as using the Page Menu selection The Test HTA WS menu selection is used to activate a manual test which verifies proper operation of the aural and visual annunciations of the system The aural message HTAWS System Test OK is played if the system passes the test
6. 0 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B 1 6 Terrain Proximity Display Units without HTAWS Terrain Proximity refers to the display of terrain information and comprises of a 2 D picture of the surrounding terrain and obstacles relative to the position and altitude of the rotorcraft however it does not provide any alerts Navigation must not be predicated upon the use of the terrain display 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 Terrain is not depicted on the terrain display within Inm of airports and heliports however terrain hazards may exist in these areas 1 7 HTAWS Function Units with HTAWS HTAWS is an optional extension of Terrain Proximity Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with HTAWS warnings HTAWS shall NOT be used for navigation purposes HTAWS is an alerting system The system does NOT guarantee successful recovery from a conflict due to factors such as pilot response aircraft performance and database limitations No standardized recovery technique is defined as recovery maneuvers may vary HTAWS functions performed by
7. GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM As Installed In Bell 206B Reg No S N This document serves as a Rotorcraft Flight Manual Supplement when the rotorcraft is equipped with the Garmin 400W Series unit This document must be carried in the rotorcraft at all times when the Garmin 400W Series unit is installed in accordance with STC SRO02080SE The information contained herein supplements or supersedes the information made available to the operator by the manufacturer in the form of clearly stated placards markings or manuals or in the form of an FAA approved Rotorcraft Flight Manual only in those areas listed herein For limitations procedures and performance information not contained in this document consult the basic placards markings or manuals or the basic FAA approved Rotorcraft Flight Manual FAA APPROVED for Manager Flight Test Branch Federal Aviation Administration Seattle Aircraft Certification Office DATE _ ial o 190 01226 06 Rev 1 Page of 14 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B LOG OF REVISIONS Complete Supplement Mgr Fit Test Br Federal Aviation Administrati
8. ON SYSTEM Bell 206B GENERAL Garmin 400W Series GPS WAAS Nav Com The Garmin 400W Series GPS WAAS Navigator is a panel mounted product that contains a GPS WAAS receiver for GPS approved primary navigation under TSO C1 46a plus optional VHF Com VHF Nav radios and HTAWS in an integrated unit with a moving map and color display The 400W Series unit features a graphical display 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 Com Freq Graphic Movin Comm Freq Dinning Window Map Display pis Direct To Key Flip Flop sired Navigation Info Window vg Range Keys 7 Menu Key z f j 7 Power and Com J PA Volume Squeich __ a Clear Key PS 2 Data Cards Enter Key Function and Nav Radio __ Volume Page Number padine Large Knob p Large Knob k eet Small Knob Com VLOC _ Cursor Press Freq MHz Terrain Flight to activate Small Knob Phase and te Com VLOC GPS Integrity z co OBS Sse Pian gt Procedure Key Freq kHz Annunciator Mounting Key Screw Key Message Navigation Way Source GPS VLOC or GPS PTK Figure 1 400W Series Control and Display La
9. Obstacle Alerting thresholds are reduced Visual and aural annunciation of caution alerts are suppressed Five Hundred HTAWS provides optional 500 ft Four Hundred through 100 ft in 100 ft increments Three Hundred altitude call out alerts Two Hundred One Hundred FAA APPROVED 190 01226 06 Rev 1 Page 11 of 14 DATE SEP 27 2010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B 3 5 GS500H Interface The GNS 400W series unit is interfaced to the GSOOH display system for the purpose of displaying HTA WS annunciations in the pilot s primary field of view Terrain and obstacle alerts are provided by the GNS 400W series unit The alerting mode for G500H Terrain Helicopter Synthetic Vision Technology HSVT will be driven by the HTAWS mode selected on the GNS 400W series unit In the event of a failure of the GNS unit providing HTAWS functionality the HSVT Terrain alerting may be available and the alerting mode can be selected by the pilot on the GSOOH terrain page Section 4 PERFORMANCE No change FAA APPROVED 190 01226 06 Rev 1 Page 12 of 14 DATE SEP 272010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATI
10. annunciated as L VNAV approaches and LNAV approaches with advisory vertical guidance annunciated as LNAV V For LNAV approaches with advisory vertical guidance the 400W Series will annunciate LNAV V indicating vertical guidance is available LNAV minimums will be controlling in this case 3 2 WFDE Prediction Program The Garmin WAAS Fault Detection and Exclusion WFDE Prediction 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 For detailed information refer to the WFDE prediction program instructions 190 00643 01 The availability of FDE is only required for Oceanic or Remote operations FAA APPROVED oc aiik SEP 27 2010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B 3 3 HTAWS Controls The HTAWS function has control options on the HTAWS Page using the MENU key The options are activated by highlighting the desired option and pressing ENTER The Inhibit HTA WS menu selection is used to inhibit HTAWS alerts When alerting is inhibited all HTAWS aural and visual alerting is suppressed HTAWS should be only inhibited when in
11. d 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 This RFMS does not constitute an operational approval for Oceanic or Remote area operations Additional equipment installations or operational approvals may be required a Oceanic navigation requires an additional approved long range oceanic and or remote area navigation system with independent display sensors antenna and power source It may be a second 400W S00W Series unit b Redundant VHF Com and VHF Nav systems may be required for other than U S 14 CFR Part 91 operations Check foreign regulation requirements as applicable It may be a second 400W SO0W Series unit c Operations approval may be granted for the use of the 400W Series unit RAIM prediction function in lieu of the Prediction Program for operators requiring this capability Refer to your appropriate civil aviation authorities for these authorizations FAA APPROVED 190 01226 06 Rev 1 Page 14 of 14 DATE SEP 2 7 2010
12. e annunciations include TERRAIN red TERRAIN yellow OBSTACLE red OBSTACLE yellow HTAWS N A yellow HTAWS INHB white These annunciations are not relative to the terrain elevation information displayed on the G500H MFD FAA APPROVED 190 01226 06 Rev 1 Page 7 of 14 DATE ___ SFP 27 2010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B Section 2 EMERGENCY PROCEDURES 2 1 Emergency Procedures No change 2 2 Abnormal Procedures a b c d If the Garmin 400W Series unit GPS navigation information is not available or is invalid utilize other remaining operational navigation equipment installed in the aircraft as appropriate If the 400W Series unit loses GPS position and reverts to Dead Reckoning mode indicated by the annunciation of DR in the lower left of the display the moving map will continue to be displayed Rotorcraft position will be based upon the last valid GPS position and estimated by Dead Reckoning methods Changes in airspeed or winds aloft can affect the estimated position substantially Dead Reckoning is only available in Enroute and Oceanic mode Terminal and Approach modes do not support DR If a Loss of Integrity INTEG message is displayed during Enroute Terminal continue to navigate using GPS equipment and periodically c
13. on Rev No Date Description FAA Approved Seattle Aircraft Certification Office Original Date q 12 w 190 01226 06 Rev 1 Page 2 of 14 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B Table of Contents Section 1 LIMITATIONS 4 1 1 Pilot s Guide 4 1 2 System Software 4 1 3 Navigation Database 5 1 4 Terrain Database 5 1 5 Navigation 5 1 6 Terrain Proximity Display Units without HTA WS 6 1 7 HTAWS Function Units with HTAWS 6 1 8 HTAWS Annunciations on the PFD Units with HTAWS 7 Section 2 EMERGENCY PROCEDURES 8 2 1 Emergency Procedures 8 2 2 Abnormal Procedures 8 Section 3 NORMAL PROCEDURES 9 3 1 Approaches with Vertical Guidance 9 3 2 WFDE Prediction Program 9 3 3 HTAWS Controls 10 3 4 HTAWS Alerts 11 3 5 GS500H Interface 12 Section 4 PERFORMANCE 12 GENERAL 13 Garmin 400W Series GPS WAAS Nav Com 13 Operation 14 Class II Oceanic Remote and other Operations 14 FAA APPROVED 190 01226 06 Rev 1 Page 3 of 14 DATE SEP 9 7 2010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B Section 1 LIMITATIONS 1 1 Pilot s Guide The GARMIN 400W Series Pilot s Guide part number and revision listed below or later
14. ross check the GPS guidance to other approved means of navigation When a Terrain or Obstacle Awareness CAUTION occurs verify the aircraft flight path and correct it if required When a Terrain or Obstacle Awareness WARNING occurs immediately initiate a maneuver that will provide maximum terrain or obstacle clearance until all alerts cease FAA APPROVED 190 01226 06 Rev 1 Page 8 of 14 DATE SEP 9 7 2010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B Section 3 NORMAL PROCEDURES Refer to the 400W Series unit Pilot s Guide defined in paragraph 1 1 of this document for normal operating procedures This includes all GPS operations VHF COM and NAV and Multi Function Display information Although intuitive and user friendly the 400W Series unit requires a reasonable degree of familiarity to enable unit operations without becoming too engrossed at the expense of basic see and avoid Pilot workload will be higher for pilots with limited familiarity in using the unit Garmin provides training tools with the Pilot s Guide and PC based simulator Pilots should take full advantage of these training tools to enhance system familiarization 3 1 Approaches with Vertical Guidance The 400W Series unit supports three types of GPS approaches with vertical guidance LPV approaches LNAV VNAV
15. yout Optional HTAWS functions are controlled by soft keys located on the dedicated TAWS page An installation option allows some of the controls to be installed on the cyclic grip FAA APPROVED 190 01226 06 Rev 1 Page 13 of 14 DATE SEP 9 7 2010 GARMIN Ltd or its subsidiaries c o Garmin International 1200 E 151 Street Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT GARMIN 400W SERIES GPS WAAS NAVIGATION SYSTEM Bell 206B Operation GPS WAAS TSO C146a Class 3 Operation The Garmin 400W Series unit uses GPS and WAAS within the coverage of a Space Based Augmentation System complying with ICAO Annex 10 for enroute terminal area non precision approach operations including GPS or GPS and RNAV approaches and approach procedures with vertical guidance including LNAV VNAV and LPV Navigation is accomplished using the WGS 84 NAD 83 coordinate reference datum GPS navigation data is based upon use of only the Global Positioning System GPS operated by the United States of America Class II Oceanic Remote and other Operations The Garmin 400W Series as installed has been found to comply with the requirements for GPS primary means of Class II navigation in oceanic and remote airspace when used in conjunction with WAAS Garmin Prediction Program part number 006 A0154 03 Oceanic operations are supported when the 400W Series unit annunciates OCN This provides an alarm limit of four NMI an
Download Pdf Manuals
Related Search