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190-01007-J4 Rev. 1 

RFMS, Bell 407 GTN GPS/SBAS System 

Page 18 of 22 

 

radar altimeter is interfaced with the GTN then VCOs are provided based on 
radar altitude and an additional VCO is provided at 50 feet above ground.  If no 
radar altimeter is interfaced with the GTN then VCOs are provided based on 
GPS altitude above terrain and no 50 foot call is available.  Selecting the altitude 
above ground at which VCOs begin is accomplished using the Audio button 
under the Systems page.   

ALERT ACKNOWLEGE 

The Alert Acknowledge function is used to mute an active HTAWS caution or 
when operating in RP Mode to muffle an active HTAWS warning.  Muting of a 
caution will last for the duration of the caution alert.  Muffling of an RP Mode 
warning will last 10 seconds at which time the pilot may elect to re-muffle the 
alert.   

HTAWS ANNUNCIATORS 

When HTAWS is installed, HTAWS Mode and Status annunciations are 
provided at the lower left corner of the HTAWS enabled GTN unit.  In addition, 
HTAWS Mode and Alert annunciators external to the GTN will be present.   

If an optional G500H system is installed in the helicopter then all HTAWS 
mode and status annunciators from the GTN will be provided on the Primary 
Flight Display of the G500H. 

If no G500H system is installed, then two HTAWS mode and status 
annunciators from the GTN will be installed in the eyebrow panel adjacent to 
the aircraft annunciator panel.  One annunciator provides visual alerts for 
HTAWS warning (red) and caution (yellow) conditions.  The second 
annunciator indicates whether HTAWS protection is being provided by means 
of a dual color HTAWS N/A indication.  When HTAWS N/A is illuminated in 
amber HTAWS protection is not being provided as the result of either a system 
failure or loss of a required input.  When HTAWS N/A is illuminated in white 
HTAWS protection is not being provided as the result of either automatic 
inhibiting below 30 knots groundspeed or pilot inhibiting of HTAWS alerting.   

Traffic System (Optional) 

Traffic may be displayed on the GTN when connected to an approved optional 
TCAS I, TAS, or TIS 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. 

Garmin GTN 6XX or GTN 7XX Cockpit Reference Guide or Garmin GTN 
6XX or GTN 7XX Pilot’s Guide provides additional information regarding the 
functionality of the traffic device. 

Summary of Contents for Bell 407 GTN

Page 1: ......

Page 2: ...90 01007 J4 Rev 1 RFMS Bell 407 GTN GPS SBAS System Page 2 of 22 FAA APPROVED LOG OF REVISIONS Page Revision Number Date Number Description FAA Approved 1 10 23 2013 All Complete Supplement See page 1...

Page 3: ...tions 9 1 10 Glove Use Covered Fingers 10 1 11 Demo Mode 10 1 12 Telephone Audio 10 Section 2 NORMAL PROCEDURES 11 2 1 Unit Power On 11 2 2 Before Takeoff 11 2 3 Telephone SMS Text Optional 11 2 4 HTA...

Page 4: ...190 01007 J4 Rev 1 RFMS Bell 407 GTN GPS SBAS System Page 4 of 22 FAA APPROVED Transponder Control Optional 22 Telephone Audio Optional 22...

Page 5: ...weather products SiriusXM Connext all optional X X X X X Display of terminal procedures data optional X X Display of traffic data X X X X X Display of marker beacon annunciators optional X X Remote au...

Page 6: ...190 01007 J4 Rev 1 RFMS Bell 407 GTN GPS SBAS System Page 6 of 22 FAA APPROVED Figure 1 GTN 750 Control and Display Layout Figure 2 GTN 635 650 Control and Display Layout...

Page 7: ...gation HTAWS Definitions The following terminology is used within this document GPS Global Positioning System GTN Garmin Touchscreen Navigator HTAWS Helicopter Terrain Awareness and Warning System IFR...

Page 8: ...ystem Status page 1 3 SD Card The SD card shall be present in the unit at all times 1 4 Ground Operations SafeTaxi or Chartview functions shall not be used as the sole basis for ground maneuvering Saf...

Page 9: ...products from SiriusXM via a GDL 69 69A and Connext via a GSR 56 Data link weather information shall not be used for maneuvering in near or around areas of hazardous weather The indicated data link we...

Page 10: ...completed The Glove Qualification Procedure is specific to a pilot glove GTN 725 750 or GTN 625 635 650 combination 1 11 Demo Mode Demo mode shall not be used in flight under any circumstances 1 12 T...

Page 11: ...VERIFY VOLUME Self Test HTAWS Annunciator on G500H if installed HTAWS TEST ILLUMINATED 2 2 Before Takeoff System Messages and Annunciators CONSIDERED 2 3 Telephone SMS Text Optional Audio from the GS...

Page 12: ...l no longer provide HTAWS alerting or display relative terrain and obstacle elevations The crew must operate the aircraft in a manner to ensure minimum safe terrain and obstacle separation 3 2 COM RAD...

Page 13: ...senger intercom will function 3 4 OTHER 3 4 1 DATA SOURCE HEADING SOURCE INOPERATIVE OR CONNECTION TO GTN LOST MESSAGE Without a heading source to the GTN the following system limitations will be impo...

Page 14: ...190 01007 J4 Rev 1 RFMS Bell 407 GTN GPS SBAS System Page 14 of 22 FAA APPROVED Section 4 PERFORMANCE No change Section 5 WEIGHT AND BALANCE See current weight and balance data...

Page 15: ...t instrument dimmer switch For this installation dimming of the GTN is controlled by The GTN photocell The aircraft instrument dimmer switch If installed the external HTAWS status annunciator is dimme...

Page 16: ...ude is shown in yellow Obstacles are depicted using a three color scale in which obstacles whose top is at or above the helicopter s current altitude are shown in red while obstacles within 250 feet o...

Page 17: ...MODE menu selection on the terrain page is used to activate the Reduced Protection RP functionality RP Mode reduces alerting thresholds and suppresses aural and visual cautions to allow operation in c...

Page 18: ...HTAWS mode and status annunciators from the GTN will be provided on the Primary Flight Display of the G500H If no G500H system is installed then two HTAWS mode and status annunciators from the GTN wil...

Page 19: ...is interfaced to the GTN A GDL 69 69A Sirius XM datalink is interfaced to the GTN A GSR 56 Iridium datalink is interfaced to the GTN Databases Database versions and effective dates are displayed on t...

Page 20: ...tion when in Normal Mode or muffle an active warning for 10 seconds when in RP Mode MOT Located on the instrument panel or center console Press to create a user waypoint at the present position PTT Lo...

Page 21: ...ion and Alerts The GTN aides the flight crew in avoiding certain airspaces with Smart Airspace and airspace alerts Smart Airspace de emphasizes depicted airspace that is not near the aircraft s curren...

Page 22: ...onder Control Optional The GTN can be interfaced to a Garmin transponder for control and display of squawk code mode and additional transponder functions The activation of the Enable ES button on the...

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