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RFMS, Bell 407 GTN GPS/SBAS System 

190-01007-J4 Rev. 1 

 

Page 21 of 22 

When installed in an aircraft without a heading source or if Track Up orientation 
is selected the maps will be oriented as follows: 

 

Until a valid track is acquired after startup the track defaults to 360.   

 

When groundspeed is less than 5 knots the ownship icon is shown as a 
non-directional icon and the map orientation is latched at the last valid 
track. 

 

When groundspeed is between 5 and 10 knots, the ownship icon is 
shown as a non-directional icon and the map orientation is oriented to 
the current track. 

 

When groundspeed is in excess of 10 knots the ownship icon is a 
directional icon oriented to track and the map is oriented to track. 

The Terrain Page will default to a Heading Up orientation if a heading data 
source is installed or will orient to Track Up if no heading data is available.  
When oriented to Track Up the Terrain page operation is the same as previously 
described.  When below 10 knots groundspeed and track up the Terrain Page 
cannot be selected to Arc View. 

Airspace Depiction 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 current altitude. Airspace Alerts provide a message indication 
to the flight crew when the aircraft’s current ground track will intercept an 
airspace type that has been selected for alerting. 

NOTE 

Smart Airspace and Airspace Alerts are separate features. 

Turning on/off Smart Airspace does not affect Airspace 

Alerts, and vice versa. 

Fuel Planning Page 

The Fuel Planning page uses Fuel on Board or Fuel Flow as received from an on 
board fuel totalizer, as entered by the pilot at system startup, or as entered by the 
pilot when on the Fuel Planning page. This 

is not

 a direct indication of actual 

aircraft fuel flow or fuel on board and those values are only used for the Fuel 
Planning page. The fuel required to destination is only a calculated and 
predicted value based on the data entered into the planner. It is not a direct 
indication of how much fuel the aircraft will have upon reaching the destination. 
Some approach leg types will result in the fuel burn incorrectly calculated as 
zero which will be evident when a zero value is shown for the fuel burn for a 
leg. 
 

 

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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