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RFMS, Bell 407 GTN GPS/SBAS System 

190-01007-J4 Rev. 1 

FAA APPROVED

 

Page 11 of 22 

Section 2.

 

NORMAL PROCEDURES 

Refer to the Cockpit Reference Guide or the Pilot’s Guide defined in Systems 
Description section of this document for normal operating procedures and a 
complete list of system messages and associated flight crew actions. This 
includes all GPS operations, VHF communication and navigation, traffic, data 
linked weather, HTAWS, and Multi-Function Display information. 

 

2.1

 

Unit Power On  

Database ..........................................................  

REVIEW EFFECTIVE DATES

 

Self Test .................................... 

VERIFY OUTPUTS TO NAV INDICATORS

 

Self Test - HTAWS Remote Annunciator: 

HTAWS (Red) .................................................................... 

ILLUMINATED 

HTAWS (Yellow)............................................................... 

ILLUMINATED

 

HTAWS N/A (Yellow) ....................................................... 

ILLUMINATED

 

AURAL MESSAGE ..................................................... 

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 GSR 56 Iridium datalink is routed through your aircraft’s audio 
panel.  The primary indications of an incoming phone call or SMS text are the 
visual indications on the GTN. 
 

2.4

 

HTAWS INHIBIT 

The HTAWS functions may be inhibited to prevent alerting, if desired. Refer to 
GTN Cockpit Reference Guide for additional information.  When HTAWS is 
inhibited, all HTAWS aural and visual alerting is suppressed, but VCOs remain 
available.  HTAWS shall only be inhibited when in visual contact with terrain 
and when the pilot can be assured of maintaining clearance from terrain and 
obstacles.   
 

To Inhibit HTAWS: 

Home Hardkey ............................................................................................ PRESS 
Terrain Button ............................................................................................. PRESS 
Menu Button ............................................................................................... PRESS 
HTAWS Inhibit Button .................................................... PRESS TO ACTIVATE 
 

 

Содержание Bell 407 GTN

Страница 1: ......

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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