Garmin Bell 407 GTN Bedienungsanleitung

190-01007-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

10/23/2013

All

Complete Supplement

See page 1

RFMS, Bell 407 GTN GPS/SBAS System 190-01007-J4 Rev. 1

FAA APPROVED Page 3 of 22

Table of Contents

SECTION PAGE

GENERAL INFORMATION 5

Garmin GTN Navigators 5

Capabilities 7

Definitions 7

Section 1. LIMITATIONS 8

1.1 Kinds of Operation 8

1.2 Applicable System Software 8

1.3 SD Card 8

1.4 Ground Operations 8

1.5 Terrain Proximity Function (All Units) 8

1.6 HTAWS Function (Optional) 9

1.7 Datalinked Weather Display (Optional) 9

1.8 Traffic Display (Optional) 9

1.9 Flight Planner/Calculator Functions 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 HTAWS INHIBIT 11

Section 3. EMERGENCY / MALFUNCTION PROCEDURES 12

3.1 HTAWS 12

3.2 COM RADIO 12

3.3 AUDIO PANEL 13

3.4 OTHER 13

Section 4. PERFORMANCE 14

Section 5. WEIGHT AND BALANCE 14

SYSTEM DESCRIPTIONS 15

Pilot’s Guide 15

Power 15

Lighting Controls 15

GMA 35 Audio Panel (Optional) 15

TERRAIN PROXIMITY 16

HTAWS 16

Traffic System (Optional) 18

Datalinks (Optional) 19

Databases 19

External Switches 20

Map Orientation 20

Airspace Depiction and Alerts 21

Fuel Planning Page 21

Charts (Optional) 22

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

RFMS, Bell 407 GTN GPS/SBAS System 190-01007-J4 Rev. 1

FAA APPROVED Page 5 of 22

GENERAL INFORMATION

Garmin GTN Navigators

The Garmin GTN navigation system is a GPS system with a Satellite Based

Augmentation System (SBAS), comprised of one or more Garmin TSO-C146c

GTN 625, 635, 650, 725, or 750 navigator(s) and one or more Garmin approved

GPS/SBAS antenna(s).

GTN system functions are shown in Table 1.

GTN 625

GTN 635

GTN 650

GTN 725

GTN 750

GPS SBAS Navigation

VHF Com Radio, 118.00 to 136.990, MHz, 8.33 or 25 kHz

increments

VHF Nav Radio, 108.00 to 117.95 MHz, 50 kHz increments

LOC and Glideslope non-precision and precision approach

guidance, 328.6 to 335.4 MHz tuning range

Moving map including topographic, terrain, aviation, and

geopolitical data

Display of datalink weather products, SiriusXM, Connext ( all

optional)

Display of terminal procedures data (optional)

Display of traffic data

Display of marker beacon annunciators (optional)

Remote audio panel control (optional)

Remote transponder control (optional)

Remote audio entertainment datalink control (optional

TSO-C194 HTAWS (optional)

Supplemental calculators and timers

Control of GSR 56 Iridium Satellite Phone and SMS Text

(optional)

Table 1 –GTN Functions

The GPS navigation functions and optional VHF communication and navigation

radio functions are operated by dedicated hard keys, a dual concentric rotary

knob, or the touchscreen.

The GTN requires a reasonable degree of familiarity to avoid becoming too

engrossed at the expense of basic see-and-avoid in VMC. 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.

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

RFMS, Bell 407 GTN GPS/SBAS System 190-01007-J4 Rev. 1

FAA APPROVED Page 7 of 22

Capabilities

The following GTN equipment is installed in this aircraft:

GTN 750

GTN 725

GTN 650

GTN 635

GTN 625

The GTN system and associated navigation interface in this aircraft have the

following capability, in addition to the core GPS navigation and display

capability:

VHF Communication Radio

VHF Navigation

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: Instrument Flight Rules

LOC: Localizer

NOTAM: Notice to Airmen

RMT: Remote

SBAS: Satellite Based Augmentation System

SD: Secure Digital

TAS: Traffic Awareness System

TCAS: Traffic Collision Avoidance System

TFR: Temporary Flight Restriction

TIS: Traffic Information Service

VCO: Voice Call Out

VHF: Very High Frequency

VFR: Visual Flight Rules

VMC: Visual Meteorological Conditions

XFR: Transfer

190-01007-J4 Rev. 1 RFMS, Bell 407 GTN GPS/SBAS System

Page 8 of 22 FAA APPROVED

Section 1. LIMITATIONS

1.1 Kinds of Operation

This model helicopter shall only be operated under VFR conditions in

accordance with 14 Code of Federal Regulations Part 91 and/or Part 135. This

RFM supplement does not grant approval for IFR operations to aircraft limited

to VFR operations.

1.2 Applicable System Software

Use of this RFMS is limited to the software versions shown in Table 2.

Software Item

Software Version

(or later FAA Approved versions for this STC)

Main SW Version

4.00

Table 2 - Software Versions

The Main software versions are displayed on the start-up page immediately after

power-on. All software versions displayed in Table 2 can be viewed on the

System –System 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.

SafeTaxi and Chartview functions do not comply with the requirements of AC

20-159 and are not qualified to be used as an airport moving map display

(AMMD). SafeTaxi and Chartview may be used by the flight crew to orient

themselves on the airport surface to improve flight crew situational awareness

during ground operations.

1.5 Terrain Proximity Function (All Units)

Aircraft maneuvers and navigation shall not be predicated upon the use of the

terrain display.

The terrain display is intended to assist the pilot with maintaining awareness of

the proximity of terrain and obstacles to the rotorcraft. By itself, the terrain

display may not provide either the accuracy or the fidelity on which to base

decisions and plan maneuvers to avoid terrain or obstacles.

RFMS, Bell 407 GTN GPS/SBAS System 190-01007-J4 Rev. 1

FAA APPROVED Page 9 of 22

1.6 HTAWS Function (Optional)

HTAWS shall NOT be used for navigation purposes.

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.

RP Mode shall only be used when in visual contact with terrain.

External HTAWS annunciators installed in the aircraft shall be fully functional

in order to use the HTAWS system.

The external “HTAWS ALERT ACK” switch shall be used in lieu of the Alert

Acknowledge function under the Terrain page menu to minimize pilot workload

during alert conditions.

NOTE

Terrain Proximity and HTAWS are separate features and

mutually exclusive. If “HTAWS” is shown on the bottom

right of the dedicated terrain page, then HTAWS is installed.

1.7 Datalinked Weather Display (Optional)

This limitation applies to datalinked weather 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 weather product age shall not be used to determine the

age of the weather information shown by the data link weather product.

Information provided by data link weather products may not accurately depict

current weather conditions. 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.

Data link services shall not be the sole means used to obtain Temporary Flight

Restriction (TFR) or Notice to Airmen (NOTAM) information. Not all TFRs

and NOTAMS may be available on the GTN.

1.8 Traffic Display (Optional)

The display of traffic is an aid to visual acquisition and shall not be utilized for

aircraft maneuvering.

1.9 Flight Planner/Calculator Functions

The Fuel Planning page shall not be used as a means to determine actual fuel on

board the aircraft.

190-01007-J4 Rev. 1 RFMS, Bell 407 GTN GPS/SBAS System

Page 10 of 22 FAA APPROVED

1.10 Glove Use / Covered Fingers

No article shall be used to cover fingers used to operate the GTN unless the

Glove Qualification Procedure located in the Pilot’s Guide/Cockpit Reference

Guide has been successfully 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 Telephone Audio

Telephone audio shall not be turned on to the pilot or co-pilot unless a phone

call is active.

Failure to turn off telephone audio when the telephone is not in use may result in

telephone ringer or text message aural notifications being received during

critical phases of flight.

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