Garmin GTN 625 Konfigurationshandbuch

MARCH 18, 2011

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151st Street

Olathe, KS 66062 USA

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

NAVIGATION SYSTEM

190-01007-A2 Rev. 1 Page 3 of 31

FAA APPROVED DATE: _________________

Table of Contents

SECTION PAGE

Section 1. GENERAL 5

1.1Garmin GTN Navigators 5

1.2Capabilities 7

1.3Electronic Flight Bag 8

1.4Definitions 9

Section 2. LIMITATIONS 11

2.1Cockpit Reference Guide 11

2.2Kinds of Operation 11

2.3Minimum Equipment 12

2.4Flight Planning 13

2.5System Use 14

2.6Applicable System Software 15

2.7SD Card 15

2.8Navigation Database 15

2.9Ground Operations 16

2.10Approaches 16

2.11Autopilot Coupling 17

2.12Terrain Proximity Function (All Units) 17

2.13TAWS Function (Optional) 17

2.14Datalinked Weather Display (XM Weather, Optional) 18

2.15Traffic Display (Optional) 18

2.16StormScope®Display (Optional) 18

2.17Flight Planner/Calculator Functions 18

2.18Glove Use / Covered Fingers 18

2.19Demo Mode 19

Section 3. EMERGENCY PROCEDURES 20

3.1Emergency Procedures 20

3.2Abnormal Procedures 21

Section 4. NORMAL PROCEDURES 25

4.1Unit Power On 25

4.2Before Takeoff 25

4.3HSI and EHSI Operation 25

4.4Autopilot Operation 26

4.5Coupling the Autopilot during approaches 27

Section 5. PERFORMANCE 28

Section 6. WEIGHT AND BALANCE 28

Section 7. SYSTEM DESCRIPTIONS 28

7.1Pilot’s Guide 28

7.2Leg Sequencing 28

MARCH 18, 2011

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151st Street

Olathe, KS 66062 USA

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

NAVIGATION SYSTEM

190-01007-A2 Rev. 1 Page 4 of 31

FAA APPROVED DATE: _________________

7.3Auto ILS CDI Capture 28

7.4Activate GPS Missed Approach 29

7.5Terrain Proximity and TAWS 29

7.6GMA 35 Audio Panel (Optional) 29

7.7Traffic System (Optional) 30

7.8StormScope®(Optional) 30

7.9Power 31

7.10Databases 31

7.11External Switches 31

MARCH 18, 2011

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151st Street

Olathe, KS 66062 USA

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

NAVIGATION SYSTEM

190-01007-A2 Rev. 1 Page 5 of 31

FAA APPROVED DATE: _________________

Section 1. GENERAL

1.1 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 navigation system functions are shown in Table 1.

GTN 625

GTN 635

GTN 650

GTN 725

GTN 750

GPS SBAS Navigation:

•Oceanic, enroute, terminal, and non-precision approach

guidance

•Precision approach guidance (LP, LPV)

X X X X X

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

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

LOC and Glideslope non-precision and precision approach guidance

for Cat 1 minimums, 328.6 to 335.4 MHz tuning range X X

Moving map including topographic, terrain, aviation, and geopolitical

data X X X X X

Display of datalink weather products (optional) X X X X X

Display of terminal procedures data (optional) X X

Display of traffic data (optional) X X X X X

Display of StormScope

data (optional) X X X X X

Display of marker beacon annunciators X X

Remote audio panel control X X

Remote transponder control X X X X X

Remote audio entertainment datalink control X X X X X

TSO-C151b Class B TAWS X X X X X

Supplemental calculators and timers X X X X X

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.

MARCH 18, 2011

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151st Street

Olathe, KS 66062 USA

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

NAVIGATION SYSTEM

190-01007-A2 Rev. 1 Page 6 of 31

FAA APPROVED DATE: _________________

Figure 1 - GTN 750 Control and Display Layout

Figure 2 - GTN 635/650 Control and Display Layout

MARCH 18, 2011

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151st Street

Olathe, KS 66062 USA

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

NAVIGATION SYSTEM

190-01007-A2 Rev. 1 Page 7 of 31

FAA APPROVED DATE: _________________

1.2 Capabilities

GPS/SBAS TSO-C146c Class 3 Operation:

The GTN, when installed in accordance with STC SA02019SE-D, has

airworthiness approval for navigation using GPS and SBAS (within the coverage

of a Satellite Based Augmentation System complying with ICAO Annex 10) for

IFR en route, terminal area, and non-precision approach operations (including

those approaches titled “GPS”, “or GPS”, and “RNAV (GPS)” approaches). The

Garmin GNSS navigation system is composed of the GTN navigator and antenna,

and is approved for approach procedures with vertical guidance including “LPV”

and “LNAV/VNAV”, within the U.S. National Airspace System.

The Garmin GNSS navigation system as installed in this aircraft, complies with

the equipment requirements of AC 90-105 and meets the equipment performance

and functional requirements to conduct RNP terminal departure and arrival

procedures and RNP approach procedures without RF (radius to fix) legs. Part 91

subpart K, 121, 125, 129, and 135 operators require operational approval from the

FAA.

The Garmin GNSS navigation system as installed in this aircraft complies with

the equipment requirements of AC 90-100A for RNAV 2 and RNAV 1

operations. In accordance with AC 90-100A, Part 91 operators (except subpart K)

following the aircraft and training guidance in AC 90-100A are authorized to fly

RNAV 2 and RNAV 1 procedures. Part 91 subpart K, 121, 125, 129, and 135

operators require operational approval from the FAA.

Applicable to dual installations consisting of two GTNs: The Garmin GNSS

navigation system, as installed in this aircraft, has been found to comply with the

requirements for GPS Class II oceanic and remote navigation (RNP-10) without

time limitations in accordance with AC 20-138A and FAA Order 8400.12A. The

Garmin GNSS navigation system can be used without reliance on other long-

range navigation systems. This does not constitute an operational approval.

Applicable to dual installations consisting of two GTNs:The Garmin GNSS

navigation system, as installed in this aircraft, has been found to comply with the

navigation requirements for GPS Class II oceanic and remote navigation (RNP-4)

in accordance with AC 20-138A and FAA Order 8400.33. The Garmin GNSS

navigation system can be used without reliance on other long-range navigation

systems. Additional equipment may be required to obtain operational approval to

utilize RNP-4 performance. This does not constitute an operational approval.

MARCH 18, 2011

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151st Street

Olathe, KS 66062 USA

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

NAVIGATION SYSTEM

190-01007-A2 Rev. 1 Page 8 of 31

FAA APPROVED DATE: _________________

The Garmin GNSS navigation system, as installed in this aircraft, complies with

the accuracy, integrity, and continuity of function, and contains the minimum

system functions required for P-RNAV operations in accordance with JAA

Administrative & Guidance Material Section One: General Part 3: Temporary

Guidance Leaflets, Leaflet No 10 (JAA TGL-10 Rev 1). The GNSS navigation

system has [one or more] TSO-C146c Class 3 approved Garmin GTN Navigation

Systems. The Garmin GNSS navigation system as installed in this aircraft

complies with the equipment requirements for P-RNAV and B-RNAV/RNAV 5

operations in accordance with AC 90-96A CHG 1 and JAA TGL-10 Rev 1. This

does not constitute an operational approval.

Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in

accordance with AC 20-153 for database integrity, quality, and database

management practices for the Navigation database. Flight crew and operators can

view the LOA status at FlyGarmin.com then select “Type 2 LOA Status.”

Navigation information is referenced to WGS-84 reference system.

Note that for some types of aircraft operation and for operation in non-U.S.

airspace, separate operational approval(s) may be required in addition to

equipment installation and airworthiness approval.

1.3 Electronic Flight Bag

The GTN as installed in this aircraft supports approval of AC 120-76A Hardware

Class 3, Software Type C Electronic Flight Bag (EFB) electronic aeronautical

chart applications when using current FliteChart or ChartView data. Additional

operational approvals may be required. For operations under 14 CFR Part 91,

Garmin suggests that a secondary or back up source of aeronautical information

necessary for the flight be available to the pilot in the airplane. The secondary or

backup information may be either traditional paper-based material or displayed

electronically. If the source of aeronautical information is in electronic format,

operators must determine non-interference with the GTN system and existing

aircraft systems for all flight phases.

MARCH 18, 2011

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151st Street

Olathe, KS 66062 USA

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

NAVIGATION SYSTEM

190-01007-A2 Rev. 1 Page 9 of 31

FAA APPROVED DATE: _________________

1.4 Definitions

The following terminology is used within this document:

ADF: Automatic Direction Finder

APR: Approach

CDI: Course Deviation Indicator

DME: Distance Measuring Equipment

EFB: Electronic Flight Bag

EHSI: Electronic Horizontal Situation Indicator

GNSS: Global Navigation Satellite System

GPS: Global Positioning System

GPSS: GPS Roll Steering

GTN: Garmin Touchscreen Navigator

HSI: Horizontal Situation Indicator

IAP: Instrument Approach Procedure

IFR: Instrument Flight Rules

ILS: Instrument Landing System

IMC: Instrument Meteorological Conditions

LDA: Localizer Directional Aid

LNAV: Lateral Navigation

LNAV+V: Lateral Navigation with advisory Vertical Guidance

L/VNAV: Lateral/Vertical Navigation

LOC: Localizer

LOC-BC: Localizer Backcourse

LP: Localizer Performance

LPV: Localizer Performance with Vertical Guidance

MLS: Microwave Landing System

OBS: Omnibearing Select

RAIM: Receiver Autonomous Integrity Monitoring

RMT: Remote

RNAV: Area Navigation

RNP: Required Navigational Performance

SBAS: Satellite Based Augmentation System

SD: Secure Digital

MARCH 18, 2011

GARMIN Ltd. or its Subsidiaries, c/o

Garmin International 1200 E. 151st Street

Olathe, KS 66062 USA

AIRPLANE FLIGHT MANUAL SUPPLEMENT or

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for STC SA02019SE-D GARMIN GTN

NAVIGATION SYSTEM

190-01007-A2 Rev. 1 Page 10 of 31

FAA APPROVED DATE: _________________

SDF: Simplified Directional Facility

SUSP: Suspend

TACAN: Tactical Air Navigation System

TAS: Traffic Awareness System

TAWS: Terrain Awareness and Warning System

TCAS: Traffic Collision Avoidance System

TIS: Traffic Information Service

VHF: Very High Frequency

VFR: Visual Flight Rules

VLOC: VOR/Localizer

VMC: Visual Meteorological Conditions

VOR: VHF Omnidirectional Range

WAAS: Wide Area Augmentation System

WFDE: WAAS Fault Data Exclusion

XFR: Transfer

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