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MARCH 18, 2011 

GARMIN Ltd. or its Subsidiaries, c/o 
Garmin International 1200 E. 151

st

 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. 
 

Содержание GTN 625

Страница 1: ......

Страница 2: ......

Страница 3: ...ware 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 1...

Страница 4: ...T 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 Terrai...

Страница 5: ...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 guid...

Страница 6: ...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 ______________...

Страница 7: ...erators 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 operation...

Страница 8: ...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 s...

Страница 9: ...gation 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...

Страница 10: ...PROVED DATE _________________ SDF Simplified Directional Facility SUSP Suspend TACAN Tactical Air Navigation System TAS Traffic Awareness System TAWS Terrain Awareness and Warning System TCAS Traffic...

Страница 11: ...ow or later revisions must be immediately available to the flight crew whenever navigation is predicated on the use of the GTN y GTN 6XX Cockpit Reference Guide P N 190 01004 04 Rev A y GTN 7XX Cockpi...

Страница 12: ...installations require an external GPS annunciator panel If installed this annunciator must be fully functional to use the GTN for IFR operations Single engine piston aircraft under 6 000 lbs maximum...

Страница 13: ...pace System on RNP and RNAV procedures when SBAS signals are not available the availability of GPS RAIM shall be confirmed for the intended route of flight In the event of a predicted continuous loss...

Страница 14: ...flight plan from the database in their entirety rather than loading route waypoints from the database into the flight plan individually Selecting and inserting individual named fixes from the databas...

Страница 15: ...route oceanic and terminal navigation is prohibited unless the pilot verifies and uses a valid compatible and current Navigation database or verifies each waypoint for accuracy by reference to current...

Страница 16: ...and fly an instrument approach procedure is indicated by the title of the procedure and notes on the IAP chart Navigating the final approach segment that segment from the final approach fix to the mis...

Страница 17: ...ap and terrain display pages as red and yellow tiles or towers and is depicted for advisory use only Aircraft maneuvers and navigation must not be predicated upon the use of the terrain display Terrai...

Страница 18: ...use only The use of the StormScope lightning data on the display for hazardous weather thunderstorm penetration is prohibited StormScope lightning data on the display is intended only as an aid to en...

Страница 19: ...t 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 19 of 31 FAA APPROVED DATE _____...

Страница 20: ...ures 3 1 1 TAWS WARNING Red annunciator and aural PULL UP Autopilot DISCONNECT Aircraft Controls INITIATE MAXIMUM POWER CLIMB Airspeed BEST ANGLE OF CLIMB SPEED After Warning Ceases Power MAXIMUM CONT...

Страница 21: ...Loss Of Integrity mode LOI The mode is indicated on the GTN by an amber DR or LOI If the Loss Of Integrity annunciation is displayed revert to an alternate means of navigation appropriate to the route...

Страница 22: ...S LOC VOR DME ADF Are Available Navigation USE ALTERNATE SOURCES If No Alternate Navigation Sources Are Available DEAD RECKONING DR MODE Navigation USE GTN NOTE y All information normally derived from...

Страница 23: ...tely upon viewing the message the unit will revert to Terminal navigation mode alarm limits If the position integrity is within these limits lateral guidance will be restored and the GPS may be used t...

Страница 24: ...ystem will no longer provide TAWS alerting or display relative terrain and obstacle elevations The crew must maintain compliance with procedures that ensure minimum terrain and obstacle separation 3 2...

Страница 25: ...ed at the expense of basic instrument flying in IMC and 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 the...

Страница 26: ...system CAUTION The pilot must verify proper course selection each time the CDI source is changed from GPS to VLOC 4 4 Autopilot Operation The GTN may be coupled to an optional autopilot if installed...

Страница 27: ...nce established on the final approach course with the final approach fix as the active waypoint the GTN will issue a flashing message indication Flashing Message Button PRESS Enable APR Output Button...

Страница 28: ...ly available to the flight crew y GTN 6XX Pilot s Guide P N 190 01004 03 Rev A or later y GTN 7XX Pilot s Guide P N 190 01007 03 Rev A or later 7 2 Leg Sequencing The GTN supports all ARINC 424 leg ty...

Страница 29: ...0 Latitude in all longitudes y The Obstacle Database has an area of coverage that includes the United States and Europe and is updated as frequently as every 56 days y To avoid unwanted alerts TAWS ma...

Страница 30: ...GTN system is receiving valid heading information the StormScope page will operate in the heading up mode as indicated by the label HDG UP presented at the upper right corner of the display In this m...

Страница 31: ...Switches External switches may be installed and interfaced to the GTN These switches may be stand alone or integrated with a TAWS or GPS annunciator Table 3 lists the switches and function they perfor...

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