Garmin GTN 650 STC GTN 6XX/7XX AFMS

Garmin GTN 650 Manual

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  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 1
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 2
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 3
    MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM Table of Contents SECTION Section 1. GENERAL 1.1 Garmin GTN Navigators 1.2 Capabilities 1.3 Electronic Flight Bag 1.4 Definitions Section 2. LIMITATIONS 2.1 Cockpit Reference Guide Section 7. SYSTEM DESCRIPTIONS 7.1 Pilot's Guide 7.2 Leg
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 4
    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 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
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 5
    MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 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 datalink weather products
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 6
    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 Figure 1 - GTN 750 Control and Display Layout Figure 2 - GTN 635/650 Control and Display Layout 190-01007-A2 Rev
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 7
    151st Street Olathe, KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 1.2 Capabilities GPS/SBAS TSO-C146c Class 3 Operation: The GTN, when installed in accordance with STC SA02019SE-D, has airworthiness approval
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 8
    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 The Garmin GNSS navigation system, as installed in this aircraft, complies with the accuracy, integrity, and continuity
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 9
    66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 1.4 Definitions The following Global Navigation Satellite System GPS: Global Positioning System GPSS: GPS Roll Steering GTN: Garmin Touchscreen Navigator HSI:
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 10
    Olathe, KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM SDF: SUSP: TACAN: TAS: System Traffic Awareness System Terrain Awareness and Warning System Traffic Collision Avoidance System Traffic Information Service
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 11
    Street Olathe, KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM Section 2. LIMITATIONS 2.1 Cockpit Reference Guide The Garmin GTN 6XX or GTN 7XX Cockpit Reference Guide, part number and revision listed below (or
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 12
    MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 2.3 Minimum Equipment If the installation of the GTN is not limited to VFR, the GTN must have the following system operations: Single GTN Navigator plus a second source of GPS navigation or a
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 13
    MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 2.4 Flight Planning For flight planning purposes, in areas where SBAS coverage is not available, the pilot scheduled to be out of service, then the availability of GPS RAIM shall be confirmed
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 14
    GARMIN GTN NAVIGATION SYSTEM Both Garmin GPS navigation receivers must be operating and providing GPS navigation guidance for operations requiring RNP-4 performance. Applicable to installations consisting of two GTNs: North Atlantic (NAT) Minimum Navigational Performance Specifications Manual entry
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 15
    or verifies each waypoint for accuracy by reference to current approved data. "GPS", "or GPS", and "RNAV (GPS)" instrument approaches using the Garmin navigation system are prohibited unless the pilot verifies and uses the current Navigation database. GPS based instrument approaches must be flown in
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 16
    AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM to define to improve pilot situational awareness during ground operations. 2.10 Approaches a) Instrument approaches using GPS guidance may only be conducted when the GTN is
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 17
    FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM f) IFR approaches are prohibited whenever any physical or visual obstruction (such as a throw-over yoke) restricts pilot view or access to the GTN and/or the CDI. 2.11 Autopilot Coupling IFR installations of a GTN allow the pilot to
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 18
    may be used to cover fingers used to operate the GTN unless the Glove Qualification Procedure located in the Pilot's Guide has been successfully completed. The Glove Qualification Procedure is specific to a pilot / glove / GTN 725, 750 or GTN 625, 635, 650 combination. 190-01007-A2 Rev. 1 FAA
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 19
    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 2.19 Demo Mode Demo mode may not be used in flight under any circumstances. 190-01007-A2 Rev. 1 FAA APPROVED DATE
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 20
    AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM Section 3. EMERGENCY unless either operating in visual meteorological conditions (VMC), or the pilot determines, based on all available information, that turning in addition
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 21
    MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 3.2 Abnormal Procedures 3.2.1 LOSS OF GPS/SBAS NAVIGATION DATA When the GPS/SBAS receiver is inoperative or GPS and Approach modes do not support Dead Reckoning. 190-01007-A2 Rev. 1 FAA
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 22
    USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM If Alternate Navigation from GPS will be removed. y The airplane symbol is removed from all maps. The map will remain centered at the last known position. "NO GPS POSITION"
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 23
    USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 3.2.2 GPS APPROACH DOWNGRADE During a GPS LPV, LNAV/VNAV, or LNAV+V approach, if GPS accuracy requirements cannot be met by the GPS receiver, the GTN will downgrade the
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 24
    to GTN Cockpit Reference Guide for additional information. To Inhibit TAWS: Home Hardkey PRESS Terrain Button PRESS Menu Button PRESS TAWS Inhibit Button PRESS TO ACTIVATE 3.2.7 TER N/A and TER FAIL If the amber TER N/A or TER FAIL status annunciator is displayed, the system will no longer
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 25
    , KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM Section 4. NORMAL PROCEDURES Refer to the Cockpit Reference Guide defined in Section 2.1 of this document or the Pilot's Guide defined in Section 7.1 for normal
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 26
    the EHSI system, refer to the FAA approved Flight Manual or Flight Manual Supplement for that 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 in
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 27
    may change. Confirm autopilot mode selection after CDI source change on the GTN. Refer to the FAA approved Flight Manual or Flight Manual Supplement for the autopilot. … This installation prompts the pilot and requires the pilot to enable the approach outputs just prior to engaging the autopilot in
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 28
    SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM Section 6. WEIGHT AND BALANCE See current weight and balance data. Section 7. SYSTEM DESCRIPTIONS 7.1 Pilot's Guide The Garmin GTN 6XX or GTN 7XX Pilot's Guide, part number and revision listed
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 29
    or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 7.4 Activate GPS Missed Approach If the GTN displays a CDI key on the Map Page (GTN 750) or Default Nav Page (GTN 650) the GTN will autoswitch from VLOC to GPS when the "Activate GPS Missed Approach" button is
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 30
    SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 7.7 Traffic System (Optional) This system is configured for the following type of traffic system. The Garmin GTN 6XX or GTN 7XX Cockpit Reference Guide or Garmin GTN 6XX or GTN 7XX Pilot's Guide provides additional
  • Garmin GTN 650 | STC GTN 6XX/7XX AFMS - Page 31
    Olathe, KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM 7.9 Power y Power to the GTN is provided through a circuit breaker labeled NAV/GPS (1/2). y Power to the optional GTN COM is provided through a circuit
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