Garmin Supplemental Manual

The GPS navigation functions and optional transponder and navigation radio functions are operated by dedicated hard keys, a dual concentric rotary knob, or the touchscreen. AFMS, Garmin GPS/GNC/GNX System FAA APPROVED 190-02207-A3 Rev. 3 Page 1 Message Annunciation and Key M MSG Function Keys Direct To Key Map * Flight Plan -08- Traffic X ENR TO -D▸ Terrain FIS-B Weather Nearest XPDR STBY 1200 ARTTY PROC Waypoint info BREAF Utilities System 4.31 N Home MAP FPL INRST-Push Photo Sensor GARMIN SD Card Slot Home/Power Buttor Transponder Code and Mode Large and Small Knobs From/To Field and Annunciations To/From Current Page Indication and Knob CDI Shortcuts Figure 1 - GNX 375 Control and Display Layout Function Keys Direct To Key Photo Sensor +0 Message Annunciation M Map -08◊ Traffic FIS-B Terrain Weather Nearest Clock/Timer MSG and Key Flight Plan ENR TO PROC Waypoint Info Flight Plan Utilities System 0 Home MAP FPL INRST--Push D Annunciations To/From Indication GARMIN Current Page and From/To Field Knob Shortcuts and CDI Figure 2 - GPS 175 Control and Display Layout 40 -08 FIS-B Map Traffic Terrain Weather Nearest COM 122.80 Flight Plan PROC Waypoint Info Utilities ENR Home 126.65 System MAP ITEKRINRST Flight Plan Figure 3 – GNC 355 Display Layout - G 190-02207-A3 Rev. 3 Page 2 AFMS, Garmin GPS/GNC/GNX System FAA APPROVED SD Card Slot Home/Power Button Large and Small Knobs The GNX 375 transponder transmits ADS-B Out data on 1090 extended squitter (1090 MHz). It integrates data from internal and external sources to transmit the following data per 14 CFR 91.227: • • GPS Position, Altitude, and Position Integrity Ground Track and/or Heading, Ground Speed, and Velocity Integrity Air Ground Status • Flight ID, Call Sign, ICAO Registration Number • Capability and Status Information • Transponder Squawk Codes between 0000-7777. • • Emergency Status IDENT - initiates SPI (special position identification) pulse for 18 seconds The transponder also receives ADS-B In data on 1090 MHz, including ADS-B and ADS-R Data. ADS-B is data directly from another transmitting aircraft, and the ADS-R data which is rebroadcasted ADS-B data from a ground station. The transponder also includes ADS-B In data on UAT (978 MHz). UAT In data includes ADS-B, ADS-R, TIS-B, and FIS-B data. TIS-B Data is a broadcast of secondary surveillance radar (SSR) derived traffic information from ground stations, and FIS-B data is broadcast of aviation data from a ground station. FIS- B data includes the following products: • Graphical and textual weather products о NEXRAD о PIREPS G AIRMETS ○ METARS ○ TAFS о Winds Aloft 0 Lightning о Icing о Turbulence о Center Weather Advisories • Aviation Data о TFRs 0 NOTAMS The transponder provides ADS-B traffic information and alerting to the pilot. The AFMS, Garmin GPS/GNC/GNX System FAA APPROVED 190-02207-A3 Rev. 3 Page 3 alerting includes aural and visual traffic alerting information on the display, as well as on interfaced displays where supported. 190-02207-A3 Rev. 3 Page 4 AFMS, Garmin GPS/GNC/GNX System FAA APPROVED 1.2 System Capabilities This Flight Manual Supplement documents the installed capabilities of the GPS 175/GNC 355/GNX 375 specific to the aircraft for which this manual is created. NOTE In sections which contain a square checkbox (□) the installer will have placed an "X" in the boxes next to the capabilities applicable to the installation. The GPS 175/GNC 355/GNX 375 system and associated navigation interface in this aircraft have the following capabilities, in addition to the core multifunction display capability: ✓ Primary GPS Navigation (Enroute) and Approach Capability (LP/LNAV) – See below - Primary GPS Approach Capability with Vertical Guidance (LNAV/VNAV, LPV) - See below ✓ Built in ADS-B In/Out Transponder (GNX 375) 1.3 GNSS (GPS/SBAS) Navigation system Equipment approvals The Garmin GPS 175/GNC 355/GNX 375 navigator installed in this aircraft is a TSO-C145c Class 3 approved GPS navigator that complies with AC 20-138D. The Garmin GPS 175/GNC 355/GNX 375 system as installed in this aircraft is approved for navigation using GPS and GPS/SBAS (within the coverage of a Satellite Based Augmentation System complying with ICAO Annex 10) for IFR en route, terminal area, non-precision approach, and approach procedures with vertical guidance operations. The Garmin GPS 175/GNC 355/GNX 375 system as installed in this airplane complies with the equipment, performance, and functional requirements to conduct RNAV operations in accordance with the following table. This table is accurate at the time it was published. However, changes to operational rules, FAA advisory circulars, flight plan formats, etc., are possible. The pilot is responsible to ensure compliance with current operational requirements. AFMS, Garmin GPS/GNC/GNX System 190-02207-A3 Rev. 3 FAA APPROVED Page 5 Navigation Spec. Operational Requirements/ Authorization ICAO Flight Plan Code Reference Item Item Notes Documents 10a 18 Code PBN/ RNAV 10 FAA AC R Α1 20-138D CHG 2, RNP 10 Oceanic and Remote Areas of Operation (Class II Navigation) GNSS FDE availability must be verified prior to flight. Maximum predicted FDE unavailability is 34 FAA AC 90-105A, FAA AC minutes.' Two GNSS 91-70B, systems required EASA to be operational, AMC (one GNSS system for those routes 20-12 requiring only one long range navigation system). No time limit using GNSS as the primary navigation sensor. Part 91, Part 91 subpart K, 121, 125, and 135 operators require operational approval. The GPS equipment as installed requires a second GNSS system for Class II navigation in oceanic and remote airspace. When installed with a second GNSS system, the GPS 175/GNC 355/GNX 375 equipment complies with the requirements for GPS primary means of Class II navigation in oceanic and remote airspace, when used in conjunction with an FDE prediction tool that satisfies the guidance of FAA AC 20-138D and AC 90-105A (or later revision).' Additional equipment may be required to obtain operational approval to utilize RNP-10 performance. B-RNAV/ RNAV 5 (Europe) This does not FAA AC R B2 constitute an 90-96A operational CHG 1, approval. EASA AMC 20- 4A RNP 4 Oceanic and Remote Areas of Operation (Class II Navigation) GNSS FDE availability must be verified prior to flight. Maximum predicted FDE unavailability is 25 minutes.¹ Two operational long-range nav systems required, (or one navigation system and one GNSS sensor for those routes requiring only one 190-02207-A3 Rev. 3 Page 6 FAA AC R L1 20-138D CHG 2, FAA AC 90-105A, FAA AC 91-70B The GPS equipment as installed requires a second GNSS system for Class II navigation in oceanic and remote airspace. Additional equipment may be required to obtain operational approval to utilize RNP-4 performance. AFMS, Garmin GPS/GNC/GNX System FAA APPROVED Operational Requirements/ ICAO Flight Plan Code Navigation Spec. Reference Authorization Documents Item 10a Item Notes 18 Code PBN/ long-range navigation sensor). No time limit using GNSS as the primary navigation sensor. Part 91, Part 91 subpart K, 121, 125, and 135 operators require operational approval. RNAV 2 The GNSS RNAV FAA AC R C2 system is installed 20-138D Includes RNAV Q and T routes. and meets the CHG 2, performance and FAA AC functional 90-100A requirements of CHG 2 AC 90-100A. In accordance with AC 90-100A, CHG 2, Part 91 operators (except subpart K) following the aircraft and training guidance in AC 90-100A are authorized to fly RNAV 2 procedures. Part 91 subpart K, 121, 125, 129, and 135 operators require operational approval. AFMS, Garmin GPS/GNC/GNX System FAA APPROVED 190-02207-A3 Rev. 3 Page 7 Navigation Spec. Operational Requirements/ Authorization ICAO Flight Plan Code Reference Item Item Notes Documents 10a 18 Code PBN/ RNAVI The GNSS RNAV system is installed FAA AC R D2 Includes RNAV terminal 20-138D and meets the CHG 2, performance and FAA AC functional 90-100A departure, arrival procedures, and approach procedures up to the Final Approach Fix. CHG 2 requirements of AC 90-100A. 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 1 procedures. Part 91 subpart K, 121, 125, 129, and 135 operators require operational approval. P-RNAV (Europe) This does not FAA AC R D2 constitute an 90-96A operational CHG 1, approval. JAA TGL 10 Rev 1 ICAO flight plan code for P-RNAV no longer exists. P-RNAV utilizes RNAV 1 flight plan codes. 190-02207-A3 Rev. 3 Page 8 AFMS, Garmin GPS/GNC/GNX System FAA APPROVED } Navigation Spec. Operational Requirements/ Authorization ICAO Flight Plan Code Reference Item Item Notes Documents 10a 18 Code PBN/ RNP 1 When flying a FAA AC 02 Includes RNP terminal RNP procedure 20-138D containing an RF CHG 2, leg, the AFCS must be FAA AC 90-105A operational. At a minimum, the flight director must be displayed and utilized when conducting procedures containing radius- to-fix (RF) legs. In accordance with AC 90-105A, Part 91 operators (except subpart K), following the aircraft and training guidance in AC 90-105A are authorized to fly RNP 1 procedures. Part 91 subpart K, 121, 125, 129, and 135 operators require operational approval. departure and arrival procedures, including procedures with radius-to- fix (RF) legs. Also includes approach procedures to the Final Approach Fix. AC 90-105A states that procedures with RF legs must be flown using either a flight director or coupled to the autopilot. Garmin has demonstrated acceptable crew workload and Flight Technical Error for hand flown procedures with RF legs when the installation complies with limitation set forth in Section 2.11 of this document. It is recommended to couple the autopilot for RF procedures, if available, but it is not required to do so. See section 4.5 of this manual to determine if this capability is supported in this installation. AFMS, Garmin GPS/GNC/GNX System FAA APPROVED 190-02207-A3 Rev. 3 Page 9 Navigation Spec. Operational Requirements/ Authorization ICAO Flight Plan Code Reference Item Item Notes Documents 10a 18 Code PBN/ RNP-2 GNSS FDE FAA AC R TBD (Oceanic / availability must 20-138D Remote) be verified prior to CHG2, flight. Maximum FAA AC predicted FDE unavailability is 5 minutes.' Two operational long-range nav systems required, (or one navigation system and one GNSS sensor for those routes requiring only one long-range navigation sensor). No time limit using GNSS as the primary navigation sensor. Part 91, Part 91 subpart K, 121, 125, and 135 operators require operational approval. 90-105A FAA AC 91-70B The GPS equipment as installed requires a second GNSS system for Class II navigation in oceanic and remote airspace. Additional equipment may be required to obtain operational approval to utilize RNP-2 performance. Item 18 PBN flight plan code is still to-be- determined at time of publication of this AFMS. RNP-2 (Domestic/ Offshore In accordance with FAA AC R TBD AC 90-105A, Part 20-138D 91 operators CHG 2, En route) (except subpart K) FAA AC following the 90-105 A aircraft and training guidance in AC 90-105A are authorized to fly RNP-2 domestic and offshore routes. Part 91 subpart K, 121, 125, 129, and 135 operators require operational approval. FAA AC 91-70B Includes RNP-2 domestic and offshore routes. Item 18 PBN flight plan code is still to-be- determined at time of publication of this AFMS. 190-02207-A3 Rev. 3 Page 10 AFMS, Garmin GPS/GNC/GNX System FAA APPROVED ) Navigation Operational Requirements/ Authorization ICAO Flight Plan Code Reference Item Item Notes Spec. Documents 10a 18 Code PBN/ RNP When flying a FAA AC S1 APCH LNAV RNP procedure with a radius-to- 20-138D CHG 2, minima fix (RF) leg, the AFCS must be EASA operational. At a minimum, the must be displayed and utilized when conducting FAA AC 90-105A, flight director procedures containing RF legs. In accordance with AC 90-105A, Part 91 operators (except subpart K), following the aircraft and training guidance in AC 90-105A are authorized to fly RNP APCH LNAV minima procedures. Part 91 subpart K, 121, 125, 129, and 135 operators require operational approval. AMC 20- 27A Includes non-precision approaches based on conventional navigation aids with "or GPS" in the title and area navigation approaches titled "GPS", "RNAV-(GPS)", and "RNAV (GNSS)". This includes procedures with radius-to-fix (RF) legs. Garmin has demonstrated acceptable crew workload and Flight Technical Error for hand flown procedures with RF legs when the installation complies with limitation set forth in Section 2.11 of this document. It is recommended to couple the autopilot for RF procedures, if available, but it is not required to do so. See section 4.5 of this manual to determine if this capability is supported in this installation. AFMS, Garmin GPS/GNC/GNX System FAA APPROVED 190-02207-A3 Rev. 3 Page 11