DEPENDENT POSITION DETERMINING

Transcription

1 DEPENDENT POSITION DETERMINING 1. DESCRIPTION This section covers that portion of the system which provides information to determine position from sources which are mainly dependent on ground installations. This includes the GPS Navigator transceivers, GPS / WAAS GPS antennas, transponder, course deviation indicator (CDI), VOR/LOC antenna, HSI components, XM Weather system, Iridium Weather system, Automatic Direction Finder (ADF), and Distance Measuring Equipment (DME) receiver and antenna. A. GPS Navigator Transceivers Two VHF communications (COM) transceivers and integrated controls are mounted in dual Garmin GNS 430(W) units or Garmin GNS 430(W)/GNC 420(W) units to provide VHF communication. The transceivers receive all narrow- and wide-band VHF communication transmissions transmitted within range of the selected frequency. The antennas pick up the signals and route the communication signals to the transceivers, which digitize the audible communication signal. The digitized audio is then routed to the audio control unit for distribution to the speakers or headphones. The Garmin GNC 420 is an IFR certified VHF communications transceiver and GPS sensor. The transceiver incorporates a GPS sensor and includes two removable data cards, one with a Jeppesen data base, and the second being a custom data card. The Garmin GNC 420W is an IFR certified, WAAS capable VHF communications transceiver and GPS sensor. The transceiver incorporates a GPS sensor and includes two removable data cards, one with a Jeppesen data base, and the second being a custom data card. WAAS guidance functionality is available to provide additional instrument approach options. The Garmin GNS 430 is an IFR certified VHF communications transceiver and Navigation Management System (NMS). The NMS includes GPS sensor, VOR/Localizer and Glideslope receivers. The GNS 430(W) includes two removable data cards, one with a Jeppesen data base, and the second being a custom data card. The Garmin GNS 430W is an IFR certified, WAAS capable VHF communications transceiver and Navigation Management System (NMS). The NMS includes GPS sensor, VOR/Localizer and Glideslope receivers. The GNS 430(W) includes two removable data cards, one with a Jeppesen data base, and the second being a custom data card. WAAS guidance functionality is available to provide additional instrument approach options. Serials thru before SB 2X-34-06: GPS signals are received by an antenna mounted inside the fuselage under the forward headliner and by an antenna mounted inside the fuselage under the instrument console. Serials thru after SB 2X-34-06, thru , thru : GPS signals are received by antennas mounted inside the fuselage under the instrument console. Serials thru after SB 2X-34-23, thru , thru after SB 2X-34-24, 2560, 2578 & subs, 22T-0001 & subs: WAAS GPS signals are received by antennas mounted externally to top of fuselage. Serials w/ GNS 430(W)/GNC 420(W) units: For upper GNS 430(W) designated as COM1, 28 VDC is supplied through the 5-amp GPS1 and 7.5-amp COM1 circuit breakers on the Avionics Essential Bus. For lower GNC 420(W) designated as COM2, 28 VDC is supplied through the 5-amp GPS2 and 7.5- amp COM2 circuit breakers on the Avionics Non-Essential Bus. Serials w/ dual GNS 430(W) units: For upper GNS 430(W) designated as COM1, 28 VDC is supplied through the 5-amp GPS1 and 7.5-amp COM1 circuit breakers on the Avionics Essential Bus. For lower GNS 430(W) designated as COM2, 28 VDC is supplied through the 5-amp GPS2 and 7.5-amp COM2 circuit breakers on the Avionics Essential Bus. All Page 1 01 Jan 2012

2 For additional information on the GPS navigator transceivers, see the Garmin 400 Series Installation Manual. (Refer to 05-10) B. Transponder Serials w/o Perspective Avionics: The Garmin GTX 327 (Serials w/o Mode S) or Garmin GTX 330 (Serials w/ Mode S) transponder is mounted in the center console. The transponder receives interrogations from a ground-based secondary radar transmitter and transmits the airplane s identification to the Air Traffic Control Center via Mode A transmissions and altitude information via Mode C. In addition, the GTX 330 transponder and Becker Mode S also send a unique aircraft address via Mode S to enhance the tracking capabilities of ATC and other Mode S transponderequipped aircraft. 28 VDC for receiver, transmitter, and altitude encoder operation is supplied through the 2-amp ENCODER/XPONDER circuit breaker on the Avionics Non-Essential Bus. For additional information on the Garmin transponders, see the GTX 327 Transponder Installation and Operation Manual and the GTX 330 Pilot s Guide. (Refer to 05-10) Serials w/ Perspective Avionics: The Garmin GTX 32 or GTX 33 transponder is located behind the aft cabin bulkhead in the empennage avionics compartment. The GTX 32 transponder provides Modes A and C interrogation/reply capabilities. The GTX 33 Mode S solid-state transponder provides Modes A, C, and S interrogation/reply capabilities. The transponder communicates with the primary Integrated Avionics Unit and is controlled via the PFD or Flight Management System Keyboard. 28 VDC for transponder operation is supplied through the 2-amp XPO- NDER circuit breaker on the Avionics Bus. Refer to the Perspective Integrated Avionics System Pilot s Guide for a complete description of the system, its operating modes, and additional detailed operating procedures. (Refer to 05-10) The GTX 32 and GTX 33 transponders are integral to the Perspective Integrated Avionics system. For an overview of the Perspective Avionics system, refer to Chapter 42, Integrated Modular Avionics. (Refer to 42-00) C. Course Deviation Indicator (CDI) Serials thru w/o PFD: The Garmin GI-102(A) and GI-106(A) are panel-mounted Course Deviation Indicators (CDI's) with rectilinear meter movements and integral GPS, NAV, and VLOC mode annunciators. Both units provide a VOR/LOC/GPS needle, TO/FROM indicator, NAV warning flag, and an integral resolver for OBS feedback. The GI-106A also provides a GS needle and flag. 28 VDC for lighting is supplied through the 2-amp INST LIGHTS circuit breaker on Main Bus 1. D. Horizontal Situation Indicator (HSI/EHSI) Serials thru w/o PFD: The NSD-1000 HSI, located directly below the attitude indicator, has an electrically driven gyro slaved to a flux detector mounted in the right wing and an amplifier mounted under the copilot floor for continuous compass card correction. The HSI mode switch is mounted directly beneath the HSI to allow the pilot to select either SLAVE or FREE GYRO mode. The HSI displays a stable indication of the airplane heading to the pilot. 28 VDC for the redundant power circuits is supplied through the 5-amp HSI#1 circuit breaker on the Essential Bus and 5-amp HSI#2 circuit breaker on Main Bus 2. Serials thru w/o PFD: The SN3308 EHSI is located directly below the attitude indicator and performs the functions of a standard HSI combined with a two-pointer RMI. The instrument also displays a moving map, marker beacon, WX500 stormscope data, and GPS data. The EHSI system includes a remote gyro located under the RH passenger seat which is slaved to a flux detector mounted in the right wing. 28 VDC for the redundant power circuits is supplied through the 5-amp HSI#1 circuit breaker on the Essential Bus and 5-amp HSI#2 circuit breaker on Main Bus 2. Page 2 01 Jan 2012 All

3 E. XM Weather System - Serials w/o Perspective Avionics Serials thru : The XM Weather system consists of the XM Weather Receiver mounted behind the RH bolster panel, XM Weather antenna (standalone, XM/COM1, or XM/WAAS) mounted externally to top of fuselage, and system wire harness. Serials & subs w/o Perspective Avionics: The XM Weather system consists of the XM Weather Receiver mounted in the RH aft fuselage, XM Weather antenna (standalone, XM/COM1, or XM/WAAS) mounted externally to top of fuselage, and system wire harness. The XMD076A Data Link Satellite Receiver receives and transmits real-time weather information to the MFD and PFD. The receiver also provides digital XM audio entertainment to the cabin audio system controlled by the XMC050 Remote Control. The XM Weather system utilizes continuous satellite broadcasts to display real time, location-specific graphical weather information on the MFD. To enhance the situational awareness to the pilot, the MFD will display NEXRAD Radar, METARs, SIGMETs, AIRMETs, TFRs, and Lightning Strikes from the National Lightning Detection Network. XM Radio is optionally integrated into the XM Weather system. (Refer to 23-30) The XM Weather system is powered by 28 VDC through the 3-amp WEATHER/STORMSCOPE circuit breaker on the Avionics Non-Essential Bus. Refer to the manufacturer s approved Instructions For Continued Airworthiness. F. XM Weather System - Serials w/ Perspective Avionics The XM Weather system consists of the XM Weather Receiver mounted in the empennage avionics compartment, XM Weather/WAAS Combo Antenna mounted externally to top of fuselage, and system wire harness. The GDL 69/69A Data Link Satellite Receiver receives and transmits real-time weather information to the MFD and PFD. Serials w/o Flight Stream 210: If GDL 69A option is installed, this unit also provides digital XM audio entertainment to the cabin audio system via the audio panel. It is controlled by the MFD or the GRT 10 XM Remote Transceiver with GRC 10 Remote Control. Serials w/ Flight Stream 210: If GDL 69A option is installed, this unit also provides digital XM audio entertainment to the cabin audio system via the audio panel. It is controlled by MFD or the Flight Stream 210 Bluetooth Transceiver with compatible mobile devices. For maintenance practices related to the Flight Stream 210, see the Passenger Address and Entertainment section of Communications. (Refer to 23-30) The XM Weather system utilizes continuous satellite broadcasts to display real time, location-specific graphical weather information on the MFD. To enhance the situational awareness to the pilot, the MFD will display NEXRAD Radar, METARs, SIGMETs, AIRMETs, TFRs, and Lightning Strikes from the National Lightning Detection Network. XM Radio is optionally integrated into the XM Weather system. (Refer to 23-30) Serials thru , 22T-0001 thru 22T-0267: The XM Weather system is powered by 28 VDC through the 3-amp WEATHER circuit breaker on the Avionics Non-Essential Bus. Serials & subs, 22T-0268 & subs: The XM Weather system is powered by 28 VDC through the 5-amp WEATHER/DATALINK circuit breaker on the Avionics Non-Essential Bus. The GDL 69/69A Data Link Satellite Receiver is integral to the Perspective Integrated Avionics system. For an overview of the Perspective Avionics system, refer to Chapter 42, Integrated Modular Avionics. (Refer to 42-00) Note: All Serials & subs, 22T-0268 & subs: The XM Weather System is available as an optional installation with or without the Iridium Weather System. Page 3 01 Jan 2016

4 G. Iridium Weather System - Serials & subs, 22T-0268 & subs w/ Perspective Avionics The Iridium Weather system consists of the GSR 56 Iridium Transceiver installed immediately behind the aft cabin bulkhead, the GPS/Iridium Combo Antenna mounted externally to top of fuselage, and system wire harness. The GSR 56 Transceiver receives and transmits real-time weather information to the MFD and PFD. If the Iridium subscription-based voice and data service is active, satellite telephone/voice communications and text messaging (SMS) are provided. The dialing interface is provided through the MFD and incoming call messages are prioritized with other aural messages. The Iridium Weather system utilizes continuous satellite broadcasts to display real time, worldwide graphical weather information on the MFD. To enhance the situational awareness to the pilot, the MFD will display NEXRAD Radar, METARs, Winds Aloft, Temps Aloft, NOTAMs, SIGMETs, AIRMETs, TFRs, PIREP, and Lightning Strikes from the National Lightning Detection Network. In addition, radar and satellite imagery are available for the United States, Southern Canada and Western Europe. The Iridium Weather system is powered by 28 VDC through the 5-amp WEATHER/DATALINK circuit breaker on the Avionics Non-Essential Bus. The GSR 56 Transceiver is integral to the Perspective Integrated Avionics system. For an overview of the Perspective Avionics system, refer to Chapter 42, Integrated Modular Avionics. (Refer to 42-00) Note: The Iridium Weather System is available as an optional installation with or without the XM Weather System. H. Automatic Direction Finder (ADF) Serials w/ Perspective Avionics: The Honeywell KR 87 Automatic Direction Finder (ADF), located in the center console below the FMS keyboard, is a digitally tuned solid state receiver which provides bearing information to stations in the 200 KHz to 1799 KHz frequency band. The ADF also provides audio reception to enable the pilot to identify stations and listen to transcribed weather broadcasts or commercial radio stations in the AM broadcast band. The ADF antenna is located on the fuselage belly. 28 VDC for ADF operation is supplied through the 3-amp DME / ADF circuit breaker on the Avionics Bus. Refer to the Honeywell ADF System Pilot s Guide for a detailed discussion of the system. (Refer to 05-10) The KR 87 Automatic Direction Finder is integral to the Perspective Integrated Avionics system. For an overview of the Perspective Avionics system, refer to Chapter 42, Integrated Modular Avionics. (Refer to 42-00) I. Distance Measuring Equipment (DME) Serials w/ Perspective Avionics: The Honeywell KN 63 Distance Measuring Equipment (DME) receiver, located under the pilot s seat, determines aircraft distance to a land-based transponder by sending and receiving pulse pairs - two pulses of fixed duration and separation. The ground stations are typically collocated with VORs. The DME antenna is located on the fuselage belly. The KN 63 receiver communicates with the Perspective Avionics system via the secondary Integrated Avionics Unit. 28 VDC for DME System operation is supplied through the 3-amp DME / ADF circuit breaker on the Avionics Bus. Refer to the Honeywell DME Installation Guide for a detailed discussion of the system. (Refer to 05-10) The KN 63 Distance Measuring Equipment (DME) receiver is integral to the Perspective Integrated Avionics system. For an overview of the Perspective Avionics system, refer to Chapter 42, Integrated Modular Avionics. (Refer to 42-00) Page 4 01 Jan 2016 All

5 2. TROUBLESHOOTING Serials w/ Perspective Avionics: Trouble Probable Cause Remedy Transponder not receiving valid data. Software or configuration error. Faulty connector. Faulty transponder. Check PFD Alert Window for GIA1, GIA2, and GTX 32/33 configuration, software, or failed data path error messages. Correct any errors before proceeding. Perform a SET>ACTV configuration reset on GTX Transponder Configuration page for each installed GTX. For GTX 33 transponders, verify aircraft registration is entered in GTX Transponder Configuration page. Check GIA and GTX racks for connector pin faults (push-back or bent) on the RS-232 interconnect lines. Replace transponder. Serials & subs, 22T-0268 & subs w/ Iridium Weather System: Trouble Probable Cause Remedy No communication with GSR 56. Disconnected or faulty wiring. Check power wiring and pin out. Incorrect settings. Verify correct communication port setting on display/control device. No or low-quality signal. Antenna interference. Ensure the Iridium antenna has an unobstructed view of satellite constellation. Disconnected or faulty wiring. Compromised ground plane. Check the antenna cable and connectors. Verify antenna ground plane is adequate. No audio output. Disconnected or faulty wiring. Check wiring from GSR 56 to audio panel. No subscription with Garmin Iridium Services. Verify subscription with Garmin Iridium Services. All Page 5 01 Jan 2012

6 Trouble Probable Cause Remedy Unable to make a phone call. No subscription with Garmin Iridium Services. No call signal. Disconnected or faulty wiring. Verify subscription with Garmin Iridium Services. Verify signal quality is adequate. Verify communication between GSR 56 and the display/control device.. Page 6 01 Jan 2012 All

7 3. MAINTENANCE PRACTICES A. Garmin 400 Series GPS Navigator - Serials w/o Perspective Avionics (See Figure 1) (1) Removal - Garmin 400 Series GPS Navigator (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. (c) Insert 3/32-inch hex wrench into front panel bolt hole and engage hex bolt. (d) Rotate locking screw counter-clockwise to loosen locking cam. Cam will move the transceiver unit out 0.25 inch (0.64 cm) and disengage from the electrical connectors. CAUTION: For dual GNS or GNS/GNC configurations, note positions for GPS1 and GPS2 when originally installed transceivers will be replaced. (e) Pull transceiver from mounting tray. (2) Installation - Garmin 400 Series GPS Navigator CAUTION: When mounting the transceivers, do not press on display window as damage may result. For dual GNS or GNS/GNC configurations, verify when replacing originally installed transceivers that GPS1 and GPS2 positions are retained. (a) With light to medium pressure, push transceiver into mounting tray to engage electrical connectors. (b) Insert 3/32-inch hex wrench into front panel bolt hole and engage hex bolt. (c) Rotate bolt clockwise to tighten locking cam. (d) Reset ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. (e) If transceiver is a different unit from the originally installed transceiver: 1 Perform Functional Test - Garmin 400 Series GPS Navigator Setup. (Refer to ) 2 Perform Functional Test - Garmin 400 Series GPS Navigator Clock Setup. (Refer to ) 3 Serials w/ Dual GNS: Perform Functional Test - Dual Garmin 400 Series GPS Navigator Crossfill Setup. (Refer to ) 4 Perform Operational Test - Garmin 400 Series GPS Navigator VHF COM Check. (Refer to ) (f) If transceiver is the same unit as the originally installed transceiver: 1 Serials w/ Dual GNS: Perform Functional Test - Dual Garmin 400 Series GPS Navigator Crossfill Setup. (Refer to ) 2 Perform Operational Test - Garmin 400 Series GPS Navigator VHF COM Check. (Refer to ) (3) Operational Test - Garmin 400 Series GPS Navigator VHF COM Check A flight test is recommended after the installation to verify satisfactory performance. To check the communications transceiver: (a) Maintain an appropriate altitude and contact a ground station facility at a range of at least 50 nautical miles. (b) Contact a close ground station. (c) Press the squelch disable button to defeat the automatic squelch feature and listen for any unusual electrical noise which would increase the squelch threshold. (d) If possible, confirm communications capability on both high and low ends of the VHF COM band. Serials w/o Perspective Avionics Page 7 01 Jan 2012

8 (4) Functional Test - Garmin 400 Series GPS Navigator Setup (a) Connect 28 ±1 VDC external power to external power receptacle. (b) Set BAT 1, BAT 2, and AVIONICS switches to ON positions. (c) Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers. (d) On transceiver(s), rotate [C] knobs for COM power counter-clockwise to OFF positions. Note: Right data card slot contains blank card. (e) (f) (g) (h) (i) (j) (k) On transceiver(s), verify data cards are installed for GPS1 and, if applicable, GPS2 in left data card slot. While holding [ENT], rotate [C] knobs for COM power clockwise to ON positions. Release [ENT] after display is on. After power-up, the Self Test pages will display, followed by the Database page. On dual GNS or GNS/GNC units, verify GPS1 and GPS2 have the same MAIN SOFT- WARE VERSION, GPS SOFTWARE VERSION, and CYCLE numbers displayed. On the Database page, press [ENT]. On the Instrument Panel Self-Test page, press [ENT]. Navigate subsequent pages by use of transceiver controls. Note: Only the GPS indicated by the NAV selection on the PFD will be displayed. Not all parameters are editable. To turn on cursor, press inner dial of [CRSR] knob. To move between data fields, rotate outer dial of [CRSR] knob. To change a field that cursor is on, rotate inner dial of [CRSR] knob. To accept entry of current selection, press [ENT]. To turn off cursor before switching pages, press inner dial of [CRSR] knob. To switch between pages, rotate inner dial of [CRSR] knob. 1 Set parameters for the Main ARINC 429 Config page for GPS1. SPEED DATA IN 1 - Serials w/ Century HSI Low Off IN 1 - Serials w/ Sandel EHSI, thru w/ PFD, & subs IN 2 - Serials w/o SkyWatch and w/ GNC 420W or GNS 430W IN 2 - Serials w/ SkyWatch and w/o GNC 420W or GNS 430W IN 2 - Serials w/ SkyWatch and w/ GNC 420W or GNS 430W Low Low Low High Sandel EHSI Off Traffic Advisory Traffic Advisory OUT Low GAMA 429 grph w/int SDI LNAV 1 Page 8 01 Jan 2012 VNAV - Serials w/ PFD S/W Rel or lower Disable Labels Serials w/o Perspective Avionics

9 VNAV - Serials w/ PFD S/W Rel. 7.0 or higher Enable Labels 2 Set parameters for the Main ARINC 429 Config page for GPS2. SPEED DATA IN 1 - Serials thru w/o PFD Low Off IN 1 - Serials thru w/ PFD, & subs w/o Perspective Avionics IN 2 - Serials w/o SkyWatch and w/ GNC 420W or GNS 430W IN 2 - Serials w/ SkyWatch and w/o GNC 420W or GNS 430W IN 2 - Serials w/ SkyWatch and w/ GNC 420W or GNS 430W Low Low Low High Sandel EHSI Off Traffic Advisory Traffic Advisory OUT Low GAMA 429 grph w/int SDI LNAV 2 VNAV - Serials w/ PFD S/W Rel or lower Disable Labels VNAV - Serials w/ PFD S/W Rel. 7.0 or higher Enable Labels 3 Set parameters for the Main RS232 Config page for GPS1 and GPS2. INPUT OUTPUT CHAN 1 Icarus-alt Aviation CHAN 2 - Serials w/o TAWS Off Off CHAN 2 - Serials w/ TAWS Off HW EGPWS CHAN 3 Crossfill Crossfill CHAN 4 - Serials w/o Stormscope Off Off CHAN 4 - Serials w/ Stormscope and GNC/GNS Main S/W Rel. 2.0 or lower CHAN 4 - Serials w/ Stormscope and GNC/GNS Main S/W Rel. 3.0 or higher FUEL TYPE Off WX 500 AV gas Off Off 4 The Main Inputs 1 page is not used. 5 The Main Inputs 2 page is not used. Serials w/o Perspective Avionics Page 9 01 Jan 2012

10 6 Set parameters for the Instrument Panel Self-Test page. LCDI LFLG TO/FRM Half Left Out of View To RMI 135 DTK 150 CAP - w/ 81 gallon wing CAP - w/ 92 gallon wing FOB FF 81gl 92gl 0gl 0.0gl 7 For the Main Lighting page, cover photocell and observe that display slowly dims and lighting values decrease. Note: Main Lighting page values may differ from those below due to your unique lighting environment. 8 Set parameters for the Main Lighting page. DISPLAY KEY LIGHTING SOURCE PHOTO 28VDC RESP TIME/MIN SLOPE/OFFSET Set parameters for the Date/Time Setup page. 10 Set parameters for the Main Discrete Inputs page. GRAY CODE DECODED ALTITUDE RMT CDI RMT OBS ft unchecked unchecked 11 The Main Discrete Outputs page is not used. 12 Serials w/ Century HSI: Set parameters for the Main CDI/ OBS Config page. CDI NAV FLAG TO-FROM Page Jan 2012 LAT Center Hidden Hidden Serials w/o Perspective Avionics

11 VERT Center Hidden SELECTED COURSE 148 Calibrate to 150? CDI OBI SOURCE VERT GPS Track CDI Flag Center 13 Serials w/ Century HSI: Toggle settings to verify outputs display correctly for the corresponding indicators. CDI NAV FLAG TO-FROM LAT Max Left Full Left Center Full Right Max Right Hidden In View From Hidden To VERT Max Up Full Up Center Full Down Max Down Hidden In View 14 Serials w/ Century HSI: Set OBS dial on HSI to Serials w/ Century HSI: Select Calibrate To 150?, then press [ENT]. 16 Serials w/ Century HSI: Set OBS to other headings around dial to verify correct readings. 17 Serials w/ Sandel EHSI, thru w/ PFD, & subs: The Main CDI / OBS Config page is not used. Note: Set SPACING only. Do not adjust any other settings. 18 Set parameters for the COM Setup page for COM1 and COM2. FREQ SPACING 25.0 KHz S S SIDE 07 MIC The VOR Discrete Inputs page is not used. Note: Set DME CGNL MODE only. Do not adjust any other settings. Serials w/o Perspective Avionics Page Jan 2012

12 20 Set parameters for the VOR/LOC/GS CDI page. CDI FLAG S-FLG TO-FR LAT Center Hide Hide From VERT Center Hide Hide SELECTED COURSE No input DME CGNL MODE Parallel 2x5 21 Set parameters for the VOR / LOC / GS ARINC 429 Config page for GPS1. RX TX SPEED Low Low SDI VOR / ILS 1 DME MODE Directed freq 1 22 Set parameters for the VOR / LOC / GS ARINC 429 Config page for GPS2. RX TX SPEED Low Low SDI VOR / ILS 2 DME MODE Directed freq 2 23 Serials w/ GNC 420W or GNS 430W: Set parameters for the GPS Vertical Offset page. GPS ANTENNA HEIGHT ABV GND 6.0ft 24 Serials w/ GNC 420 or GNS 430 and GNC/GNS Main S/W Rel or higher: On the Main System Config page, set parameters for GPS1 and GPS2. CONFIGURE TERRAIN TYPE TEST CARD HW CONFIG Terrain Terrain Untested Terrain Page Jan 2012 (l) (m) 25 Serials w/ GNC 420 or GNS 430 and GNC/GNS Main S/W Rel or higher: Highlight the TEST CARD field, then press [ENT]. Verify the TEST CARD field indicates Pass. When setup is completed, on transceiver(s), rotate [C] knobs for COM power counterclockwise to OFF positions. Allow display to blank completely. Serials w/o Perspective Avionics

13 (n) (o) (p) On transceiver(s), rotate [C] knobs for COM power clockwise to ON positions. The Self-Test pages will be displayed followed by the Database page. On the Database page, press [ENT]. Set parameters on the Instrument Panel Self-Test page. LCDI LFLG VCDI VFLG CAP - w/ 81 gallon wing CAP - w/ 92 gallon wing FOB FF TO/FRM Half Left Out of View Half Up Out of View 81gl 92gl 0gl 0.0gl To RMI 135 OBS 150 ANNUN On DTK 150 (q) Verify parameters for self-test data output on the displays indicated. Display Parameter Self-Test VOR and HSI/PFD Course Deviation ½ scale left deviation, TO flag, NAV flag pulled VOR and HSI - Serials thru w/o PFD Glidescope/ Vertical Deviation ½ scale up deviation, GS flag pulled MFD and EHSI/PFD Active Waypoint (WPT) "GARMN" MFD and EHSI/PFD Distance To Go (DIS) 10.0 nautical miles MFD and EHSI/PFD Desired Track (DTK) 150 MFD and EHSI/PFD Bearing to Wpt (BRG) 135 MFD and EHSI/PFD Groundspeed (GS) 150 knots MFD and EHSI - Serials thru w/o PFD Track (TRK) 135 MFD and EHSI/PFD Time to Go (ETE) 4 minutes Serials w/o Perspective Avionics Page Jan 2012

14 (r) (s) On transceiver(s), press [ENT]. Upon approval of the Database page, the Satellite Status page will be displayed. Serials w/ GNC 420W or GNS 430W: Verify continuous GPS reception during COM transmissions for GPS1 and GPS2. 1 Using large outer RH knob, select NAV group. 2 Rotate small RH knob to select Satellite Status page. 3 On audio panel, select COM1. 4 Set COM1 to each of the following frequencies and verify that the reception of GPS1 and GPS2 is not lost during a COM transmission. Page Jan On audio panel, select COM2. 6 Set COM2 to each of the following frequencies and verify that the reception of GPS1 and GPS2 is not lost during a COM transmission. (t) Serials thru w/ PFD, & subs w/o Perspective Avionics: Verify coupling between PFD and COM/NAVs: 1 On PFD, press [Nav1] to select "GPS1". 2 Verify Nav1 selection on PFD matches CDI setting of "GPS" on GNS 430(W). 3 On PFD, press [Nav1] to select "VLOC1". 4 Verify CDI setting on GNS 430(W) changes to "VLOC". 5 On GNS 430(W), press [CDI] to select "GPS". 6 On PFD, verify Nav1 selection changes back to "GPS1". 7 Repeat coupling procedure for the lower GNS 430(W) or GNC 420(W). (u) Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers. (v) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (w) Disconnect 28 ±1 VDC external power from external power receptacle. (5) Functional Test - Garmin 400 Series GPS Navigator Clock Setup (a) Set BAT 1 and AVIONICS switches to ON positions. (b) On GNS unit, rotate [C] knob for COM power clockwise to ON position. (c) After power-up, the Self Test pages will display, followed by the Database page. (d) On the Database page, press [ENT]. (e) On the Instrument Panel Self-Test page, press [ENT]. (f) Rotate outer dial of [CRSR] knob to select the first Aux (Flight Planning) page. (g) Rotate inner dial of [CRSR] knob to select the third Aux (Setup 1) page. (h) Press inner dial of [CRSR] knob to activate cursor. (i) Rotate inner dial of [CRSR] knob to select Date / Time, then press [ENT]. (j) Rotate inner dial of [CRSR] knob to highlight TIME FORMAT. (k) Rotate inner dial of [CRSR] knob to select "Local 24hr", then press [ENT]. (l) Rotate inner dial of [CRSR] knob to highlight TIME OFFSET. (m) MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz MHz Rotate inner dial of [CRSR] knob to select present UTC time, then press [ENT]. Serials w/o Perspective Avionics

15 (n) Rotate [C] knob for COM power counter-clockwise to OFF position. (o) Set BAT 1 and AVIONICS switches to OFF positions. (6) Functional Test - Dual Garmin 400 Series GPS Navigator Crossfill Setup (a) Set BAT 1 and AVIONICS switches to ON positions. (b) On GNS unit, rotate [C] knob for COM power clockwise to ON position. (c) Rotate outer right dial of [CRSR] knob to select the first Aux (Flight Planning) page. (d) Press inner right dial of [CRSR] knob to highlight the cursor. (e) Rotate inner right dial of [CRSR] knob to select "Crossfill", then press [ENT]. (f) Verify that status displayed is READY. (g) Rotate [C] knob for COM power counter-clockwise to OFF position. (h) Set BAT 1 and AVIONICS switches to OFF positions. Serials w/o Perspective Avionics Page Jan 2012

16 INSTRUMENT PANEL (REF) or 2 3 NOTE Insert 3/32 inch hex wrench into front panel bolt hole and engage hex bolt. LEGEND 1. GNC 420 Transceiver 2. GNS 430 Transceiver 3. Captive Screw SR22_MM34_1477D Page Jan 2012 Figure 1 Transceiver Installation - Serials w/o Perspective Avionics Serials w/o Perspective Avionics

17 B. GPS1 / GPS2 Antenna - Serials thru , thru (See Figure 2) (1) Removal - GPS1 / GPS2 Antenna (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. (c) Serials thru : For GPS1, remove cabin headliner. (Refer to 25-10) (d) Serials thru , thru : For GPS1, remove glareshield. (Refer to 25-10) (e) For GPS2, remove glareshield. (Refer to 25-10) (f) Disconnect antenna cable from antenna. (g) Pry antenna from hook and loop fastener securing antenna to installation area. (h) Remove antenna from airplane. (2) Installation - GPS1 / GPS2 Antenna (a) To secure antenna to installation area, firmly press fastener strip on antenna against fastener strip. (b) Connect antenna cable. (c) Reset ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. (d) Serials thru : For GPS1, install cabin headliner. (Refer to 25-10) (e) Serials thru , thru : For GPS1, install glareshield. (Refer to 25-10) (f) For GPS2, install glareshield. (Refer to 25-10) Serials thru , thru Page Jan 2012

18 C. WAAS GPS1 / GPS2 Antenna - Serials , 2578 & subs, 22T-0001 & subs (See Figure ) (1) Removal - WAAS GPS1 / GPS2 Antenna (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. (c) Remove cabin headliner. (Refer to 25-10) (d) Disconnect GPS cable from antenna. (e) Serials w/ XM Weather: Disconnect XM Weather cable from antenna. (f) Serials w/ Iridium Weather: Disconnect Iridium Weather cable from antenna. (g) Remove nuts, washers, and screws securing antenna to fuselage. (h) Remove antenna and gasket from fuselage. (i) Remove remaining sealant from fuselage. (2) Installation - WAAS GPS1 / GPS2 Antenna (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Caulk Sealant (Refer to 51-30) (Refer to 51-30) Weather sealant. (b) Position gasket and antenna to fuselage and insert screws through mounting holes. CAUTION: Note: To prevent damage to rubber gasket at screwhead, turn nuts onto screws during installation. Tighten forward screws prior to tightening aft screws. (c) Install washers and nuts securing antenna to fuselage. Torque nuts to maximum of in-lb ( Nm). (d) Fillet seal antenna perimeter. (Refer to 20-10) (e) Connect GPS cable to antenna. (f) Serials w/ XM Weather: Connect XM Weather cable to antenna. (g) Serials w/ Iridium Weather: Connect Iridium Weather cable to antenna. (h) Install cabin headliner. (Refer to 25-10) (i) Reset ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. Page Jan 2012 Serials , 2578 & subs, 22T-0001 & subs

19 Serials thru after SB 2X Serials thru , thru CABIN CEILING (REF) OR GLARESHIELD (REF) Serials thru before SB 2X NOTE GPS 1 installed on cabin ceiling. GPS 2 installed on glareshield. GPS 1 installed on RH glareshield. GPS 2 installed on LH glareshield. GPS 1 installed on RH outboard glareshield. GPS 2 installed on RH inboard glareshield. SR22_MM34_1476E Figure 2 GPS Antenna Installation - Serials thru , thru (1 of 2) Serials thru , thru Page Jan 2012

20 4 1 7 FUSELAGE (REF) Serials thru after SB 2X w/o XM Weather, Serials thru , thru after SB 2X w/o XM Weather, , & subs, 22T-0001 & subs w/ WAAS GPS1 w/o XM Weather. 7 FUSELAGE (REF) FUSELAGE (REF) Serials thru after SB 2X-34-23, Serials thru , thru after SB 2X-34-24, Serials , thru , 22T-0001 thru 22T-0267 w/ WAAS GPS2. 3 NOTE Optional Iridium Weather system installation. 3 3 Serials & subs, 22T-0268 & subs w/ WAAS GPS LEGEND 1. WAAS GPS 1 Antenna 2. WAAS GPS 2 Antenna 3. Antenna Connector 4. Screw 5. Washer 6. Nut 7. Gasket SR22_MM34_2565C Page Jan 2012 Figure 2 WAAS GPS Antenna Installation - Serials , 2578 & subs, 22T-0001 & subs (2 of 2) Serials , 2578 & subs, 22T-0001 & subs

21 D. COM1 Antenna - Serials thru after SB 2X w/o combo antenna kit, 1793 & subs, 22T-0001 & subs (See Figure 3) (1) Removal - COM1 Antenna (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. (c) Remove cabin headliner. (Refer to 25-10) (d) Disconnect antenna cable from antenna. (e) Remove nuts, washers, and screws securing antenna to fuselage. (f) Remove antenna and gasket from top of fuselage. (g) Remove remaining sealant from fuselage. (2) Installation - COM1 Antenna (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Caulk Sealant (Refer to 51-30) (Refer to 51-30) Weather sealant. (b) Position gasket and antenna on fuselage roof, then insert screws through mounting holes. (c) Install washers and nuts securing antenna to fuselage. (d) Fillet seal antenna perimeter. (Refer to 20-10) (e) Connect antenna cable. (f) Install cabin headliner. (Refer to 25-10) (g) Reset ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. Serials thru after SB 2X w/o combo antenna kit, 1793 & subs, 22T-0001 & subs Page Jan 2012

22 E. COM1 / XM Weather Antenna - Serials thru after SB 2X w/ COM1 / XM antenna kit, thru w/ factory XM Weather (See Figure 3) (1) Removal - COM1 / XM Weather Antenna (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. (c) Remove cabin headliner. (Refer to 25-10) (d) Disconnect XM weather cable from antenna. (e) Disconnect COM1 cable from antenna. (f) Remove nuts, washers, and screws securing antenna to fuselage. (g) Remove antenna and gasket from fuselage. (h) Remove remaining sealant from fuselage. (2) Installation - COM1 / XM Weather Antenna (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Caulk Sealant (Refer to 51-30) (Refer to 51-30) Weather sealant. (b) Position gasket and antenna to fuselage and insert screws through mounting holes. (c) Install washers and nuts securing antenna to fuselage. (d) Fillet seal antenna perimeter. (Refer to 20-10) (e) Connect XM Weather cable to antenna. (f) Connect COM1 cable to antenna. (g) Install cabin headliner. (Refer to 25-10) (h) Reset ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. Page Jan 2012 Serials thru after SB 2X w/ COM1 / XM antenna kit, thru w/ factory XM Weather

23 F. COM2 Antenna (See Figure 3) (1) Removal - COM2 Antenna (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. (c) Remove baggage compartment floor access panel. (Refer to 06-00) (d) Disconnect antenna cable from antenna. (e) Remove nuts and washers securing antenna to fuselage. (f) Remove antenna and gasket from belly of fuselage. (g) Peel off remaining sealant from fuselage. (2) Installation - COM2 Antenna (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Caulk Sealant (Refer to 51-30) (Refer to 51-30) Weather sealant. (b) Position gasket and antenna on fuselage belly, then insert screws through mounting holes. (c) Install washers and nuts securing antenna to fuselage. (d) Fillet seal antenna perimeter. (Refer to 20-10) (e) Connect antenna cable. (f) Install baggage compartment floor access panel. (Refer to 06-00) (g) Reset ESSENTIAL and NON-ESSENTIAL AVIONICS circuit breakers. All Page Jan 2012

24 4 7 BAGGAGE COMPARTMENT FLOOR (REF) FUSELAGE (REF) Serials thru before SB 2X w/ COM 1 / XM antenna in kit, Serials thru after SB 2X w/o COM 1 / XM antenna in kit, & subs, 22T-0001 & subs. 5 2 FUSELAGE (REF) Serials thru after SB 2X w/ COM 1 / XM antenna in kit, Serials thru w/ factory XM Weather. 4 LEGEND 1. COM 1 Antenna 2. COM 1 / XM Weather Antenna 3. COM 2 Antenna 4. Antenna Connector 5. Screw 6. Washer 7. Nut 8. Gasket SR22_MM34_2463A Page Jan 2012 Figure 3 COM Antenna Installation All

25 G. Garmin GTX Transponder - Serials w/o Perspective Avionics (See Figure 4) (1) Removal - Garmin GTX Transponder (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull ENCODER/TRANSPONDER circuit breaker. (c) Insert hex wrench into front panel bolt hole and engage hex bolt. (d) Turn locking screw counter-clockwise to loosen locking cam. Locking cam will move the transponder unit out 0.25 inch (0.635 cm) and disengage from the electrical connectors. (e) Pull transponder from mounting tray and remove from airplane. (2) Installation - Garmin GTX Transponder (a) With light to medium pressure, push transponder into mounting tray to engage electrical connectors. (b) Insert hex wrench into front panel bolt hole and engage hex bolt. (c) Turn bolt clockwise to tighten locking cam. (d) Reset ENCODER/TRANSPONDER circuit breaker. (e) If transponder is a different unit from the originally installed transponder: 1 Serials w/ GTX 327 Transponder: Perform Functional Test - Garmin GTX 327 Transponder Setup. (Refer to ) 2 Serials w/ GTX 330 Transponder: Perform Functional Test - Garmin GTX 330 Transponder Setup. (Refer to ) (f) Perform Functional Test - Altitude Encoder Calibration. (Refer to 34-10) (g) Perform Operational Test - Garmin GTX Transponder. (Refer to ) (3) Operational Test - Garmin GTX Transponder (a) Verify transponder operation in accordance with 14 CFR (4) Functional Test - Garmin GTX 327 Transponder Setup (a) Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers. (b) Set BAT 1, BAT 2, and AVIONICS switches to ON positions. (c) On GTX 327, press [OFF] key. (d) Hold down [FUNC] and press [ON]. Set highlighted parameters as follows: To sequence through configuration pages, press [FUNC]. To highlight selectable fields on each page, press [CRSR]. When a field is highlighted, numeric data entry is performed with 0-9 keys, and list selections with 8 or 9 keys. To accept changes, press [CRSR] key. Pressing [FUNC] key moves on to the next configuration page without saving the changes. 1 Set parameters for the Display Mode page. DISPLAY MODE AUTO LEVEL 75 2 Set parameters for the Display Backlight page. BKLT AUTO RSP TIME 4 MIN 08 BKLT SRCE Serials w/o Perspective Avionics PHOTO Page Jan 2012

26 SLOPE 50 OFFSET 50 3 Set parameters for the Key Lighting page. KEY AUTO RSP TIME 4 MIN 08 KEY SRCE 28V SLOPE 50 OFFSET 50 4 Set parameters for the Contrast Configuration page. CONTRAST MODE AUTO 5 Set parameters for the RS-232 Input/Output page. INPUT OUTPUT CHNL 1 OFF ICARUS ALT CHNL 2 GPS 6 Set parameters for the Operation Configuration page. VS RATE 0500 FLT TMR CLEAR VFR ID 1200 FORMAT FEET 7 Set parameters for the Squat Switch page. SQUAT SWITCH? SENSE AUTO STANDBY? NO LOW ON DELAY TIME 10 8 Set parameters for the Aircraft Type page. AC TYPE <15.5K lb Page Jan Set parameters for the RS-232 INPUT VIEW page. Serials w/o Perspective Avionics

27 Note: With GPS in self-test mode, GSPD should read 150 kts. CH1 OFF +. n/a CH2 GSPD + _ kts 10 Set parameters for the Gray Code Input page. GRAY CODE ########## DECODED ALTITUDE #### (Field Elevation ±300 ft) Note: No external switches are used. 11 Set parameters for the External Switch page. IDENT STANDBY SQUAT unchecked unchecked unchecked 12 Set parameters for the Analog Input page. 14/5V LTG 000 PHOTO 000 LCD TEMP V LTG 000 REPLY 000 UNIT TMP Press [OFF] to exit setup. (e) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (f) Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers. (5) Functional Test - Garmin GTX 330 Transponder Setup (a) Pull STARTER RELAY and FUEL PUMP RELAY circuit breakers. (b) Set BAT 1, BAT 2, and AVIONICS switches in ON positions. (c) On GTX 330, press [OFF]. (d) Hold down [FUNC] and press [ON]. Set highlighted parameters as follows: To sequence through configuration pages, press [FUNC]. To highlight selectable fields on each page, press [CRSR]. When a field is highlighted, numeric data entry is performed with 0-9 keys, and list selections with 8 or 9 keys. To accept changes, press [CRSR]. Pressing [FUNC] moves on to the next configuration page without saving changes. Serials w/o Perspective Avionics Page Jan 2012

28 Note: The MODE S Address (A/C Reg) page will only be displayed on initial power-up if no address is entered. 1 Set parameters for the MODE S Address (A/C Reg) page. ADDRESS US TAIL# NXXX 2 Set parameters for the Configuration Menu page. JUMP TO DIAGNOSTICS 3 Set parameters for the Audio Mode pages. Verify audio messages by selecting 2, 3, 4, or 5 for MESSAGE. VOICE FEMALE MESSAGE 0 AUDIO PAGE CHANGE ALTITUDE MONITOR MSG ENABLE COUNT DOWN TIMER MSG 4 Set parameters for the Traffic Information page. TRAFFIC MESSAGES TONE 5 Set parameters for the Display Mode page. DISPLAY MODE AUTO LEVEL 75 6 Set parameters for the Display Backlight page. BKLT AUTO RSP TIME 4 MIN 08 BKLT SRCE PHOTO SLOPE 50 OFFSET 50 7 Set parameters for the Key Lighting page. KEY AUTO Page Jan 2012 RSP TIME 4 Serials w/o Perspective Avionics

29 MIN 08 KEY SRCE 28V SLOPE 50 OFFSET 50 8 Set parameters for the Contrast Configuration page. CONTRAST MODE AUTO 9 Set parameters for the ARINC 429 Input pages. SPEED DATA CHANNEL 1 LOW GPS CHANNEL 2 LOW OFF SPEED DATA CHANNEL 3 LOW OFF CHANNEL 4 OFF 10 Set parameters for the ARINC 429 Output page. CHANNEL 1 CHANNEL 2 OFF OFF 11 Set parameters for the RS-232 Input/Output page. INPUT OUTPUT CHNL 1 OFF ICARUS ALT CHNL 2 OFF OFF 12 Set parameters for the Operation Configuration page. VS RATE 0500 FORMAT FEET VFR ID 1200 ALT ALRT DEV Set parameters for the Squat Switch page. Serials w/o Perspective Avionics SQUAT SWITCH? NO Page Jan 2012

30 SENSE LOW DELAY TIME 10 AUTO FLT TMR? CLEAR 14 Set parameters for the Temperature page. SENSOR INSTALLED NO 15 Set parameters for the Mode S Address (A/C Reg) page. ADDRESS US TAIL# NXXX 16 Set parameters for the Mode S Address (Flight ID) page. FLT ID SAME AS TAIL 17 Set parameters for the Mode S Aircraft Type page. AC TYPE MAX A/S <15.5K lb <=300 kt 18 Set parameters for the Gray Code Input page. GRAY CODE ########## DECODED ALTITUDE #### (Field Elevation ±300 feet) Note: No external switches are used. 19 Set parameters for the External Switch page. IDENT STANDBY SQUAT unchecked unchecked unchecked 20 Set parameters for the Analog Input page. 14/5V LTG 000 PHOTO ### LCD TEMP ### 28V LTG 000 REPLY 000 Page Jan 2012 UNIT TMP ### Serials w/o Perspective Avionics

31 21 Set parameters for the RS-232 Input page. CH1 OFF +. n/a CH2 OFF +. n/a 22 Set parameters for the ARINC 429 Channel pages. Note: With GPS in self-test mode, GSPD should read 150 kts. CH1 ### + _ kts CH n/a CH n/a CH n/a (e) (f) 23 Press [OFF] to exit setup. Set BAT 1, BAT 2, and AVIONICS switches in OFF positions. Reset STARTER RELAY and FUEL PUMP RELAY circuit breakers. Serials w/o Perspective Avionics Page Jan 2012

32 H. Transponder Antenna - Serials w/o Perspective Avionics (See Figure 4) (1) Removal - Transponder Antenna (a) Remove access panel CF8. (Refer to 06-00) (b) Disconnect antenna cable from antenna. (c) Serials thru before SB 2X-34-05, & subs: Verify transponder antenna is supported and remove nut and washers securing antenna to fuselage belly. (d) Serials thru after SB 2X-34-05: Verify transponder antenna is supported and remove nut, washers, and ground plane ring securing antenna to fuselage belly. (e) Remove antenna from airplane. (2) Installation - Transponder Antenna (a) Solvent clean installation area. (Refer to 20-30) (b) Serials thru after SB 2X-34-05: Install ground plane ring between transponder antenna gasket and fuselage belly. (c) Verify transponder antenna is inserted and supported in antenna mounting hole in fuselage belly by another aircraft technician. (d) Install washers and nut securing antenna to fuselage belly. (e) Serials thru after SB 2X-34-05, & subs: Torque nut as necessary to ensure antenna collar makes electrical contact with ground plane ring. (f) Connect antenna cable to antenna. (g) Install access cover CF8. (Refer to 06-00) Page Jan 2012 Serials w/o Perspective Avionics

33 FUSELAGE BELLY (REF) 5 3 FUSELAGE BELLY (REF) 5 FUSELAGE BELLY (REF) Serials thru before SB 2X Serials thru after SB 2X Serials thru , & subs w/o Perspective Avionics. Serials thru after SB 2X NOTE Typical installation shown. Avionics stackup may change based on optional equipment installation. Ensure hole in ground plane ring aligns with fuselage skin drain. Figure 4 Transponder and Antenna Installation - Serials w/o Perspective Avionics Serials w/o Perspective Avionics LEGEND 1. GTX Transponder 2. Mounting Rack 3. Ground Plane Ring 4. Transponder Antenna 5. Gasket 6. Washer 7. Nut 8. Connector 9. Coaxial Cable SR22_MM34_1478C Page Jan 2012

34 I. Garmin GTX Transponder - Serials w/ Perspective Avionics (See Figure 5) (1) Removal - Garmin GTX Transponder (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull XPONDER circuit breaker. (c) Remove empennage access panel RE3. (Refer to 06-00) (d) Remove ELT. (Refer to 25-60) (e) Loosen screw securing handle-lock mechanism to transponder. (f) Lift handle-lock mechanism to disengage transponder from connectors. (g) Remove transponder from rack. (2) Installation - Garmin GTX Transponder (a) Position transponder to rack, ensuring handle-lock mechanism engages slot on side of rack. (b) Using handle-lock mechanism, gently push transponder into rack to engage connectors. (c) Tighten screw securing handle-lock mechanism to transponder. (d) Reset XPONDER circuit breaker. (e) If transponder is a different unit from the originally installed transponder, perform Adjustment/Test - Component Software and Configuration Loading. (Refer to 42-00) (f) Perform Adjustment/Test - Garmin GTX Transponder Setup. (Refer to ) (g) Perform Operational Test - Garmin GTX Transponder. (Refer to ) (h) Install ELT. (Refer to 25-60) (i) Install empennage access panel RE3. (Refer to 06-00) (3) Operational Test - Garmin GTX Transponder (a) Verify transponder operation in accordance with 14 CFR (4) Adjustment/Test - Garmin GTX Transponder Setup (a) Power on PFD and MFD in Configuration mode. 1 While holding far right softkey on PFD and MFD, set BAT 1 and AVIONICS switches to ON positions. 2 When INITIALIZING SYSTEM appears in upper left corner of displays, release softkeys. (b) On PFD, use [FMS] knob to select GTX page group. (c) Select Transponder Configuration page. (d) Verify 'ADDRESS TYPE' is 'US TAIL' under the 'SET' and 'ACTIVE' columns. (e) Activate cursor and highlight 'ADDRESS' field. On PFD, use inner and outer [FMS] knob to enter aircraft registration number. (f) On PFD, press [ENT] key. (g) When transponder has successfully configured, press [ENT] key on PFD to accept the message. (h) Deactivate cursor. (i) Pull PFD#1, PFD#2, MFD#1, MFD#2 circuit breakers. (j) Reset PFD and MFD circuit breakers to restart displays in normal operating mode. Page 34 Serials w/ Perspective Avionics