TEMPORARY REVISION AFM-TR-28-01

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Avis Clarke
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1 TEMPORARY REVISION TEMPORARY REVISION INSTALLATION AND OPERATION GTX 330 ES This Temporary Revision is approved and is valid in conjunction with the latest revision of the DA20-C1 Airplane Flight Manual (AFM) until this Temporary Revision has been incorporated into the AFM. This Temporary Revision: - Provides information regading the installation of the Garmin GTX 330 ES transponder. This transponder provides the abiltiy for ADS-B out signals and meets the requirements of TSO-C166b. The limitations and information contained herein either supplement or, in the case of conflict, override those in the Airplane Flight Manual. Doc. No. Chapter Affected Pages DA202-C1, Rev. 28 Chapter DA202-C1, Rev. 28 Chapter DA202-C1, Rev. 28 Chapter 9 S18-1 to S18-6 Instructions: - Print this document on white paper (single-sided). - Copy on yellow paper (single-sided) at a reduced size of 72% to get the correct size for the AFM. - Cut the paper to 6 wide by 8.5 and punch the holes on the left side of each page. - Insert this cover page as the first page of the AFM. - Insert Page 0-19 of this Temporary Revision in front of Page 0-19 in the AFM - Insert Page 9-5 of this Temporary Revision in front of Page 9-5 in the AFM. - Insert Supplment 18 after the last page of the current supplement section - Sign the Temporary Revision Log as having inserted this Temporary Revision. April22, 2015 Cover Page

3 Temporary Revision Supplement No. Title Pages 17 Chinese Placards and Markings 6 18 Garmin GTX 330 with ADS-B Out 6 April 22, 2015 Page 9-5

4 Temporary Revision SUPPLEMENT 18 GARMIN GTX 330 WITH ADS-B OUT TABLE OF CONTENTS Page 1. GENERAL...S OPERATING LIMITATIONS...S EMERGENCY PROCEDURES...S NORMAL OPERATING PROCEDURES...S PERFORMANCE...S WEIGHT AND BALANCE...S DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS...S HANDLING, PREVENTIVE AND CORRECTIVE MAINTENANCE...S18-6 April 1, 2015 Page S18-1

5 Temporary Revision DA20-C1 Flight Manual Intentionally left blank Page S18-2 April 1, 2015

6 Temporary Revision 1. GENERAL The Garmin GTX 330 (Non-Diversity Mode S Transponders) and the GTX 330D (Diversity Mode S Transponders). The ES option of any of the transponders provides ADS-B extended Squitter functionality. All Garmin GTX transponders are a radio transmitter/receiver that operates on radar frequencies, receiving ground radar or TCAS interrogations at 1030 MHz and transmitting a coded response of pulses to ground-based radar on a frequency of 1090 MHz. Each unit is equipped with IDENT capability and will reply to ATCRBS Mode A, Mode C and Mode S All-Call interrogation. Interfaces to the GTX 330 are shown in the following block diagrams. GTX 330D Installas Only Audio Panel Heading Source Traffic System (opt) Display External Ident Squat Switch External STBY Temperature GTX 330/330D GPS Altitude Source Power/Ground Figure S GTX 330/330D Interface The GTX 330 performs the following ADS-B Out functions: Transmission of ADS-B out data on 1090 extended squitter (1090ES) (1090 MHz) Integration of data from internal and external sources to transmit the following data: GPS Position, Altitude, and Position Integrity April 1, 2015 Page S18-3

7 Temporary Revision DA20-C1 Flight Manual 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 code, IDENT, and emergency status Pressure Altitude Broadcast Inhibit 1.1 Capabilities The Garmin GTX 330/33 with ADS-B Out functionality as installed in this aircraft has been shown to meet the equipment requirements of the following: CS-ACNS.D.ADSB. A detailed description of the system operation can be found in the Garmin GTX 330 Pilot s Guide, , Rev G or later. 2. OPERATING LIMITATIONS 2.1 Minimum Equipment ADS-B Out In order provide the proper ADS-B data the GPS source and Altitude source must be fully functional. The GTX 330 only complies with the integrity requirements for ADS-B Out when all required functions are operational. When the system is not operational, ADS-B Out transmit failure messages will be present on the GTX 330 display. 2.2 Applicable Software This AFMS/AFM is applicable to the software versions 7.02 or later approved versions. The Main GTX software version is displayed on the splash screen during start up, for the GTX Pressure Altitude Broadcast Inhibit Pressure Altitude Broadcast Inhibit (PABI) shall only be enabled when requested by Air Traffic Control while operating within airspace requiring an ADS-B Out compliant transmitter. PABI is enabled by selecting the GTX to ON mode. Page S18-4 April 1, 2015

8 Temporary Revision 3. EMERGENCY PROCEDURES 3.1 Abnormal Indications The loss of an interfaced input to the GTX 330 may cause the transponder to stop transmitting ADS-B Out data. Depending on the nature of the fault or failure, the GTX may no longer be transmitting all of the required data in the ADS-B Out messages. If the GTX 330 detects any internal faults or failures with the ADS-B Out functionality, the GTX 330 will annunciate this event via the NO ADSB annunciator on the GTX 330 display screen. When the GTX 330 annunciates the NO ADSB annunciation, one of the following failures or faults have occurred: Loss of adequate GPS position data ADS-B TX (transmit) is selected OFF When the GTX 330 annunciates FAIL to the flight crew, the GTX 330 has detected an internal failure and no transponder data is transmitted. When a GTX 330 NO ADSB, or FAIL annunciation is received, verify proper operation of all interfaced equipment (refer to Section 1.) as the failure of one of these devices could be the cause of the abnormal indication. 3.2 Loss of GPS Navigation Data When the GPS/SBAS receiver is inoperative or GPS position information is not available or invalid, the GTX will no longer be transmitting ADS-B Out data. NO ADSB annunciator illuminated: GPS...VERIFY VALID POSITION 4. NORMAL PROCEDURES NOTE Cockpit Reference Guides for interfaced displays will provide additional operating information specific to the displays or other traffic systems. ADS-B Out functionality resides within the GTX transponders thereby providing a single point of entry for Mode 3/A code, Flight ID, IDENT functionality and activating or deactivating emergency status for both transponder and ADS-B Out functions. Details on performing these procedures are located in the GTX 330/330D Pilot s Guide. April 1, 2015 Page S18-5

9 Temporary Revision DA20-C1 Flight Manual 4.1 Unit Power On NO ADSB... CONSIDERED 4.2 Before Takeoff NOTE The NO ADS-B Annunciation (or associated display annunciations) may illuminate as the unit powers on and begins to receive input from external systems, to include the SBAS position source. NO ADSB... EXTINGUISHED NOTE The NO ADS-B Annunciation (or associated display annunciations) must be EXTINGUISHED for the system to broadcast the ADS-B Out signal. 5. PERFORMANCE There is no change in the performance of the airplane. 6. WEIGHT AND BALANCE / EQIUPMENT LIST The weight and balance of the airplane is not affected. 7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS The Garmin GTX 330 Pilot s Guide, , Rev G or later contain additional information regarding GTX system description, control, and function. Also refer to the latest revision of the Garmin GPS (GNS430/530 or GTN 650) for further information. 8. HANDLING, PREVENTIVE AND CORRECTIVE MAINTENANCE Other than periodic functional checks required by operational rules, maintenance of the GTX 330 is on condition only. Refer to the GTX 330 Maintenance Manual (Garmin P/N ). There is no change to the handling, preventive and corrective maintenance. Page S18-6 April 1, 2015

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Page 9 - S Dec-09 D42L-AFM-002 Supplement 2 D42L AFM Intentionally left blank Page 9 - S2-2 10-Dec-09 D42L-AFM-002 DOT Approved D42L AFM Supplement 2 LIST OF EFFECTIVE PAGES Chapter Page Date 0 DOT-approved 9-S2-1 10-Dec-09 9-S2-2 10-Dec-09