Technisonic TDFM-136A VHF/FM Digital Airborne Transceiver User Manual 1

Technisonic Industries Limited VHF/FM Digital Airborne Transceiver 1

Contents

User Manual 1

   VHF/FM DIGITAL AIRBORNE TRANSCEIVER MODEL TDFM-136A      Installation Instructions   TiL Document No. 09re404 Revision C Issue 1   JUNE 2009         Technisonic Industries Limited 240 Traders Boulevard, Mississauga, Ontario L4Z 1W7 Tel: (905) 890-2113 Fax: (905) 890-5338 www.til.ca
  REVISIONS for 09re404 Sections 1 – 2 REV  SECTION - PAGE -  DESCRIPTION DATE      A  - Table 1-1 - STC Approv. - Table 1-5  - FCC Compliance Changed operating temp to –30 to +60 C. Change references of DO-160C to 160D. Change Temp & Alt to B4 and D1. Change Magnetic Effect to class Z. Add FCC RF Exposure Requirements warning. May 26/09 B - FCC Compliance  - Table 1-4 - 2.5 Antenna Installation. - Footer, all pages. Change separation distance from 110cm to 1.0m. Change RF Output Power Low to read “1W”.  Change 0dB to 3dBi and 20cm (8 inches) to 1.0m (40 inches).  Remove “and Operating” from “Installation and Operating Instructions”. June 15/09 C  2.5  Change antenna supplier & part number to Comant Industries Inc. / Part No. CI 292-3 Jun 26/09      D  2-5  Fig 2-3 Wiring Connections (added ITEM 4)  Aug 12/09
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TECHNISONIC INDUSTRIES LIMITED www.til.ca    ESD CAUTION  This unit contains static sensitive devices. Wear a grounded wrist strap and/or conductive gloves when handling printed circuit boards.   FCC COMPLIANCE INFORMATION This device complies with Part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference and (2) this device must accept any interference received, including interference that may cause undesired operation.  WARNING:  For compliance with FCC RF Exposure Requirements, the mobile transmitter antenna installation shall comply with the following conditions:  1.  The transmitter antenna gain shall not exceed 3 dBi.  2.  The transmitter antenna is required to be located outside of a vehicle and kept at a separation distance of 1.0 meter or more between the transmitter antenna of this device and persons during operation.  NOTE:  This equipment has been tested and found to comply with the limits for a Class B digital device, pursuant to Part 15 of the FCC Rules. These limits are designed to provide reasonable protection against harmful interference in a residential installation. This equipment generates, uses, and can radiate radio frequency energy and, if not installed and used in accordance with the instruction manual, may cause harmful interference to radio communications. However, there is no guarantee that interference will not occur in a particular installation. If this equipment does cause harmful interference to radio or television reception, which can be determined by turning the equipment off and on, the user is encouraged to try to correct the interference by one or more of the following measures: •  Re-orient or relocate the receiving antenna •  Increase the separation between the equipment and receiver •  Connect the equipment into an outlet or circuit different from that to which the receiver is connected. •  Consult the dealer or an experienced radio/TV technician for help.   WARNING Changes or modifications not expressly approved by Technisonic Industries could void the user’s authority to operate the equipment.   WARRANTY INFORMATION The Model TDFM-136A transceiver is under warranty for one year from date of purchase. Failed units caused by defective parts, or workmanship should be returned to:   Technisonic Industries Limited 240 Traders Boulevard Mississauga, Ontario L4Z 1W7  Tel: (905) 890-2113 Fax: (905) 890-5338   NOTICE: The above stated address supersedes all others that may appear otherwise in this manual.
TECHNISONIC INDUSTRIES LIMITED www.til.ca    STC APPROVAL NOTE Presently, no TSO standard exists for airborne FM transceivers. To make it easier for installation agencies to provide their customers with an approved installation supported by an effective Airworthiness Approval, Technisonic has secured Supplemental Type Certificate (STC) Approvals (both US and Canadian) on its Airborne FM products for many helicopters currently being delivered in the US and Canada as well as a number of single engine fixed wing aircraft. The above referenced DO-160D test data is also on file and available from Technisonic to support approval requirements in airframes for which Technisonic does not possess an STC.  Approved aircraft types are listed in the attachments to the formal STC documents. These STCs are the exclusive property of Technisonic and require the written authority of Technisonic for their use. To assist Factory Authorized Technisonic Dealers in the certification process, we have placed copies of our Canadian and US STCs on our web site along with a letter of authorization for their use. These documents may be downloaded and used as support for the technical submission to FAA or Transport Canada. Only authorized factory dealers/installers are permitted to download and make use of these documents on behalf of their customers (end users) in support of regulatory agency approval. Please refer to the Technisonic web site www.til.ca for the latest issue of available STCs and letter of authorization for use.         COPYRIGHT NOTICE This document contains designs and other information which are the property of Technisonic Industries Ltd. Except for rights expressly granted by contract to the Canadian Government, or to the United States Government, this document may not, in whole or in part, be duplicated or disclosed or used for manufacture of the part disclosed herein, without the prior permission of Technisonic Industries Ltd.         WARNING AND DISCLAIMER This manual is designed to provide information about the TDFM-136A. Every effort has been made to make this manual as complete and accurate as possible.
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions        Page v TiL 09RE404 Rev C Issue 1  TABLE OF CONTENTS  SECTION  TITLE  PAGE Table of Contents .............................................................................................................................       v List of Figures ...................................................................................................................................      vi List of Tables ....................................................................................................................................      vi    SECTION 1  GENERAL DESCRIPTION 1.1 Introduction  .......................................................................................................................     1-1 1.2 Description  ........................................................................................................................     1-1 1.3  Purpose of Equipment ......................................................................................................     1-1 1.4 Model Variation  .................................................................................................................     1-2 1.5 Technical Characteristics  ................................................................................................     1-2 1.6 Certification Summary ......................................................................................................     1-5    SECTION 2  OPERATING INSTRUCTIONS 2.1 General ...............................................................................................................................     2-1 2.2  Equipment Packing Log  ...................................................................................................     2-1 2.3 Transceiver Installation ....................................................................................................     2-1 2.4  Installation Kit – Contents ................................................................................................     2-1 2.5 Antenna Installation ..........................................................................................................     2-1 2.6  Installation - Pin Locations and Connections ................................................................     2-2 2.7 Wiring Instructions  ...........................................................................................................     2-4 2-7.1 Main Power +28VDC ....................................................................................................     2-4 2-7.2 Main Ground .................................................................................................................     2-4 2-7.3 PTT (Ground Keying)  ...................................................................................................     2-4 2-7.4  Front Panel Back Lighting  ............................................................................................     2-4 2-7.5  Audio Outputs (600 ohms and 4 0hms)  .......................................................................     2-4 2-7.6 Audio Output Ground  ...................................................................................................     2-4 2-7.7 Mic Signal Input ............................................................................................................     2-4 2-7.8 Memory Up/Memory Down  ..........................................................................................     2-4 2-7.9 Data Input/Output .........................................................................................................     2-4 2.8  Transmitter Side Tone Level Adjustment .......................................................................     2-6 2.9  Main and Guard Noise Squelch Adjustment  ..................................................................     2-6 2.10 Reference Layouts ............................................................................................................     2-7    APPENDICES APPENDIX A Post Installation EMI Test Instructions.......................................................................     A-1  PURPOSE ................................................................................................................................     A-1  TEST CONDITIONS .................................................................................................................     A-1  METHODOLOGY ......................................................................................................................     A-1  RESULTS .................................................................................................................................     A-1  PROCEDURE ...........................................................................................................................     A-2
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions        Page vi TiL 09RE404 Rev C issue 1  LIST OF FIGURES  FIGURE  TITLE  PAGE2-1  Transceiver Mounted View of the 15-Pin Connector  ..........................................................     2-2 2-2  Outline Drawing for TDFM-136A Transceiver .....................................................................     2-3 2-3  Wiring Connections for TDFM-136A Transceiver  ...............................................................     2-5 2-4  Control points for the TDFM-136A MCU Board  ..................................................................     2-7       LIST OF TABLES  TABLE  TITLE  PAGE 1-1  TDFM-136A – General Characteristics ...............................................................................     1-3 1-2  TDFM-136A – Operational Characteristics .........................................................................     1-4 1-3  TDFM-136A – Receiver Characteristics – Main and Guard  ...............................................     1-4 1-4  TDFM-136A – Transmitter Characteristics  .........................................................................     1-5 1-5  TDFM-136A – Environmental Testing Summary  ................................................................     1-5   2-1  TDFM-136A - Rear Connector Pin Assignments ................................................................     2-2
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 1-1 TiL 09RE404 Rev C Issue 1  SECTION 1 - GENERAL DESCRIPTION  1.1 INTRODUCTION This publication provides operating and installation information for the TDFM-136A, Digital Transceiver manufactured by Technisonic Industries Limited. The TDFM-136A is Project 25 (P25), Phase 1 compliant. The unit offers digital or conventional analog FM communications over an extended frequency range with selectable channel spacing and is intended for use (in the U.S.) only by government agencies or contractors thereto, who have obtained licensing for operation in the 136-150 MHz portion of the band. If the TDFM-136A transceiver is used in CANADA, operation is restricted to the following sub bands: 138-144, 148-148.99, 149.005-150.005 and 150.05-174 MHz. Furthermore the frequency agile transceiver is restricted to airborne use and must not be operated as a base station in Canada.  1.2   DESCRIPTION The TDFM-136A, Transceiver is a frequency agile, fully synthesized airborne transceiver capable of operating in the 136.000 MHz to 174.000 MHz frequency range in 2.5 kHz increments with either 25 kHz analog, 12.5 kHz analog channel spacing and P25, 12.5 kHz digital modulation on a channel by channel basis. The Transceiver can operate without restriction on any split frequency pair in the band and also incorporates a two channel synthesized guard receiver.  The TDFM-136A Transceiver provides 230 operator accessible memory positions. Each of which is capable of storing Scan List membership information, up to eight (8) character alphanumeric identifier, and Operating Mode information. In addition each memory position contains information for both transmit and receive including: frequency, CTCSS tone, DCS (DPL) code, P25 TalkGroup, and P25 Network Access Code (NAC) information.  Channel operating parameters, including frequency and other related data, are presented on a 48-character, two-line LED matrix display. Data entry and function control takes place via a 12-button keypad.  1.3   PURPOSE OF EQUIPMENT The TDFM-136A, Digital VHF/FM Transceiver is designed to provide secondary airborne communications to facilitate operations which are typically performed in a low altitude environment. The transmitter section of this unit has a minimum of 8 watts and does not exceed 10 watts output power, which may be reduced by a front panel switch to 1 watt, in order to reduce interference to land based systems.
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 1-2 TiL 09RE404 Rev C Issue 1  1.4   MODEL VARIATION There are twelve variations of the Model TDFM-136A Transceiver.  All units offer identical features and performance except for the following differences:  TDFM-136A, P/N 091258-1-10      GREEN display 28v back lighting, no Encryption. TDFM-136A, P/N 091258-1-11      GREEN display 28v back lighting, with Encryption. TDFM-136A, P/N 091258-2-10      RED display 28v back lighting, no Encryption. TDFM-136A, P/N 091258-2-11       RED display 28v back lighting, with Encryption. TDFM-136A, P/N 091258-3-10      NV display 28v back lighting, no Encryption. TDFM-136A, P/N 091258-3-11       NV display 28v back lighting, with Encryption. TDFM-136A, P/N 091258-4-10      GREEN display 5v back lighting, no Encryption. TDFM-136A, P/N 091258-4-11      GREEN display 5v back lighting, with Encryption. TDFM-136A, P/N 091258-5-10      RED display 5v back lighting, no Encryption. TDFM-136A, P/N 091258-5-11       RED display 5v back lighting, with Encryption. TDFM-136A, P/N 091258-6-10      NV display 5v back lighting, no Encryption. TDFM-136A, P/N 091258-6-11       NV display 5v back lighting, with Encryption.
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 1-3 TiL 09RE404 Rev C Issue 1  1.5 TECHNICAL CHARACTERISTICS The tables below provide the technical characteristics for the Technisonic Industries Ltd. Model TDFM-136A.  TABLE 1-1 TDFM-136A – General Characteristics Characteristic  Specification Dimensions (including heat sink)  Approx. 8.0" X 3.0" X 5.75" Weight  Approx. 3.5 Lbs (1.6 Kg) Mounting    Panel Mount via DZUS fasteners   Power Requirement:    Voltage    Current  28.0 VDC, ±15% Receive - 0.7 A Max. Transmit Low Power (1W) - 1.3 A Max. Transmit High Power (8-10W) - 2.0 A Max.   Audio Output Power:    Headset    Speaker Output  0.5 Watts into 600 ohms 2.5 Watts min. into 4 ohms   Back Lighting  28 Volts (standard) 5 Volts (specify)   Display Colour  Green (standard) Red (specify) NVG (optional)   Temperature Range:    Operating    Storage -30ºC to +60ºC -55ºC to +85ºC Altitude 50,000 feet
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 1-4 TiL 09RE404 Rev C Issue 1  TABLE 1-2 TDFM-136A – Operational Characteristics Characteristic  Specification Frequency Range:  136.000 to 174.000 MHz Operating Modes:  Conventional analog: 12.5 / 25 kHz. P25 CAI: 12 KBPS FSK, 9.6 KBPS C4FM Channel Spacing:  25 kHz. or 12.5  kHz Programmable Memories:    Scan Lists    Description    Operating Modes    Frequency    Squelch Modes 230 memories  15 scan lists  Up to 8 characters, alpha-numeric   Analog Wide, Analog Narrow, P25 Digital  Rx/Tx (Simplex/Duplex), 136.0000 – 174.0000  Rx/Tx (Simplex/Duplex), CTCSS Tones, DCS Codes,    P25 TalkGroup, P25 NAC Guard Receiver:    Description    Operating Modes    Frequency    Squelch Modes 2 channels programmed with:   Up to 8 characters, alpha-numeric    Analog Wide, Analog Narrow, Digital   Rx/Tx (Simplex/Duplex), 136.0000 – 174.0000 MHz.   Rx/Tx (Simplex/Duplex), CTCSS Tones, DCS Codes,      P25 TalkGroup, P25 NAC CTCSS Tones  42 CTCSS tones, including all standard tones. DCS Codes  All standard DCS (DPL1) codes P25 TalkGroup  $0000 to $FFFF  ( 0 to 65535 )  P25 Network Access Code (NAC)  $000 to $FFF  ( 0 to 4095 )   DPL1 is a trademark of Motorola Corporation  TABLE 1-3 TDFM-136A – Receiver Characteristics – Main and Guard Characteristic  Specification Sensitivity at 12 dB SINAD  -116dBm Adjacent Channel Selectivity  -60dB (25 or 12.5 kHz) Spurious Attenuation  -70 dB Third Order Intermodulation  -70 dB Image Attenuation  -80 dB FM Acceptance   ± 6 kHz Hum and Noise  better than 45dB Audio Distortion  less than 5% Antenna Conducted Emission  less than -57dBm
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 1-5 TiL 09RE404 Rev C Issue 1  TABLE 1-4 TDFM-136A – Transmitter Characteristics Characteristic Specification RF Output Power:      Low      High  1W. 10W. Output Impedance  50 ohms Maximum Deviation:      Wide (25 kHz)      Narrow (12.5 kHz)  ± 5 kHz  ± 2.5 kHz Maximum Deviation – Narrow  ± 2.5 kHz  (12.5 kHz mode) Spurious Attenuation  -90 dB below carrier level Frequency Stability  ± 2.5 ppm Microphone Circuit  Carbon or equivalent Sidetone Output  0.5W (max) into 600 ohms Harmonic Attenuation  -65 dB below carrier level FM Hum And Noise  -40 dB Audio Input  50 mV at 2.5 into 200 Ω input circuit for ± 3.5 deviation, adjust. Audio Distortion  Less than 5% 1.6 CERTIFICATION SUMMARY The following table gives a summary of DO-160D Environmental Testing for Technisonic Model TDFM-136A, VHF Digital Transceiver.   TABLE 1-5 TDFM-136A – Environmental Testing Summary Conditions  Section  Description of Conducted Tests Temperature and Altitude  4.0  Equipment tested to categories B4 and D1. Temperature Variation  5.0  Category B. Humidity 6.0 Category A. Operational Shock and Crash Safety 7.0 Category A. Vibration  8.0  Equipment is tested without shock mounts to categories S and U. Magnetic Effect  15.0  Equipment is class Z. Power Input  16.0  Category B. Voltage Spike  17.0  Category B. Audio Frequency Susceptibility  18.0  Category B. Induced Signal Susceptibility  19.0  Category A. Radio Frequency Susceptibility  20.0  Category U. RF Emission (DO-160D) RF Emission (DO-160C) 21.0 Category B. Category Z. Electrostatic Discharge  25.0  Category A.
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TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 2-1 TiL 09RE404 Rev C Issue 1  SECTION 2 – INSTALLATION INSTRUCTIONS 2.1   GENERAL This section contains information and instructions for the correct installation of the  TDFM-136A, VHF/FM Digital Transceiver. Make certain that the correct frequencies are pre-programmed in accordance with the equipment user's valid FCC operator's license, prior to installation.  2.2   EQUIPMENT PACKING LOG Unpack the equipment and check for any damage that may have occurred during transit. Save the original shipping container for returns due to damage or warranty claims. Check that each item on the packing slip has been shipped in the container. Verify that the equipment display and back-lighting configuration are the same as those ordered.  2.3   TRANSCEIVER INSTALLATION The TDFM-136A Transceivers are designed to be Dzus mounted and should be installed in conjunction with an IN-150 installation kit. See Figure 2-1 for an outline drawing of the unit with dimensions to facilitate the installation.  2.4   INSTALLATION KIT - CONTENTS The IN-150 installation kit consists of: 1.  One 15-pin (female) Cannon D-mating connector complete with crimp pins and hoods. 2.  One BNC antenna mating RF connector (male) and hood.  2.5   ANTENNA INSTALLATION Antenna, P/N CI 292-3 may be obtained from Comant Industries Inc. or a suitable equivalent 3dBi gain antenna may be used with the TDFM-136A transceivers. The antenna should be mounted on the bottom of the aircraft whenever possible and must be located at least 1.0 meter (40 inches) from any occupant in the airframe. Consult with instructions provided with the antenna. Connect RF cable from antenna to the back of the TDFM-136A unit by utilizing the BNC mating connector provided in the installation kit.  2.6   INSTALLATION - PIN LOCATIONS AND CONNECTIONS A single 15-pin DSUB connector, mounted on the rear of the unit, provides the means to connect all power, control and audio signals between the TDFM-136A and the airframe. The pin numbers and locations for the 15-pin DSUB connector are shown in figure 2-1 below. The view shown is of the connector mounted in the unit, select mating connector appropriately.    FIGURE 2.1 Transceiver mounted view of 15-pin male connector
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 2-2 TiL 09RE404 Rev C Issue 1  Table 2-1 provides the description of the pin connections for the transceiver.  TABLE 2-1 TDFM-136A  - Rear Connector Pin Assignments Pin #  Description  Notes 1  Audio - Headset  Output  – 600 Ohms 2  Serial Data Out  Output  – RS232 3  Power - Panel Lighting  28 VDC Standard, 5VDC Optional 4  Signal - Memory Up  Input – active low 5  Signal - Memory Down  Input – active low 6  Audio - Microphone  Input 7,14  Power - Main +28VDC  Power 8,15  Power - Main Ground  Power 9  Audio - Speaker  4-Ohm Speaker Output 10  Signal Ground  4-Ohm / 600-Ohm Output Ground 11  Serial Data In  Input  – RS232 13  Signal – PTT  Input – active low
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 2-3 TiL 09RE404 Rev C Issue 1    (All dimensions in inches)  FIGURE 2-2 Outline Drawing for Model TDFM-136A Transceiver
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 2-4 TiL 09RE404 Rev C Issue 1  2.7  WIRING INSTRUCTIONS – 15-PIN D-CONNECTOR Figure 2-3 shows all required connections and recommended wire sizes for the TDFM-136A Transceiver operation in the airframe.  2.7.1  Main Power +28 VDC The main power +28VDC (± 15%) is connected to pins 7 and 14 of the 15-pin D-connector on the transceiver. Both pins should be connected.  2.7.2 Main Ground Ground connections for the transceiver are made on pins 8 and 15. Both pins should be connected.  2.7.3  PTT (Ground Keying) The PTT line is connected to pin 13 and should be floating when the transceiver is in receive mode, and grounded during transmit mode.  2.7.4  Front Panel Back Lighting Front panel back lighting connection should be made on pin 3 of the transceiver. The opposite end of this lead should be connected to the panel lighting system of the aircraft. Before connecting, verify the required panel lighting voltage (28 VDC or 5 VAC) on the transceiver configuration control label.  2.7.5  Audio Outputs (600 Ohms and 4 Ohms) The audio output from pin 9 can be used to drive a 4 ohm speaker up to 2.5 watts. Audio output from pin 1 is 600 Ohms, 0.5 watts maximum.  2.7.6   Audio Output Ground Pin 10 is the ground for both the 4 and 600 Ohms audio output signals on pins 9 and 1.  2.7.7   Mic Signal Input The microphone input signal is to be provided on pin 6, utilizing shielded wire with the shield grounded to pin 10.  2.7.8   Memory Up/Memory Down Remote scrolling through the 25 memory positions can be achieved by providing a ground to pins 4 (up) and 5 (down) through a momentary contact cyclic switch.  2.7.9   Data Input Channel data may be transferred to and from the unit using RS-232 communications protocol via pins 2 and 11.
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 2-5 TiL 09RE404 Rev C Issue 1      Figure 2-3 Wiring Connections for TDFM-136A Transceiver
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 2-6 TiL 09RE404 Rev C Issue 1  2.8   TRANSMITTER SIDE TONE LEVEL ADJUSTMENT The side tone level is set at the factory; however, this level can be altered to suit local conditions as follows: 1.  Set the transceiver operating frequency to 155.000 MHz and connect an appropriate test receiver to the RF output connector.  Ensure that the output of the transceiver is terminated into a proper dummy load. 2.  Key the transmitter and input a 1 kHz audio signal @ -10 dBm (0.25 VRMS) into the microphone input. 3.  Select the side-tone adjust command (L2-7) and then adjust the side-tone level using the up/down arrows (keys 2 & 8) to produce a +3.0 dBm (1.0 VRMS) 600 Ohm audio output.  2.9  MAIN AND GUARD NOISE SQUELCH ADJUSTMENT The squelch (on both the main and guard receivers) is factory set to open at approximately 0.5 micro-volts. This adjustment can be altered to suit local conditions as follows: 1.  Set the main receiver of the transceiver to 155.000 MHz. Connect a signal generator to the antenna input of the transceiver. 2.  Set the signal generator to produce a ± 3 deviation with a 1 kHz tone on 156.000 MHz. Increase the signal generator RF level from 0.1 uV until the squelch indicator LED is on. Verify the receiver SINAD ratio is between 12 and 14 dB. 3.  If not, re-adjust main receiver squelch via the main receiver squelch software command. 4.  Repeat the above procedure to adjust the guard receiver squelch setting using guard receiver squelch adjustment software command.   2.10   REFERENCE LAYOUTS A reference layout indicating the position of control points for the MCU board is shown in Figure 2-4.
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                     Page 2-7 TiL 09RE404 Rev C Issue 1  J2:  Boot Program Enable - factory set   DO NOT INSTALL J4: Option Jumpers:   1-2 Maintenance Mode Enable - DO NOT INSTALL IN AIRFRAME, BENCH ONLY  2-4 Factory Use Only – DO NOT INSTALL   5-6 n/u reserved  R8:  Main Rx Audio adjust - factory set R10:  Tx Mic Audio Level Adjust – factory set R11:   Guard Rx Audio adjust – factory set R17:  RF Low power adjust – factory set R18:  RF High power adjust – factory set R56:  DTMF Level Adjust – factory set     FIGURE 2-4 Control points for the TDFM-136A MCU Board
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TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                    Page A-1 TiL 09RE404 Rev C Issue 1  APPENDIX A – POST INSTALLATION EMI TEST INSTRUCTIONS”  PURPOSE The purpose of these tests is to identify any interference that the TDFM-136A may cause with existing aircraft systems. TEST CONDITIONS The TDFM-136A transceiver should be installed and function tested. The antenna VSWR should be checked. A forward/reverse power check with an in-line wattmeter should show no more than 10% reflected power. For the following tests, insure that the power switch is in the high position. METHODOLOGY Most of the EMI tests can be accomplished on the ground. In some cases flight testing is required or is easier. If the aircraft is approved for IFR operations, then it is mandatory that interference between the TDFM-136A Airborne FM and the approach aids be checked in flight.  The GPS should be operational and navigating with at least the minimum compliment of satellites. The VHF COMM should be set to the frequencies indicated with the squelch open. VOR/DME receivers should be set to the frequencies indicated and selected for display. If possible, set up a DME ramp test set on the frequencies indicated and adjust the output until the flags are out of view. The transponder and encoder should be monitored with ramp test equipment. Set the output of the transponder test set to 3db above the output necessary to achieve 90% reply. If possible set the ADF to a nearby navigation station.  Modulate the TDFM-136A transmitter on the indicated frequencies for at least 20 seconds. Observe the GPS for any degradation in satellite status or availability or flags. Listen for any noise or detected audio signals on the VHF COMM(s). Listen for any noise or detected audio signals on the VOR/LOC receiver audio; look for any movement of flags or needles on the VOR/LOC/GS navigation display(s). Observe the transponder for any loss of reply or spurious reply.  List the power plant, fuel and other electric instruments in the chart provided and note any anomalies that occur while transmitting. Assess the results.  If the aircraft is equipped with an auto-pilot or a stability augmentation system, then test fly the aircraft and verify that operation of the TDFM-136A transceiver does not have adverse effects on these systems. After checking for gross effects at a safe altitude, fly an approach with each of the different navigation systems coupled to the auto-pilot (ILS, GPS etc.) and look for any anomalies. RESULTS If the installed system passes all of the applicable EMI tests, then no further action is required. If interference is observed, then the interference must be assessed against the appropriate standards of airworthiness for the system in question. For example, it is permissible for a VFR certified GPS to lose navigation capability while the TDFM-136A is transmitting providing that it recovers properly and promptly, but is not permissible for an IFR approach certified GPS to be affected in the same way. A complete discussion of all the standards of airworthiness to be applied in assessing EMI effects is beyond the scope of this document.
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                    Page A-2 TiL 09RE404 Rev C Issue 1  PROCEDURE A.   Operate the TDFM-136A transmitter on the following frequency for at least 20 seconds. Observe the GPS for any degradation in satellite status or availability or flags.   FREQUENCIES  GPS #1  GPS #2 TDFM-136A  PASS FAIL PASS FAIL 143.1800 MHz      143.1825 MHz      157.5000 MHz      157.5425 MHz        NOTES:
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                    Page A-3 TiL 09RE404 Rev C Issue 1  B.   Determine if the image frequency for the VHF COMM falls within the range of the TDFM-136A. If so, select a set of frequencies that will cause the TDFM-136A to be set as close as possible to the image frequency. Any one of the many possible sets will suffice. Record those values in the spaces provided in the following chart. Modulate the TDFM-136A transmitter on the following frequencies for at least 20 seconds. Listen for any noise or detected audio signals on the VHF Comm.  EXAMPLE: Bendix/King KY 196A.  The first IF frequency is 11.4 MHz. The LO is above the receive frequency (high side injection). Therefore, the image frequency is 22.8 MHz above the selected frequency. Set the KY 196A to 120.000 MHz and the TDFM-136A to 142.8000 MHz.   FREQUENCIES RESULTS VHF #1  TDFM-136A  PASS  FAIL 135.975 MHz  135.975 MHz     121.150 MHz  121.150 MHz     131.250 MHz  131.250 MHz     Image       FREQUENCIES RESULTS VHF #2  TDFM-136A  PASS  FAIL 138.0000 MHz  138.0000 MHz     157.5000 MHz  157.5000 MHz     157.5000 MHz  157.5000 MHz     Image       NOTES:
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                    Page A-4 TiL 09RE404 Rev C Issue 1  C.   Determine if the image frequency for the VOR/ILS Nav falls within the range of the TDFM-136A. If so, select two sets of frequencies that will cause the TDFM-136A to be set a close as possible to the image frequency.  Chose one set in the localizer frequency range and one in the VOR frequency range. Record those values in the spaces provided in the following chart. Modulate the TDFM-136A transmitter on the following frequencies for at least 20 seconds. Listen for any noise or detected audio signals on the receiver audio; look for any moment of flags or needles on the navigation display.   FREQUENCIES RESULTS VOR / ILS #1  TDFM-136A  PASS  FAIL 108.000 MHz  162.0000 MHz     108.100 MHz  162.1500 MHz     Image     Image       FREQUENCIES RESULTS VOR / ILS #2  TDFM-136A  PASS  FAIL 108.000 MHz  162.0000 MHz     108.100 MHz  162.1500 MHz     Image     Image       NOTES:
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                    Page A-5 TiL 09RE404 Rev C Issue 1  D.   Modulate the TDFM-136A transmitter on the following frequencies for at least 20 seconds.  Observe the Glide Slope displays. Look for any movement of flags or needles on the Navigation display.   FREQUENCIES RESULTS Glide slope #1  TDFM-136A  PASS  FAIL 334.7 (108.1)   167.3500 MHz               FREQUENCIES RESULTS Glide slope #2  TDFM-136A  PASS  FAIL 334.7 (108.1)   167.3500 MHz               NOTES:
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                    Page A-6 TiL 09RE404 Rev C Issue 1  For the following tests (E & F), select a frequency at the top, middle and bottom of the band of the TDFM-136A Transceiver.   VHF Band (138 to 174 MHz) Frequency No. 1   Frequency No. 2   Frequency No. 3     E.  At a safe altitude engage the autopilot or stability augmentation system. Modulate the TDFM-136A on the above frequencies for at least 20 seconds. Observe any effect on the autopilot or stability augmentation system.  Observations:               F.  Perform a coupled ILS approach to the aircraft’s certified limits. Modulate the TDFM-136A transmitter on the above frequencies for at least 20 seconds. Observe any effect on the autopilot. Repeat for second flight director/autopilot if so equipped.  Observations:
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                    Page A-7 TiL 09RE404 Rev C Issue 1  G.   List the power plant, fuel and other electric instruments in the chart provided and note any anomalies that occur while transmitting. Assess the results.  STEP SYSTEM PASS FAIL  NOTES 1  COMM 1 and 2       2 Transponder and Encoder      3  ADF 1 and 2       4 Vertical Gyro       5  Glide slope 1 and 2       6  VOR/LOC 1 and 2       7 Directional Gyro       8 Compass       9 Fuel Pressure       10 Oil Temperature       11 Ammeter       12 Bus Voltage       13 Fuel       14 Nt       15 TOT       16 % Torque       17 Digital Clock       18 Oil Pressure       19 Annunciators
TECHNISONIC INDUSTRIES LIMITED www.til.ca   TDFM-136A    Installation Instructions                    Page A-8 TiL 09RE404 Rev C Issue 1  STEP SYSTEM PASS FAIL  NOTES                                                                                            NOTES:

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