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Apollo Mode A/C Transponder Model SL70 Installation Manual Final Draft August 11, 1999 August 1999 560-0402-00 1999 by UPS Aviation Technologies. All rights reserved. Printed in the U.S.A. No part of this document may be transmitted, reproduced, or copied in any form or by any means without the prior written consent of UPS Aviation Technologies. Due to our commitment to constantly improve the quality and performance of our products, information contained in this document is subject to change without notice. UPS Aviation Technologies and Apollo are registered trademarks of UPS Aviation Technologies. UPS Aviation Technologies P.O. Box 13549 Salem, OR 97309 Phone (503)581-8101 1-800-525-6726 In Canada 1-800-654-3415 FAX (503)364-2138 2345 Turner Rd. S.E. Salem, OR 97302 U.S.A. HISTORY OF REVISIONS Revision Draft Date 8/11/99 Description Final draft. IMPORTANT NOTE The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those desiring to install this article on or within a specific type or class of aircraft to determine that the aircraft operating conditions are within TSO standards. The article may be installed only if further evaluation by the applicant documents an acceptable installation and is approved by the Administrator. ORDERING INFORMATION To receive additional copies of this publication, order part # 560-0402, Apollo SL70 Mode A/C Transponder Installation Manual. REFERENCE PUBLICATIONS Following are other publications referenced in this guide. NOTES Table of Contents TABLE OF CONTENTS SECTION 1 - INTRODUCTION.................................................................................................1 ABOUT THIS MANUAL......................................................................................................................1 APOLLO SL70 DESCRIPTION.............................................................................................................1 FEATURES.........................................................................................................................................2 REGULATORY COMPLIANCE .............................................................................................................2 UNPACKING THE EQUIPMENT............................................................................................................3 PACKAGE CONTENTS........................................................................................................................3 OTHER REQUIRED MATERIALS .........................................................................................................3 SPECIAL TOOLS REQUIRED ...............................................................................................................4 SECTION 2 - INSTALLATION..................................................................................................5 PRE-INSTALLATION INFORMATION....................................................................................................5 INSTALLATION OVERVIEW................................................................................................................5 INSTALLATION CONSIDERATIONS......................................................................................................5 MOUNTING CONSIDERATIONS.................................................................................................................................... 5 MINIMUM SYSTEM CONFIGURATION ......................................................................................................................... 5 ALTITUDE INPUT........................................................................................................................................................ 5 ANTENNA.................................................................................................................................................................. 6 EQUIPMENT MOUNTING....................................................................................................................6 UNIT INSTALLATION / REMOVAL ............................................................................................................................... 7 ELECTRICAL CONNECTIONS..............................................................................................................7 POWER ...................................................................................................................................................................... 8 ALTITUDE INPUT........................................................................................................................................................ 8 SERIAL INTERFACE .................................................................................................................................................... 8 DISCRETE INPUTS...................................................................................................................................................... 8 ANTENNA INSTALLATION AND CONNECTIONS ..................................................................................9 POST INSTALLATION CHECKOUT.....................................................................................................12 TEST MODE CHECKOUT AND SETUP........................................................................................................................ 12 OPERATION / PERFORMANCE CHECKOUT ................................................................................................................ 13 SECTION 3 - SPECIFICATIONS.............................................................................................15 ELECTRICAL ...................................................................................................................................15 PHYSICAL .......................................................................................................................................15 ENVIRONMENTAL ...........................................................................................................................16 ALTITUDE INPUT.............................................................................................................................16 DISCRETE INPUTS ...........................................................................................................................16 SERIAL INTERFACE .........................................................................................................................16 TRANSPONDER PERFORMANCE.......................................................................................................17 ANTENNA REQUIREMENTS..............................................................................................................17 SECTION 4 - LIMITATIONS ...................................................................................................19 INSTALLATION ................................................................................................................................19 OPERATIONAL ................................................................................................................................19 APPENDIX A - TROUBLESHOOTING..................................................................................21 CONTACTING THE FACTORY FOR ASSISTANCE................................................................................22 Apollo SL70 Installation Manual i Table of Contents APPENDIX B - PERIODIC MAINTENANCE ....................................................................... 23 BIENNIAL CHECK ........................................................................................................................... 23 CLEANING THE FRONT PANEL ........................................................................................................ 23 APPENDIX C - ENVIRONMENTAL QUALIFICATIONS .................................................. 25 APPENDIX E - SERIAL DATA PROTOCOL........................................................................ 27 ALTITUDE INPUT / OUTPUT......................................................................................................................................27 LIST OF TABLES TABLE 1 PACKAGE CONTENTS ........................................................................................................ 3 TABLE 2 REAR CONNECTOR PINOUT............................................................................................. 18 TABLE 3 TROUBLESHOOTING GUIDE............................................................................................. 21 TABLE 4 ALTITUDE DATA FORMAT............................................................................................... 27 LIST OF FIGURES FIGURE 1 SL70 FRONT PANEL ........................................................................................................ 2 FIGURE 2 MOUNTING FRAME ASSEMBLY........................................................................................ 6 FIGURE 3 CABLE ROUTING.............................................................................................................. 7 FIGURE 4 COAX CABLE ASSEMBLY................................................................................................. 9 FIGURE 5 WIRING DIAGRAM - GRAY CODE ALTITUDE INPUT ....................................................... 10 FIGURE 6 WIRING DIAGRAM - SERIAL ALTITUDE INPUT................................................................ 11 FIGURE 7 UNIT DIMENSIONS ......................................................................................................... 15 ii Apollo SL70 Installation Manual Introduction SECTION 1 - INTRODUCTION ABOUT THIS MANUAL This manual describes the installation of the Apollo SL70 transponder . It is intended for use by persons certified by the Federal Aviation Administration (FAA) to install aircraft avionics. Section 1 Section 2 Section 3 Section 4 Provides an introduction to the Apollo SL70 unit. TSO certification information is also included in this section. Includes installation and checkout procedures. Includes complete specifications. Includes limitations for the equipment and installation. Appendix A Appendix B Appendix C Appendix E Includes troubleshooting information. Includes periodic maintenance requirements. Includes the environmental qualification form. Includes serial data protocol specifications. APOLLO SL70 DESCRIPTION The Apollo SL70 is a TSO-C74c, Class A2, mode A/C transponder. The SL70, in addition to providing replies to ATC interrogations, includes an altitude display and altitude hold function and user-friendly interface features including rotary knob squawk code selection, a VFR button, and built-in self-test and diagnostics. Apollo SL70 Installation Manual 1 Introduction Figure 1 SL70 Front Panel FEATURES small size 1.3 panel height full range input supply voltage high brightness LED display altitude display altitude hold function gray code or RS-232 serial data altitude input RS-232 altitude data output built-in self-test and diagnostics REGULATORY COMPLIANCE The Apollo SL70 is designed and tested to meet the following TSO:
FAA TSO-C74c, Class A2 The SL70 complies with the FCC requirements specified in:
CFR 47, Part 87, Aviation Services, Subpart D, Technical Requirements The SL70 software is designed and tested to RTCA/DO-178B, level C. Note: Un-authorized changes or modifications to the SL70 may void the compliance to regulatory agency requirements and authorization for continued equipment usage. 2 Apollo SL70 Installation Manual Introduction UNPACKING THE EQUIPMENT Carefully unpack the equipment. Visually inspect the package contents for any evidence of shipping damage. Retain all shipping containers and packaging material in case reshipment is necessary. PACKAGE CONTENTS As shipped from the UPS Aviation Technologies factory, the Apollo SL70 package includes most necessary items for installation other than supplies normally available at the installation shop, such as wire and coax cable, the antenna, or any optional switches. The items included in the package are listed in Table 1. Table 1 Package Contents Description Part #
Apollo SL70 Installation Kit, Part # 424-0306-xx 37 pin dsub connector shell 162-0103 Right angle coax plug 162-0043 Cable tie 202-0001 204-0037 Edge grommet 4-40 x SS pan head Phillips machine screw with lock 221-0400 washer 4-40 x flat head Phillips machine screw 9/16 OD flat washer Crimp contact for dsub, 20 to 24 awg wire 7/16 retaining ring Connector mounting bracket Mounting frame 3/32 hex driver 224-0404 240-0008 245-0022 265-0007 310-2295-00 310-5181-00 998-0048 Apollo SL70 Manual Kit, Part # 564-0072-xx 560-0401-00 560-0402-00 SL70 Users Manual SL70 Installation Manual Qty 1 1 2 6 10 2 1 37 1 1 1 1 1 1 OTHER REQUIRED MATERIALS In addition to the materials supplied with the SL70, the following is required. a suitable 2A circuit breaker an altitude data source either gray code or RS232 a standard transponder antenna Apollo SL70 Installation Manual 3 Introduction SPECIAL TOOLS REQUIRED Crimp Tool A crimp tool meeting MIL specification M22520/1-01 and a positioner are required to ensure consistent, reliable crimp contact connections for the rear 37 pin dsub connector. These tools are available from:
Astro Tool Corp. 21615 SW TV Highway Beaverton, OR 97006 Crimp tool:
Positioner:
Phone (503)642-9853 Fax (503)591-7766 Astro Tool part #615708 Astro Tool part #616356 4 Apollo SL70 Installation Manual Installation SECTION 2 - INSTALLATION This section describes the installation of the Apollo SL70 including mounting, wiring, and connections. A post installation check-out procedure is included at the end of this section. PRE-INSTALLATION INFORMATION Always follow good avionics installation practices per FAA Advisory Circulars AC 43.13-1B, 43.13-2A, or current FAA guidance. Follow the installation procedure in this section as it is presented for a successful installation. Read the entire section before beginning the procedure. Perform the post installation check-
out before closing the work area in case problems occur. INSTALLATION OVERVIEW A successful installation should start with careful planning including determination of mounting location for the SL70, antenna location and mounting, connections to an altitude data source, power, cable routing, and other required modifications. Once the mounting location has been determined, prepare the mounting frame for installation. If may be easier to complete the wiring harness and attach the connectors to the mounting frame prior to installing the mounting frame in the aircraft. INSTALLATION CONSIDERATIONS MOUNTING CONSIDERATIONS The SL70 is designed to mount in the avionics stack in the aircraft instrument panel within easy view and reach of the pilot. The standard package includes the mounting frame for ease of mounting, connections, and service of the unit. Allow an additional one inch clearance to the rear of the mounting frame for connections and cables. For typical installations, the SL70 does not require external cooling. When mounting the unit, leave a clearance of 1/8 to 1/4 inch between avionics to allow for air circulation. MINIMUM SYSTEM CONFIGURATION The SL70 requires connections to the following equipment as a minimum:
power input altitude data gray code or RS232 a standard transponder antenna ALTITUDE INPUT The SL70 can use either a standard altitude gray code input from an encoding altimeter or an RS-232 input from a serial encoder. For new installations, a serial encoder is recommended because it simplifies the wiring and is more reliable. The SL70 can detect failures on the RS-
232 input, thereby eliminating erroneous mode C altitude replies. Apollo SL70 Installation Manual 5 Installation The altitude source must be accurate to within 125 feet, 95% probability, and have a resolution of 100 feet (the serial input resolution may be better than 100feet). ANTENNA The antenna shall be a standard transponder quarter wave monopole antenna, such as the TED
#104-12 or Comant CI-101. EQUIPMENT MOUNTING Once the cable assemblies have been made, attach the 37 pin dsub and coaxial cable connectors to the rear connector mounting plate and the mounting frame as illustrated in Figure 2 and Figure 3. Route the wiring bundle as appropriate. The rear connector plate should be attached to the mounting frame before installing the frame in the instrument panel. The rear connector plate can be used to tie down the cable assemblies. Connect the shields on any shielded cables directly to the connector mounting plate. Figure 2 Mounting Frame Assembly 6 Apollo SL70 Installation Manual Installation Figure 3 Cable Routing Once the cable assemblies are complete and the connectors are attached to the mounting frame, install the mounting frame assembly in the aircraft instrument panel. Be sure to use low profile head screws so the unit will slide in and out freely. Attach the front of the mounting frame to the instrument panel. Use support brackets to attach the rear of the frame to the aircraft. UNIT INSTALLATION / REMOVAL To install the SL70 in the mounting frame, make sure the cam lock is rotated so the rear part is up, then slide the unit into the frame and tighten with the 3/32 hex tool. The unit will be pulled into the frame by the cam lock and the connectors will fully engage. To remove the SL70 from the mounting frame, use the hex tool and turn the tool CCW. The unit will be pushed out of the frame by the cam lock assembly. No special extraction tools are required. ELECTRICAL CONNECTIONS The SL70 installation kit includes a 37 pin dsub shell and crimp contacts. The crimp contacts are specified for 20 to 24 AWG wire. Make the crimp connections with a crimp tool as specified in the Special Tools Required section on page 4. All wires should be 20 to 24 AWG unless otherwise specified. Wiring diagrams are included on pages 10 and 11. Apollo SL70 Installation Manual 7 Installation POWER The SL70 is internally fused at 3 amps. A separate 2 amp circuit breaker or fuse should be installed for downline overload or short circuit protection. Make the power connections to the SL70 using 20 AWG wire. Note: Circuits should be protected in accordance with guidelines in AC 43.13-1B, chapter 11, section 4. ALTITUDE INPUT If using the gray code altitude input, connections can be made directly from the SL70 to the altitude source. Isolation diodes are included within the SL70. Make sure a common ground connection exists, or connect a ground wire between the source and the SL70. If using the RS-232 serial altitude input, make the connections as described in the following section. SERIAL INTERFACE The SL70 includes an RS-232 serial port which can be used for inputting or outputting altitude data. This is an optional connection if the altitude gray code input is used. When making serial connections to the SL70, use a shielded two or three conductor cable. Make the RxD, TxD, and serial ground connections on the 37 pin dsub connector. Connect the shield to the rear of the mounting frame on the connector plate. Complete serial interface specifications are included in Appendix E. DISCRETE INPUTS Remote Ident The ident input can be connected to a remotely mounted momentary switch to initiate the ident function the same as using the front panel IDENT button. When using the ident input, connect it to a remotely mounted momentary switch, and connect the other terminal of the switch to ground. Remote Standby The standby input is for use when the installation includes more than one transponder. When two transponders are installed, connect the standby input to a two position selector switch, with the common on the switch connected to ground. The SL70 will be in standby when the input is pulled low to ground. Suppresion Input The suppress input is used when installed with a DME that includes a suppression output. The transponder will be suppressed, or will not generate replies, when the input is driven high from the DME (or other source). To use the suppression input, connect it to the suppression output on a DME (or other appropriate suppression source). 8 Apollo SL70 Installation Manual Installation ANTENNA INSTALLATION AND CONNECTIONS The antenna should be mounted in a vertical position in an area on the bottom of the aircraft away from other antennas or landing gear. The antenna coax cable should be a double shielded low loss cable and must have a cable loss of < 3 dB, including connectors. A typical installation should have a cable loss of 1 to 2 dB. Several suitable coaxes are RG142B and RG400. The assembly of the rear panel coax connector included with the installation kit is illustrated in the following figure. Shield 0.250 Cable Solder Outer Shield to Connector STEP 1 STEP 2 STEP 3 STEP 4 Figure 4 Coax Cable Assembly 0.125 1.000
-Slide shrink tube over cable.
-Strip cable as shown. Insulation
.125 Shrink Tube
-Flare Outer Shield as Shown Cap Matching Ring Solder Center Conductor Solder Cap 2 Places
-Place cable in connector as shown placing inner shield inside connector.
-Flatten outer shield against connector.
-Solder outer shield to connector.
-Solder center conductor
-Slide matching ring into connector and around conductor.
-Attach cap.
-Solder cap into place, 2 Places.
-Shrink tube as shown. Apollo SL70 Installation Manual 9 Installation SL70 Transponder Power Ground C4 C2 C1 B4 B2 B1 A4 A2 A1 D4 Ground Ident Standby Suppress Ground TxD RxD Ground 1 2 15 34 16 32 14 33 12 31 13 35 30 10 29 19 37 5 4 3 2A Breaker
+
-
Avionics Power Altitude Encoder or Digitizer C4 C2 C1 B4 B2 B1 A4 A2 A1 D4 Ground GPS Unit RxD Ground Note 2 (Optional) Note 3 (Optional) Suppress return Remote Ident
(Optional) RS-232 Serial Altitude Output (Optional) Shielded Cable Chassis Ground Chassis Ground Coax Cable To Antenna Notes:
1. Select the gray code input in the setup mode when using the parallel gray code altitude input. 2. Use standby input to select between two transponders using a selector switch. Unit is in standby when input switched to ground. 3. Suppression input, typically connected to DME suppression output. Transponder is suppressed when input is high. Figure 5 Wiring Diagram - Gray Code Altitude Input 10 Apollo SL70 Installation Manual SL70 Transponder Power Ground C4 C2 C1 B4 B2 B1 A4 A2 A1 D4 Ground Ident Standby Suppress Ground TxD RxD Ground 1 2 15 34 16 32 14 33 12 31 13 35 30 10 29 19 37 5 4 3 Installation 2A Breaker
+
-
Avionics Power Remote Ident
(Optional) Note 2 (Optional) Note 3 (Optional) Suppress return RS-232 Serial Altitude Input Chassis Ground Shielded Cable Coax Cable Chassis Ground To Antenna Altitude Encoder or Serializer TxD Ground Notes:
1. Select altitude input in the setup mode when using RS-232 serial altitude input. 2. Use standby input to select between two transponders using a selector switch. Unit is in standby when input switched to ground. 3. Suppression input, typically connected to DME suppression output. Transponder is suppressed when input is high. Figure 6 Wiring Diagram - Serial Altitude Input Apollo SL70 Installation Manual 11 Installation POST INSTALLATION CHECKOUT Once the unit is installed, complete the checkout procedure to verify proper operation. Refer to the users guide for operating instructions. The steps that are not applicable to a particular installation may be skipped. A checkout log sheet is included on page 14 to fill out during the checkout procedure. Make a photocopy of the log sheet for ease of use if desired. Mounting / Wiring Check Verify that all cables are properly secured and shields are connected to the rear of the mounting frame. Check the movement of the aircraft controls to verify that there is not interference. TEST MODE CHECKOUT AND SETUP The SL70 has a built-in setup mode to simplify the checkout. To operate the SL70 in the setup mode, hold down the IDENT and ALT buttons while switching on the power. To return to normal operation, switch the power off, then back on. Altitude Input Source Selection The SL70 altitude input type must be selected. To select the altitude input type:
1. In test mode, rotate the LARGE knob to the SL70 CONF (SL70 Configuration) page, then rotate the SMALL knob to the ASRC (Altitude source) page. 2. Press IDENT (the altitude type field will start to flash), rotate the SMALL knob to select the altitude type, then press IDENT to save the selection. The altitude types that can be selected are:
GRAY ..................................... to use the parallel gray code input SER ........................................ to use the RS-232 serial altitude input RS-232 Baud Rate Selection If using the RS-232 serial interface, the baud rate must be selected to match the connected equipment. To select the baud rate:
1. In test mode, rotate the LARGE knob to the SL70 CONF (SL70 Configuration) page, then rotate the SMALL knob to the BAUD (baud rate) page. 2. Press IDENT (the baud rate field will start to flash), rotate the SMALL knob to select the desired baud rate, then press IDENT to save the selection. The baud rates available are 1200, 2400, 4800, 9600, and 19200. VFR Code Selection The VFR code used by the SL70 when pressing the VFR button can be selected as appropriate for the aircrafts operating area. To change the VFR code:
1. In test mode, rotate the LARGE knob to the SL70 CONF (SL70 Configuration) page, then rotate the SMALL knob to the VFR (VFR code selection) page. 2. Press IDENT (the first VFR code character will start to flash). 12 Apollo SL70 Installation Manual Installation 3. Rotate the SMALL knob to change the character, rotate the LARGE knob to move the cursor. 4. Press IDENT to save the selection. OPERATION / PERFORMANCE CHECKOUT Self Test The SL70 includes a self test that is executed every time the unit is turned on that checks the receiver and transmitter operation as well as other internal functions. Verify that the unit does not display a failure indication when turned on. Altitude Input Verify that the displayed altitude matches the altimeter pressure altitude (at 29.92). External Inputs If the external ident or standby inputs are connected, verify operation by:
a) Verify that the unit goes to standby when the external standby input is pulled low. b) Verify that the ident LED turns on when the external ident button is pressed (must be in the ON or ALT modes). Performance (Ramp) Test After installation, the transponder should be tested as specified in Appendix F of CFR 14 part 43, to AC 43-6A, and/or other appropriate regulations. The test is typically done as a ramp test using a transponder ramp test set, such as the IFR ATC-600A. The ramp test includes checks as follows. reply frequency Reference part 43 Appendix F:
a) b) suppression c) d) Reference AC 43-6A:
altitude reporting receiver sensitivity reply RF output power Apollo SL70 Installation Manual 13 Installation APOLLO SL70 POST-INSTALLATION CHECKOUT LOG Date: ___/___/___ By: _______________ CONFIGURATION INFORMATION:
Apollo SL70 430-6090-____ Mod ___ Serial #_______________ TEST MODE CHECKOUT AND SETUP:
Self Test:
[ ] Pass
[ ] Fail Altitude source:
[ ] Gray code (GRAY)
[ ] Serial RS-232 (SER) OPERATION / PERFORMANCE CHECK:
Altitude data (on display):
[ ] Pass External inputs:
[ ] Remote ident checked [ ] N/A
[ ] External standby [ ] N/A COMMENTS:
RS-232 baud rate: _________ VFR Code: ________ Performance verification:
[ ] Pass 14 Apollo SL70 Installation Manual Specifications SECTION 3 - SPECIFICATIONS This section specifications for the Apollo SL70. includes detailed electrical, physical, environmental, and performance ELECTRICAL Input voltage .............................................10VDC to 35VDC, reverse polarity protected Input current..............................................500mA typical, 1.4A max at 14VDC 270mA typical, 660mA max at 28VDC Input power...............................................7 watts typical (8 pulse reply, 200 replies / second) 20 watts max (12 pulse reply, 1200 replies / second) 5.8 watts standby Internal fuse ..............................................3 amp slow blow (UPS Aviation Technologies
#S172-0007-012) Memory backup ........................................Internal EEPROM PHYSICAL Height .......................................................1.30 inches (3.30 cm) Width ........................................................6.25 inches (15.88 cm) Depth ........................................................11.452 inches (29.09cm) behind panel, including mounting frame and connectors Weight (with mounting frame) .................2.64 lb. (1.2 kg) Required clearance....................................Allow 3 inches behind unit for connector and cable clearance 0.648 Mounting Holes (8x) 11.452 10.420 1.038 0.219 0.862 1.300 0.375 3.625 3.025 1.750 1.625 6.250 1.300 Figure 7 Unit Dimensions Apollo SL70 Installation Manual 15 Specifications ENVIRONMENTAL The Apollo SL70 is designed and tested to meet appropriate categories of RTCA/DO-160D. The Environmental Qualification Form is included in Appendix C. Operating temperature.............................. -20C to +55C Storage temperature.................................. -55C to +85C Temperature variation .............................. 2C per minute Humidity................................................... 95% at 50C for 6 hours (2 day cycle) Maximum altitude .................................... 25,000 feet Cooling..................................................... Not required ALTITUDE INPUT 10 bit gray code ........................................ Uses 10 bit gray code altitude data, includes isolation diodes. Range: -1000feet to 63,000 feet On: <= 3.5 volts, Off: open Serial input ............................................... Uses RS-232 serial data input (See Appendix E Serial Interface Specifications) Note: The altitude data input type must be selected using the setup function during the post installation checkout. DISCRETE INPUTS Remote Ident ............................................ Input pulled low momentarily to initiate ident transmission (same function as front panel button) On: <= 3.5 volts, Off: open Standby input............................................ Input pulled low to disable the transponder (will not generate replies) On: <= 3.5 volts, Off: open Suppression input ..................................... Input pulled high to initiate suppression typically connected to DME suppression output Suppressed: >= 5.0 volts;
Not suppressed: < 2.5 volts (or open) SERIAL INTERFACE RS-232...................................................... Defined in Appendix E Serial Interface Specifications 16 Apollo SL70 Installation Manual Specifications TRANSPONDER PERFORMANCE TSO...........................................................TSO-C74c TSO Class.................................................2A Warm-up...................................................none required Receiver Frequency ..................................1030 MHz Sensitivity (MTL) .....................................72 dBm Dynamic Range.........................................> 50 dB Side Lobe Suppression .............................2 pulse (P1,P2) Transmitter Frequency..............................1090 MHz +/- 120 kHz Transmitter Power ....................................250 watts minimum, 325 watts typical Reply rate..................................................1200 / second Mode A Capability ...................................4096 codes plus SPI ident pulse Mode C Capability....................................-1000 to 63,000 feet, 100 foot increments, from either gray code or RS-232 serial inputs ANTENNA REQUIREMENTS The SL70 requires a standard transponder quarter wave monopole antenna, such as the TED
#104-12 or Comant CI-101. Apollo SL70 Installation Manual 17 Specifications Pin #
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 I/O Connection I I O I O O O I I I
--
I I I I I
--
--
I O I O
--
--
I I
--
--
I
--
I I I I I
--
--
Power +
Power ground Serial ground RxD TxD reserved reserved reserved reserved Ident NC A4 A1 B2 C4 C1 reserved reserved Suppress NC reserved reserved NC Ground reserved reserved Ground Ground Standby Ground A2 B4 B1 C2 D4 reserved Ground 1 20 Table 2 Rear Connector Pinout Function main DC power input main DC power ground RS-232 serial ground RS-232 serial data input RS-232 serial data output remote ident input no connection A4 altitude gray code input A1 altitude gray code input B2 altitude gray code input C4 altitude gray code input C1 altitude gray code input remote suppression input no connection no connection remote standby input A2 altitude gray code input B4 altitude gray code input B1 altitude gray code input C2 altitude gray code input D4 altitude gray code input 19 37 Viewed from rear of unit 18 Apollo SL70 Installation Manual Limitations SECTION 4 - LIMITATIONS INSTALLATION Aircraft installation must be made in accordance with this installation manual and applicable FAA FARs and ACs. OPERATIONAL The SL70 must be operated within the limitations as follows, or by other regulatory guidance as appropriate. 1. The altitude should be verified by comparing the pressure altitude display to the aircraft altimeter relative to barometric setting of 29.92. 2. The transponder is to be operated in compliance with CFR 14 section 91.215 for ATC transponder and altitude reporting equipment. 3. The transponder must be tested as specified in CFR 14 section 91.413 within the previous 24 months. Apollo SL70 Installation Manual 19 Limitations NOTES 20 Apollo SL70 Installation Manual APPENDIX A - TROUBLESHOOTING This appendix provides information to assist troubleshooting if problems occur after completing the installation. Use Table 3 to assist in troubleshooting. Troubleshooting Problem The SL70 does not power on. The altitude is not correct. Table 3 Troubleshooting Guide Cause The unit is not getting power. The unit is not getting the correct altitude. The altitude display is ---
The unit is not getting an altitude, or the altitude is invalid. The unit fails the start-up test. The unit does not generate replies. TX fails. Other failure. The unit is in standby. The unit is not receiving interrogation signals. No interrogation signal available. Solution Check power connections, breakers, and main avionics switch. If the gray code inputs are used, check all connections from the altitude source and/or verify the altitude source. If the serial altitude input is used, check for the correct baud rate and connections to the altitude source. Check the connections to the altitude source. Check the altitude source to make sure it is operating correctly. Check antenna connections. The unit may need repair. The unit must be in either the On or Alt modes to generate replies. Check the antenna connections. If the unit does not Fail the receive test, then check antenna connections. Need to either use a ramp test set or climb to altitude where ATC radar service is available. Apollo SL70 Installation Manual 21 Troubleshooting CONTACTING THE FACTORY FOR ASSISTANCE If the Apollo SL70 unit fails to operate despite troubleshooting efforts, contact the UPS Aviation Technologies factory for assistance. UPS Aviation Technologies 2345 Turner Rd. S.E. Salem, Oregon 97302 U.S.A. Phone (503)581-8101 or 1-800-525-6726 Be prepared to offer the following information about the installation:
Installation configuration (accessories, antenna, ...) Model number, part number with mod levels, and serial number Software versions (The software versions can be displayed in the setup mode by rotating the LARGE knob to the SW VER page, and rotating the SMALL knob to display the microcontroller and FPGA versions.) Description of problem Efforts made to isolate the problem 22 Apollo SL70 Installation Manual Periodic Maintenance APPENDIX B - PERIODIC MAINTENANCE The Apollo SL70 is designed to not require any regular general maintenance except as included in this section. BIENNIAL CHECK The transponder must be tested within the previous 24 months as specified in 91.413 of the FAA regulations. No other periodic maintenance is required. CLEANING THE FRONT PANEL The front bezel, keypad, and display can be cleaned with a soft cotton cloth dampened with clean water. DO NOT use any chemical cleaning agents. Extreme care must be taken to avoid scratching the surface of the display. Apollo SL70 Installation Manual 23 Periodic Maintenance NOTES 24 Apollo SL70 Installation Manual Environmental Qualifications APPENDIX C - ENVIRONMENTAL QUALIFICATIONS The Apollo SL70 has been tested to the following environmental categories per procedures defined in RTCA/DO-160D. Nomenclature: Apollo SL70 Part No.: 430-6090-xxx TSO No.: TSO_C74c Conditions Temperature and Altitude In-flight Loss of Cooling Altitude Decompression Overpressure Temperature Variation Humidity Operational Shocks and Crash Safety Vibration Explosion Proofness Waterproofness Fluids Susceptibility Sand and Dust Fungus Resistance Salt Spray Magnetic Effect Power Input Voltage Spike Audio Frequency Conducted Susceptibility Power Inputs Induced Signal Susceptibility Radio Frequency Susceptibility
(Radiated and Conducted) Emission of Radio Frequency Energy Lightning Induced Transient Susceptibility Lightning Direct Effects Icing Electrostatic Discharge (ESD) Remarks:
Environmental Qualification Form Manufacturer:
UPS Aviation Technologies 2345 Turner Road S.E. Salem, Oregon 97302 Section Description of Conducted Tests 4.0 4.5.4 4.6.1 4.6.2 4.6.3 5.0 6.0 7 8.0 9.0 10.0 11.0 12.0 13.0 14.0 15.0 16.0 17.0 18.0 19.0 20 21 22.0 23.0 24.0 25.0 Equipment tested to Category B1 with ....... No cooling required Equipment tested to 25,000 feet Equipment tested for decompression to 35,000 feet Equipment tested for overpressure Equipment tested to Category C, 2C/min Equipment tested to Category A, standard humidity environment Equipment tested for both operational and crash safety shocks. (Equipment operates normally after both the crash safety shocks.) Equipment tested without shock mounts to Categories S(M) Equipment identified as Category X, no test required Equipment identified as Category X, no test required Equipment identified as Category X, no test required Equipment identified as Category X, no test required Equipment identified as Category X, no test required Equipment identified as Category X, no test required Equipment is Class Z Equipment tested to Categories A (28volt systems) & B (14 and 28 volt systems) Equipment tested to Category A Equipment tested to Categories A & B Equipment tested to Category Z Equipment tested to Category V Equipment tested to Category M Equipment tested to A3 and B2 Equipment identified as Category X, no test required Equipment identified as Category X, no test required Equipment tested to Category A Apollo SL70 Installation Manual 25 Environmental Qualifications NOTES 26 Apollo SL70 Installation Manual Serial Data Protocol APPENDIX E - SERIAL DATA PROTOCOL This appendix includes the RS-232 serial port interface specifications. ALTITUDE INPUT / OUTPUT The SL70 will output altitude data whenever it is available, either from the gray code or serial input. The SL70 will accept altitude input data when the serial altitude data source is selected. The format for the altitude input and output data is as follows. Baud rate................................1200 to 19200 Data bits.................................8 Stop bits.................................1 Parity......................................none Message length ......................17 characters Expected input rate................once per second Output rate.............................once per second Byte 1 2 3 4 5 6-10 11 12 13-14 15-16 Data Format
#
A L
+ or -
ddddd T
+ or -
dd dd 17
<CR>
Table 4 Altitude Data Format Description ASCII # (023h) ASCII A (041h) ASCII L (04Ch) ASCII space (020h) Altitude sign: ASCII + or - (02Bh or 02Dh) Altitude in feet, right justified, with leading zeros ASCII T (054h) Temperature sign: ASCII + or - (02Bh or 02Dh) Altimeter temperature Checksum of bytes 1 through 14, computed in hex, output is ASCII format (i.e., FA hex) ASCII carriage return (0Dh) The SL70 will interpret several altitude input codes as status or error codes, in the place of the altitude data, as follows.
-09980 ................................Encoder heater not ready, expected during encoder warm-
up or if there is a loss of signal from the encoder. The SL70 will reply with only framing pulses to mode C interrogations. Apollo SL70 Installation Manual 27 Serial Data Protocol
-09981................................ Possible hardware problem, expected from the encoder indicating a temperature above normal. The SL70 will reply with only framing pulses to mode C interrogations.
-09982................................ Altitude out of range, expected from the encoder indicating that the altitude is out of a valid range. The SL70 will reply with only framing pulses to mode C interrogations. When the gray code input is selected, the SL70 will output the -09982 error code in place of the altitude data if an undefined altitude input is detected on the gray code input. 28 Apollo SL70 Installation Manual NOTES Serial Data Protocol Apollo SL70 Installation Manual 29
1 | Operation manual | Users Manual | 353.58 KiB |
800.525.6726 U.S.A. Toll Free Canada Toll Free 800.654.3415 503.391.3411 International FAX 503.364.2138 Visit our web page at http://www.upsat.com Apollo Mode C Transponder Model SL70 Operation Manual Using Altitude Hold Altitude Hold helps you maintain a constant altitude. The current pressure altitude is stored as a reference and is the displayed value unless Altitude Hold is activated. The hold altitude is displayed in 100-foot increments. The displayed altitude is the same as is sent for Mode C interrogation replies. When the HLD button is pressed, the altitude display will be set to +000. The altitude display values will increase/decrease as the aircraft changes altitude. The altitude display will flash when the aircraft change in altitude exceeds the selected threshold. Setting the Hold Altitude 1. Press the HLD button to set the current altitude as the hold altitude. The LED above the HLD button will light to indicate Altitude Hold is active. 2. The Altitude display now shows a value that is relative to the hold altitude in 100-foot increments. A displayed value of +001 means you are 100 ft above the hold altitude. Setting the Altitude Hold Buffer 1. Set the Altitude Hold Buffer value by pressing the HLD button for two seconds, or longer. Select a value between 200 and 2500 feet. The factory default value is 300 feet. The value is retained when the SL70 is turned off. 2. Turn the SMALL knob to change the buffer value, such as 02. Press HLD again to save the value. Displays Squawk Codes The four-digit squawk code is shown on the left side of the display. Altitude The Altitude display is used to show the pressure altitude, Hold Altitude, and Hold Altitude buffer with 100 ft resolution. 1999 by UPS Aviation Technologies, Inc. All rights reserved. Printed in the U.S.A. UPS Aviation Technologies, Inc. 2345 Turner Road, S.E. Salem, OR 97302 August 1999 560-0401-00 Apollo SL70 The Apollo SL70 Mode C Transponder complements the Apollo SL series of slimline avionics. The SL70 provides Mode A/C functionality certified to TSO-C74c Class 2A meeting VFR and IFR requirements, operates on 10-35 VDC, includes squawk code display and selection, standby, altitude, and ident operation. All of these features are contained in the space-saving 1.3H x 6.25W form factor, with bright easy-to-read LED characters, and user-
friendly operation. A photocell on the front of the SL70 adjusts the LED intensity for ambient light conditions. The SL70 will automatically test its receive function if no interrogations have been received in the last 30 seconds. Knobs A single knob on the left side controls power on/off. Rotate the knob clockwise to turn transponder power on. Rotate the knob counterclockwise to turn power off. Dual concentric knobs on the right side are used to select squawk codes and change altitude values. Turning the large, outer knob moves the cursor to allow editing of the selected character. Turning the small, inner knob changes values. Pushbuttons Press the pushbutton once to activate the selected operation. An LED above each pushbutton will light when that button is pressed. IDENT Press the IDENT button once to reply with an identifying squawk code, Ident mode. In Ident mode, the Reply LED will be lighted for 20 seconds. The Reply (Ident) LED will also flash when the SL70 generates transponder replies. SBY Press SBY to place the transponder in Standby mode. The SL70 is on, but no information will be transmitted. ON Press for Mode A operation. The SL70 is on and will transmit its squawk code when interrogated. ALT Press for Mode C operation. The SL70 is on and will transmit its squawk code and altitude when interrogated. VFR Press VFR once to set the VFR squawk code. Press VFR a second time to toggle between the VFR squawk code and the previously entered code. HLD Press to enable/disable altitude hold. The LED above the HLD button is lighted when altitude hold is enabled. Selecting a Squawk Code The selected squawk code will always be in use. As you change a squawk code, the original code will be sent until you are finished selecting the new code. When changing a code, the display will stop flashing and selection is stopped if the controls are not used for three seconds or more. Pressing any pushbutton will also end code selection. The squawk code is automatically reset to the VFR code when the SL70 is turned back on. 1. Rotate the LARGE knob clockwise one position. The first character of the squawk code will flash. 2. Rotate the SMALL knob to the desired number for the first digit. 3. Rotate the LARGE knob to move the cursor to the next desired digit. Turn the SMALL knob to select the desired number. 4. Repeat step 3 for each of the desired digits. 5. After the last digit is selected, rotate the LARGE knob clockwise one more position. The display will stop flashing and the new code will be sent. Special Squawk Codes Special Squawk Codes Special Squawk Codes Special Squawk Codes 1200 Default VFR code in the USA. 7500 - Hijacking 7600 Loss of communications 7700 Emergency See the Airmans Information Manual for more information about squawk codes.
1 | Brady label info | ID Label/Location Info | 142.80 KiB |
MASTER MATERIALS CHART master materials chart master materials chart maste MMASTER MATERIALS CHART B-12 Acetate Cloth Beige Pre-Printed Brady Material # Material B-11 Polyester Color White &
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-20F to 221F
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(-40C to 100C) Thermal Transfer B-420 Polyester White Thermal Transfer Low profile labeling. UL recognized/CSA accepted B-421 Polyimide White Thermal Transfer B-422 Polyester White
-40F to 248F
(-40C to 120C) Thermal Transfer TLS2200 B-423 Polyester White
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(-40C to 120C) Thermal Transfer TLS2200 Top- or bottom- side board application for SMT or Top-side in mixed processes. Low profile construction for SMT/Through hole processing. Gloss white film with permanent acrylic-based adhesive. Designed for rough surfaces and applications where increased adhesion is required. Electronic PCB and component; bar code label and rating plates. UL recognized/CSA accepted; 2 mil adhesive, recommended for application on textured surfaces Thermal transfer-printable with a permanent acrylic adhesive. Electronic PCB and component;bar code label and rating plates. UL recognized/CSA accepted.
-40F to 158F
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-40F to 200F
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(-40C to 70C) Print Technology Thermal Transfer TLS2200 B-425 Polyolefin White Thermal Transfer
-40F to 194F
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-40F to 158F
(-40C to 70C) Thermal Transfer TLS2200 B-428 Metallized Polyester Silver
-40F to 176F
(-40C to 80C) Thermal Transfer TLS2200 B-430 Polyester Clear
-40F to 212F
(-40C to 100C) Thermal Transfer TLS2200 B-432 Polyester Clear
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(-40C to 100C) Thermal Transfer B-433 Polyester White
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(-40C to 120C) Thermal Transfer B-434 Metallized Polyester Silver
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(-40C to 90C) Thermal Transfer B-435 Metallized Polyester Silver
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(-65C to 135C) Thermal Transfer B-438 Metallized Polyester Silver
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(-40C to 260C)
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-40F to248F
(-40C to 120C)
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-40F to 150F
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-40F to 200F
(-40C to 155C)
-40F to 311F
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-40F to 311F
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-40F to 221F
(-40C to 105C)
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-40F to 266F
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87958. Applications requiring self-extinguishing, easily printed cable or wire identification. Aerospace and military cable marking. Resistant to UV light and weathering; not printable. Overlaminate for labels where resistance to UV light and weathering is necessary. 270 MS-901-i x/reference index/reference index/reference index/reference MASTER MATERIALS CHART CONTINUED Brady Material # Material B-642 Tedlar Color White/
Transparent Temp. Range
-40F to 266F
(-40C to 130C) Print Technology Dot Matrix Thermal Transfer B-652 Polyimide Amber B-654 Polyimide Amber B-658 Polyimide Amber B-673 Metallized Polyester Silver
-40F to 572F
(-40C to 300C)
*5 Minutes Up to 320F
(160C) Dot Matrix ID PRO Plus LS2000 Laser N.A.
-40F to 572F
(-40C to 300C)
*5 Minutes
-40F to 311F
(-40C to 155C) Dot Matrix Laser Dot Matrix Properties & Applications Applications requiring flame-retardant identification. Self-
laminating, wire and cable marking. Excellent abrasion and smudge resistance. Designed to resist soldering fluxes, cleaning solvents and molten solder dips used in circuit board manufacturing. bar code-printable. Recommended for use on surface-mount technology applications and underside of circuit boards. Masking material. Removes cleanly without adhesive residue after processing through vapor phase or wave solder cycle. Designed to remove cleanly after exposure to high temperatures and solvents. Recommended for use on solder-side of circuit boards, EPROM and SMT applications. Removable after high-temperature exposure. UV opaque; good chemical resistance. Designed for EPROM labeling where removability and opacity are important. B-691 Polypropylene Transparent
-20F to 200F
(-29C to 93C) Custom No Stock Parts Biaxially oriented film. Excellent clarity and flexibility; not printable. Clear protective overlaminates for most labels. B-693 B-702 Metallized Polyester Vinyl-Coated Polyester Silver White
-40F to 248F
(-40C to 120C) Dot Matrix Low-cost metallized identification or rating plate material. It exhibits good smudge, solvent, and heat resistance.
-40F to 221F
(-40C to 105C) Pre-Printed Thermal Transfer High adhesion; good conformability; low profile; resistant to oil and mild solvents. Environments containing oil or mild solvents. Ideal for wire marking. B-707 Polyester White
-40F to 267F
(-40C to 130C) Laser B-708 Vinyl White
-40F to 150F
(-40C to 66C) Pre-Printed B-709 Polyester White
-40F to 267F
(-40C to 130C) Laser B-712 Polyester Clear B-722 Polyester Clear
-40F to 200F
(-40C to 93C)
-40F to 200F
(-40C to 93C) Laser Laser Electronic component labeling; general identification. Rough surface application; Stronger bond to low surface energy plastics. UL recognized. Good strength and conformability. Resistant to oil, mild solvents and water. Environments containing oil, mild solvents or water. Indoor or outdoor use. Excellent for cable identification. Applications requiring general purpose permanent and temporary labeling or marking with printable or write-on properties. Leaves no adhesive residue when removed from PC board. Good EPROM label. Electronic component labeling; general identification. Rough surface application. Stronger bond to low surface energy plastics. Permanent acrylic-based adhesive. Design for rating and serial plates using alphanumerics, bar codes, graphic symbols, and logos that require name plate quality. Withstands numerous solvents and can be applied to variable surfaces. B-725 Vinyl White Up to 176F
(Up to 80C) Custom No Stock Parts Good conformability; dielectric strength. Electrical-grade cable markers. B-737 Tedlar White or Yellow
-40F to 266F
(-40C to 130C) Laser Self-extinguishing. Meets MIL-M-87958. Applications requiring self-extinguishing, easily printed cable or wire identification. Aerospace and military cable marking. Repositionable. MS-901-i t r a h c s l a i r e t a m r e t s a m 271 m a s t e r m a t e r i a l s c h a r t m a s t e r m a t e r i a l s c h a r t MASTER MATERIALS CHART CONTINUED Brady Material # Material B-747 Polyester Color White or Yellow Temp. Range
-40F to 267F
(-40C to 130C) Print Technology Laser B-759 Paper White B-773 Polyester Silver
-40F to 158F
(-40C to 70C)
-40F to 248F
(-40C to 120C) Laser Laser Properties & Applications Electronic PCB component, bar code labels. Excellent solvent and smudge resistance; and equipment labeling high-resolutio and high temperature performance;
available in white only; UL/CSA Permanent adhesive; smudge resistant. Applications requiring economical, general purpose label. Bar code-
printable. Excellent toner adhesion. Permanent acrylic adhesive. Designed for rating and serial plate that utilize alphanumeric, graphic symbols and logos. Electronic component marking. Designed to withstand numerous solvents and variable temperatures. Adheres to a variety of surfaces. UL recognized/CSA approved. B-799 Nylon Cloth White
-40F to 193F
(-40C to 90C) Laser Recommended for applications requiring permanent wire marking or general labeling. B-917 Aluminum Foil Silver
-40F to 266F
(-40C to 130C) Dot Matrix B-953 Polyester White
-40F to 311F
(-40C to 155C) Pre-Printed Printable; resistant to solvents, high temperatures. Identification and serialized labels, rating plates, general labeling. Full hard aluminum. Resistant to high temperatures and solvents. Can accept extremely small print. Ideal for identifying small electrical, electronic components and parts labeling. B-966 Polyester Clear
-40F to 266F
(-40C to 130C) Ink Jet Release-coated surface. Not printable. Overlaminate for PermaShield labels. Transparent/durable. B-969 Metallized Polyester Silver
-40F to 311F
(-40C to 155C) Dot Matrix ID PRO Plus LS2000 Print-receptive topcoat. Rating or serial plate, product information property identification, warranty labels and inventory control labels, electronic component marking. Suitable for printing. UL recognized/CSA approved. B-994 Metallized Polyester Silver
-40F to 266F
(-40C to 130C) Dot Matrix Write-on coating. Rating or serial plate, product information property identification, warranty labels and inventory control labels. Adheres well to rough surfaces. Suitable for printing. UL recognized. B-999 Polyester Clear
-320F to 320F
(-200C to 160C) Custom No Stock Parts Printable. Aircraft tubing identification. Ideal for use as fluid wire tape. 272 MS-901-i
1 | Label specifications | ID Label/Location Info | 13.37 KiB |
II MORROW COMPONENT SPECIFICATION Last Maintained: 6/14/99 Page 1 of 3 RELEASED II Morrow Part Number: 565-9000-XX Rev:
Description: LABEL STK,POLYES,THRM XFR,PERM ADH VENDOR NAME BRADY VENDOR PART NUMBER SEE SPEC STATUS PRIMARY SINGLE/SOLE SOURCED FIRST USED IN: GENERAL Additional Information:
ORDERING INFORMATION UNDER MECHANICAL SPECIFICATION. TECHNICAL APPROVALS PROJECT ENGINEER : J CONNELLY MANUFACTURING ENG : J CONNELLY COMPONENT ENGINEER: J KREBS Alternate Parts:
Associated Parts:
UPS CONFIDENTIAL - DO NOT DUPLICATE OR DISTRIBUTE II MORROW COMPONENT SPECIFICATION Last Maintained: 6/14/99 Page 2 of 3 RELEASED II Morrow Part Number: 565-9000-XX Rev:
Description: LABEL STK,POLYES,THRM XFR,PERM ADH Electrical Specifications N/A Physical Specifications APPROVED CLEANING : N/A APPROVED SOLDERING : N/A PACKAGING : SUPPLIED ON 3" I.D. ROLLS SPECIAL HANDLING: MUST BE KEEP DUST FREE UPS CONFIDENTIAL - DO NOT DUPLICATE OR DISTRIBUTE II MORROW COMPONENT SPECIFICATION Last Maintained: 6/14/99 Page 3 of 3 RELEASED II Morrow Part Number: 565-9000-XX Rev:
Description: LABEL STK,POLYES,THRM XFR,PERM ADH Mechanical Specifications FAMILY : LABEL, THERMAL TRANSFER PRINTABLE TYPE : GENERAL IDENTIFICATION MATERIAL : POLYESTER ADHESIVE : PERMANENT ACRYLIC (PA) PRINT WIDTH : 3.27 INCHES (MAX) WEB WIDTH : 3.35 INCHES (MAX) TEMPERATURE RANGE : -40 TO 120 DEG C HIGH PERFORMACE MATERIAL DESIGNED FOR USE IN LABELING APPLICATIONS REQUIRING EXCELLENT SOLVENT RESISTANCE AND PRINT PERFORMANCE. UL RECOGNIZED/CSA CERTIFIED. REQUIRES R6002 SERIES BRADY THERMAL TRANSFER RIBBON ORDERING INFORMATION:
II MORROW P/N DESCRIPTION
(MANUFACTURER PART NUMBER COLOR QUANTITY/ROLL) 565-9000-01 LBL STK,POLYES,PA,1.875X.833,WHT THT-1.875 X .833 B-423 WHT WHITE 2,500 BRADY ASSIGNED P/N 10C9602491 565-9000-02 LBL STK,POLYES,PA,1.875X.833,YEL THT-1.875 X .833 B-423 YEL YELLOW 2,500 565-9000-03 LBL STK,POLYES,PA,1.50X.50,WHT THT-37-423-10 WHITE 10,000 565-9000-04 LBL STK,POLYES,PA,1.00X.50,WHT THT-5-423-10 WHITE 10,000 565-9000-05 LBL STK,POLYES,PA,1.50X.25,WHT THT-45-423-10 WHITE 10,000 565-9000-06 LBL STK,POLYES,PA,2.75X2.75,WHT THT-2.75 X 2.75 B-423 WHT WHITE 1,000 BRADY ASSIGNED P/N 10C9602918 565-9000-07 LBL STK,POLYES,PA,2.00X2.00,WHT THT-2.00 X 2.00 B-423 WHT WHITE 2,500 565-9000-08 LBL STK,POLYES,PA,3.00X2.00,WHT THT-19-423-1 WHITE 1,000 565-9000-09 LBL STK,POLYES,PA,1.5X.5,3 SET,WHT THT-1.5 X.5,SET OF 3,B-423,WHT WHITE 1,500 SETS 565-9000-10 LBL STK,POLYES,PA,.375X.375,WHT THT-38-423-10 WHITE 10,000 565-9000-11 LBL STK,POLYES,PA,2.00X.50,WHT THT-53-423-3 WHITE 3,000 565-9000-12 LBL STK,POLYES,PA,.75X.25,WHT THT-1-423-10 WHITE 10,000 565-9000-13 LBL STK,POLYES,PA,.50X.20,WHT THT-36-423-10 WHITE 10,000 565-9000-14 LBL STK,POLYES,PA,3.00X1.00,WHT THT-18-423-3 WHITE 3,000 565-9000-15 LBL STK,POLYES,PA,3X6,MULTI-8,WHT 10C9700853 WHITE 500 565-9000-16 LBL STK,POLYES,PA,3X7.25,MULTI-11,WHT THT-423 WHITE 500 565-9000-17 LBL STK,POLYES,PA,0.25X0.25,WHT THT-11-423 WHITE 10,000 UPS CONFIDENTIAL - DO NOT DUPLICATE OR DISTRIBUTE
frequency | equipment class | purpose | ||
---|---|---|---|---|
1 | 1999-10-26 | 1090 ~ 1090 | TNB - Licensed Non-Broadcast Station Transmitter | Original Equipment |
app s | Applicant Information | |||||
---|---|---|---|---|---|---|
1 | Effective |
1999-10-26
|
||||
1 | Applicant's complete, legal business name |
Garmin AT, Inc.
|
||||
1 | FCC Registration Number (FRN) |
0001549476
|
||||
1 | Physical Address |
2345 Turner Road SE
|
||||
1 |
Salem, 97302
|
|||||
1 |
United States
|
|||||
app s | TCB Information | |||||
n/a | ||||||
app s | FCC ID | |||||
1 | Grantee Code |
EOJ
|
||||
1 | Equipment Product Code |
SL-70
|
||||
app s | Person at the applicant's address to receive grant or for contact | |||||
1 | Name |
G****** C****
|
||||
1 | Title |
RF Engineering Manager
|
||||
1 | Telephone Number |
503-3********
|
||||
1 | Fax Number |
503-3********
|
||||
1 |
g******@garmin.com
|
|||||
app s | Technical Contact | |||||
1 | Firm Name |
CKC Laboratories, Inc.
|
||||
1 | Name |
T****** P******
|
||||
1 | Physical Address |
5473A Clouds Rest
|
||||
1 |
Mariposa, California 95338
|
|||||
1 |
United States
|
|||||
1 | Telephone Number |
1-800********
|
||||
1 | Fax Number |
209-9********
|
||||
1 |
t******@ckc.com
|
|||||
app s | Non Technical Contact | |||||
1 | Firm Name |
CKC Laboratories, Inc.
|
||||
1 | Name |
J******** W******
|
||||
1 | Physical Address |
5473A Clouds Rest
|
||||
1 |
Mariposa, California 95338
|
|||||
1 |
United States
|
|||||
1 | Telephone Number |
1-800********
|
||||
1 | Fax Number |
209-9********
|
||||
1 |
j******@ckc.com
|
|||||
app s | Confidentiality (long or short term) | |||||
1 | Does this application include a request for confidentiality for any portion(s) of the data contained in this application pursuant to 47 CFR § 0.459 of the Commission Rules?: | Yes | ||||
1 | Long-Term Confidentiality Does this application include a request for confidentiality for any portion(s) of the data contained in this application pursuant to 47 CFR § 0.459 of the Commission Rules?: | No | ||||
if no date is supplied, the release date will be set to 45 calendar days past the date of grant. | ||||||
app s | Cognitive Radio & Software Defined Radio, Class, etc | |||||
1 | Is this application for software defined/cognitive radio authorization? | No | ||||
1 | Equipment Class | TNB - Licensed Non-Broadcast Station Transmitter | ||||
1 | Description of product as it is marketed: (NOTE: This text will appear below the equipment class on the grant) | Mode C Transponder | ||||
1 | Related OET KnowledgeDataBase Inquiry: Is there a KDB inquiry associated with this application? | No | ||||
1 | Modular Equipment Type | Does not apply | ||||
1 | Purpose / Application is for | Original Equipment | ||||
1 | Composite Equipment: Is the equipment in this application a composite device subject to an additional equipment authorization? | No | ||||
1 | Related Equipment: Is the equipment in this application part of a system that operates with, or is marketed with, another device that requires an equipment authorization? | No | ||||
1 | Is there an equipment authorization waiver associated with this application? | No | ||||
1 | If there is an equipment authorization waiver associated with this application, has the associated waiver been approved and all information uploaded? | No | ||||
app s | Test Firm Name and Contact Information | |||||
1 | Firm Name |
CKC Laboratories, Inc.
|
||||
1 | Name |
S******** B********
|
||||
1 | Telephone Number |
209-9******** Extension:
|
||||
1 | Fax Number |
866-7********
|
||||
1 |
r******@ckc.com
|
|||||
Equipment Specifications | |||||||||||||||||||||||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Line | Rule Parts | Grant Notes | Lower Frequency | Upper Frequency | Power Output | Tolerance | Emission Designator | Microprocessor Number | |||||||||||||||||||||||||||||||||
1 | 1 | 87 | 1090.00000000 | 1090.00000000 | 370.0000000 | 100.0000000000 ppm | 14MOM1D |
some individual PII (Personally Identifiable Information) available on the public forms may be redacted, original source may include additional details
This product uses the FCC Data API but is not endorsed or certified by the FCC