TECHNISONIC INDUSTRIES LIMITED
www.til.ca
TDFM-7000 Installation & Operating Instructions
TiL 05RE375 Rev n/c Issue 13
3-7
QTY ITEM PART
NUMBER
DESCRIPTION
SPEC
MATERIAL
1 1
TDFM-7000 VHF/UHF/800
COMMUNICATIONS
TRANSCEIVER.
TECHNISONIC INDUSTRIES LTD
1
2
CI-292-3,-4
VHF ANTENNA, 136 TO 174 MHZ
COMANT INDUSTRIES
1
3
CI-275
UHFLO ANTENNA, 403 TO 470 MHZ
COMANT INDUSTRIES
1
4
CI-275
UHFHI ANTENNA, 450 TO 512 MHZ
COMANT INDUSTRIES
1
5
CI-285
UHFHI (ii) ANTENNA, 450 TO 520 MHZ
COMANT INDUSTRIES
1
6
CI-306
800 ANTENNA, 806 TO 870 MHZ
COMANT INDUSTRIES
1
7
CI-285
800/700 (II) ANTENNA, 700 TO 870 MHZ
COMANT INDUSTRIES
1
8
7274-11-10
CIRCUIT BREAKER, 7.5 AMPS
KLIXON
NOTES:
1)
ALL WIRE IAW MIL-W-22759 UNLESS OTHERWISE SPECIFIED.
2)
ALL CABLE IAW MIL-C-27500 UNLESS OTHERWISE SPECIFIED.
3)
COAXIAL CABLE IAW MIL-C-17 UNLESS OTHERWISE SPECIFIED. DO NOT USE COAX WITH PVC INSULATION.
4)
FABRICATION & INSTALLATION OF WIRING HARNESS IAW AC 43.13-1B CHAPTER 11.
5)
GROUNDING AND BONDING IAW AC 43.13-1B CHAPTER 11, SECTION 15.
6)
ALL SINGLE WIRE TO BE #22 AWG MINIMUM AND ALL SHIELDED WIRES TO BE #24 AWG MINIMUM, UNLESS OTHERWISE
SPECIFIED.
INSTALLATION OF ANTENNA IAW AC 43.13-1B CHAPTER 4, SECTION 4, CHAPTERS 6 & 7, AND AC 43.13-2A CHAPTER 3.
IF POSSIBLE, THE ANTENNA SHOULD BE LOCATED A MINIMUM OF 12 FT FROM AIRCRAFT NAVIGATION RECEIVER
ANTENNAS AND A MINIMUM OF 4 FEET FROM AIRCRAFT COMMUNICATIONS AND ELT ANTENNAS. BE CAREFUL NOT TO
CHOSE SEPARATIONS THAT CLOSELY APROXIMATE 1/4 OR 1/2 OR WHOLE NUMBER MULTIPLES OF THE NAVIGATION OR
COMMUNICATIONS WAVELENGTH.
AN EQUIVALENT CIRCUIT BREAKER OR FUSE MAY BE USED.
THE MEMORY UP/DOWN PUSH BUTTONS ARE OPTIONAL.
THIS INPUT IS FOR BOTH 28 AND 5 VAC OR VDC PANEL LIGHTING. SELECT THE APPROPRIATE VOLTAGE IN THE
CONFIGURATION MENU. SEE PARA 2.17.
CONNECT TO THE APPROPRIATE AIRCRAFT DIMMING BUSS.
CONNECT TO THE AIRCRAFT AUDIO SYSTEM OR STAND-ALONE HEADSET JACKS.
INSTALLATION OF TRANSCEIVER IAW AC 43.13-1B CHAPTER 4, SECTION 4 AND AC 43.13-2A, CHAPTER 2. PR3 1/2 DZUS
RAIL OR EQUIVALENT MAY BE USED.
14)
TEST THE SYSTEM IN ACCORDANCE WITH THE POST-INSTALLATION TEST PROCEDURE IN THE INSTALLATION AND
OPERATING INSTRUCTIONS MANUAL.
15)
REFER TO THE AIRCRAFT STRUCTURAL REPAIR MANUAL AND THE MAINTENANCE MANUAL FOR INSTRUCTIONS AND
INFORMATION PERTINENT TO THIS INSTALLATION.
16)
THE USE OF RED DISPLAYS SHOULD BE MINIMIZED OR AVOIDED SO AS NOT TO DETRACT FROM THE ATTENTION GETTING
CHARACTERISTICS NEEDED IN WARNING AND CAUTION ANNUNCIATORS. RED SHOULD BE USED TO ANNUNCIATE
EMERGENCY CONDITIONS REQUIRING IMMEDIATE RESPONSE BY THE FLIGHT CREW. UNITS WITH RED DISPLAYS SHOULD
NOT BE LOCATED IN CLOSE PROXIMITY TO WARNING AND CAUTION ANNUNCIATORS. THE INSTALLATION OF UNITS WITH
RED DISPLAYS MUST BE EVALUATED ON A CASE BY CASE BASIS TO ENSURE THAT THE EFFECTIVENESS OF THE
WARNING AND CAUTION ANNUNCIATORS IS NOT ADVERSELY AFFECTED.
NOT NORMALLY USED IN AIRCRAFT.
CONNECTION TO AN OPTIONAL RC-7000 SLAVE CONTROL HEAD.
CONNECT TO GROUND FOR THE UNIT TO POWER UP WHEN THE POWER BUS IS SWITCHED ON. LEAVE UNCONNECTED
OTHERWISE.
OPTIONAL 4 OHM SPEAKER OUTPUT FOR COMBINED AUDIO. LEAVE UNCONNECTED IF NOT USED.
OPTIONAL RECEIVE ATTENUATOR. CAN BE USED ON ANY BAND AS REQUIRED FOR TRUNKING SYSTEMS.
SWITCH SHOULD BE MOUNTED ON THE PANEL NEAR THE TDFM-7000. THE ON POSITION SHOULD BE LABELED 'IN FLIGHT'
AND THE OFF POSTION LABELED WITH 'ON GROUND'
FIGURE 3.2b
Wiring connections for the TDFM-7000 Transceiver
Summary of Contents for TDFM-7000
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