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Kx 155 installation manual
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About this item. This translation tool is for your convenience only. A warning signal input current of A or greater shall produce a fully concealed warning flag 1.
The bearing error shall be less than 2. A warning signal input current of ,A or less shall produce a fully visible warning flag. The indicator shal] meet a11 applicable requirements of TSO C40a. A warning signal input current of yA or less shall produce a fully visible warning flag. A warning signal input current of A or greater shall produce a fully concealed warning flag. A warning signal input current of uA or greater shall produce a fully concealed warning flag 1. KI 5. KN 72, KI 2.
KI 6. XN 72, KI A 3. Close adherence to these suggestions will assure a more satisfactory performance from the equipment, 2. Make a visual inspection of the unit for evidence of damage incurred during shipment. If a claim for a danage is to be made, save the shipping container to substantiate the claim. When all equipment is removed, place in the shipping container, all packing materials for use in unit storage or reshipnent.
The installing agency will supply and fabricate all external cables. Interconnect diagrams are Figures through Model DMB or equivalent should be used. While modern day individual circuit designs consume much less electrical energy, the watts per cubic inch dissipated within avionics units remains much the same due to high density packaging techniques utilized. Consequently, the importance of providing avionics stack cooling is stil] with us. Select a position in the panel that is not too close to any high external heat source.
Remember to allow adequate space for installation of cables and connectors. Avoid sharp bends and placing the cables near aircraft control cables. Mark and drill the mounting holes C, Secure the mounting rack to the instrument panel per Figure The rear mounting bosses should be attached to the aircraft by means of support brackets. Antennas should be installed per manufacturer's recommendations.
Mount antenna on flat metal surface or install a ground plane at least 18 inches square. The antenna should be well removed from any projections and the engine s and propeller. Navigation Antenna a.
The location should be well removed from other antennas, projections and engine s. It should have a clear line of sight area if possible. The antenna must be mounted symmetrically with the centerline of the aircraft. Avoid running other coaxial and wires near the NAV antenna cable.
Assembly of the connector is as follows: A. The last two digits of the contact terminal part number indicates the number of terminals required. Place the conductor tab section of a contact terminal on Anvil 8 with the contact portion facing away from the operator, Close the crimper slightly until the contact tabs touch the female jaw.
Crimp the conductor tabs by squeezing the handles together until the jaws are fully closed or a sufficient crimp is obtained. Place the insulating tab section on Anvil A. Crimp again until the jaws are fully closed or a sufficient crimp is obtained.
Contact Insertion into Molex Connector Hous ing 1. The terminal cannot be inserted upside down. Be sure to push the terminal all the way in, until a click can be felt or heard. Location of Polarizing Key in Housing 1, Prior to insertion of connector into rear of unit, check polarizing key position between contacts 3 and 4. When the ejector is slid into place, the retaining tab of the contact is raised, allowing the contact to be removed by pulling moderately on the lead, 3.
Neither the contact or position is damaged by removing a contact; however, the contact should be checked visually before reinstalling in connector to be certain that retaining tab "A" extends as shown see Figure Coax Connector Refer to Figure for the details for mounting the right angle coaxial BNC connector to the coax cable. Install the connector into the mounting rack. Looking at the top of the unit, make sure the front lobe of the holddown device is in a vertical position.
Slide the unit into the mounting rack until the front lobe touches the mounting rack. Turn clockwise until the rear lobe engages the mounting rack. Normally, this does not damage the source units but can cause lower signal levels resulting in less audio from these sources sharing that input pin. After installation, verify that turning the power off on each of the sources does not stop the audio from all the sources sharing the input. Connection to other devices may result in damage to both the KX A and the other device.
Variations in microphones, even with identical manufacturers part numbers, can produce this problem when both are connected at the same time. Microphone isolation relays are recommended so that only one microphone is connected at one time. Both pins have identical signals but are at different voltage levels. No signals, other than the five inputs, are output from the amplifier, thus allowing the installer complete flexibility. The KX A audio amplifiers do not need external loads applied to either their inputs or outputs when they are not used.
Perform a ground check of the installation prior to the flight test. Using a local frequency, confirm that the COMM function can receive and transmit a modulated signal. An operation performance flight test is recommended after the installation is completed to insure satisfactory performance of the equipment in its normal environment.
Check all aircraft control movements to be sure no electrical cables interfere with their operation. To check the communications transceiver, maintain an altitude of at least feet and contact a ground station facility at a range of at least fifty nautical miles. Contact a ground station close in.
Pull the volume control knob out to defeat the automatic squelch feature and listen for any unusual electrical noise which would reduce the COMM receiver sensitivity by increasing the squelch threshold. Listen to the VOR audio and insure that no electrical interference such as magneto noise is present. Check the tone identifier filter operation. Check the VOR accuracy. The glideslope function will not operate for units that do not have the glideslope receiver.
Check section 1 for unit part numbers that have glideslope receivers. Then insert the terminal into the jaws from the back side. The terminal is in the correct position when the insulation tabs are flush with the outside face of the crimp jaws.
Push the wire stop down so that it rests snugly behind the contact portion of the terminal. Squeeze the handles until the crimp jaws close and the ratchet releases. Straighten the terminal if necessary, then release the plier grips and remove the crimped terminal. It takes the desired audio signal. AEM is responsible for all matters related to this product, including sales,. Description and Specifications Contents 1.
If you have any questions concerning. Operation Manual for Users Model No. It allows up to 10 base stations. Securitron Magnalock Corp. Nothing contained herein shall. Record of Revisions Retain this record in front of handbook. Upon receipt of a revision, insert changes and. Accurate measurement. Savant Systems AMP is a multi-room amplifier for distributed audio applications. The AMP is an ultraefficient Class D amplifier delivering 8 channels of reliable amplification rated at 25 watts.
It is usually sold as a combination to provide a simple, turn key tracking. Ameritron ATP The Ameritron ATP relieves temperature related stress on amplifiers, tuners, and dummy loads while allowing proper system adjustments. It allows amplifiers to be properly adjusted. Hear The Future The guideline published by Occupational Safety. Drawings and general provisions of Contract, including General and Supplementary Conditions and Division-1 Specification. Each product and program carries a respective written warranty, the only warranty on which the customer can rely.
Avery Dennison Corp. No part of this publication may be reproduced, stored in a retrieval. Our products are based on a simple philosophy: The component shall reproduce the original.
Section I General Information 1. Turbo X channel UHF true diversity The new Turbo X series from Smart Wireless is the culmination of two years of research and development into advanced wireless technology. Using sophisticated RF design. A01 Copyright Dell, Inc. All rights reserved. Dell is a trademark of Dell, Inc. EqualLogic is a registered trademark. All trademarks. Phone: FANs , The only warranties for HP products and services are set forth in the express warranty statements accompanying.
Contents Safety Warnings These have been designed for operation in RV s providing a DC power system, with optional. If the carton is. Panasonic welcomes you to our ever growing family.
It is important. B NG Comm munications 5. Class B devices have a Federal Communications. Microsoft, Windows, and Windows Vista are either.
For the remainder of the document, we will refer to using the term Hearing Loop rather than Audio. Microsoft and Windows are U. The only warranties for HP. Retain this Owner s Manual for future reference. This set of instructions applies to racking and rail kit installation for 6XX and above. The Rack Mounting Instructions section below provides information on installing the SC chassis into a rack unit. Simplified Directions 1. Install the batteries. Turn the unit on rotate volume knob clockwise.
Enter the first five digits of desired frequency 2 2 5 0 0 for Table of. The carton and packaging have. Modifying the Yaesu FT External These connectors are designed for use in pluggable. Please read and ensure that you fully understand the installation and set up procedures. Timo Rantanen This transmitter type. Read all instructions before installation.
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