DOCSLIB.ORG

Aircraft Electrical Systems What Is Electricity?

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Aircraft Electrical Systems What Is Electricity? Aircraft Electrical Systems What is Electricity? Electromagnetic Induction was •Electromagnetic Induction - movement of electrons through wires (or conductors) to create electric current. •Magnets passed across a closed-loop of wire at right-angles create an electromotive force (ELF) ELF – VOLTS – occurr when electrons move in the wire •Vice Versa: Electricity produces magnetism Vice Versa: Electricity produces magnetism Aircraft Electrical System Power Sources Battery • Provides Electrical Power when Alternator or Generator is not available • Several types of Batteries – Most Common – Lead-Acid Battery • Lead and Acid produce electrical charge Electrical battery • Small, light, not a lot of power • Simple and effective built to last • Recharges during flight from Alternator or Generator Aircraft Electrical System Power Sources Alternator Converts • Alternating Current (AC) to • Direct Current (DC) • For electrical system uses •DC is easier to use, • Lower volts, Safer •Also, provides Current to Battery to maintain battery power at max levels Aircraft Electrical System Power Sources Generator Produces Direct Current (DC) • For electrical system uses •DC is easier to use, • Lower volts, Safer •Like Alternator- provides Current to Battery to maintain battery power at max levels when Battery is “off –line” Aircraft Electrical System Controls Aircraft Electrical System Controls Master Switch Controls ALL aircraft electrical power from Source to Use Points •Left Side Switch controls Alternator Power Source •Right Side Switch controls Battery Power Source Aircraft Electrical System Controls Circuit Breaker & Fuses •Protect individual electrical User Systems from Electrical Overload (too much power) •Breakers and Fuses do Same Job •Difference: • Replace a Fuse • Reset a Circuit breakers •Technology Improvement • Fuses- Older Technology • Circuit Breakers – Newer Technology Airplane Electrical Systems Ammeter •Monitors electrical system performance Two types •To/from battery •Alternator load Aircraft Electrical System Controls Voltage Regulator • Volt is a measure of Electrical Power • Voltage regulator automatically maintains constant voltage level Master Switch Master Solenoid Starter Solenoid Electrical Switch • starter solenoid relays a large electrical current from origination source (Battery or Auxiliary Power Unit – APU) to rotate Starter Motor Starter Switch Starter • Electric Motor connected by special gearing to Engine Crankshaft • Rotates at very high speeds to rotate Engine Crankshaft • Engine Crankshaft rotation Aircraft Engine Magnetos Magneto • Magneto is a Field Generator – Rotating Magnet surrounded by loops of conducting wires • Rotating magnets generate electrical current flow through wires • Aircraft engines have TWO Magnetos for Redundancy – Safety feature – two spark sources are better than one Magneto Systems AND, TWO Spark Plugs • Two plugs fire simultaneously in Each Cylinder from Each Spark Source • Efficiency – More even spark – More even, steady burning – More complete burning – Spark improves burning in all areas of cylinder – Plug fouling – A problem Airplane Electrical Systems Battery •Stores Electricity •Powers Engine •Short-term Power Magneto and Electrical System By Cory and Amanda Electrical System- 727 Simplified Magneto and electrical system Jonathan Hord Magnetoes are self-sufficient Air, fuel and spark starts engine Glass Cockpits • Electrical power is • Magneto Powered Engine essential for Glass Panel can run without Battery Cockpits power • Glass Panels Can’t Glass Cockpit Power - Critical • Backup Battery – 30 Minutes?? Aircraft Electrical Systems The End – Fly Safe! Basic Electrical/Magneto Aircraft System A cylinder is a central working part of an engine. The space in which a piston travels. Multiple cylinders are arranged side by side by the engine block. The distance the piston travels in a cylinder is called the stroke. In the cylinder is where combustion occurs. A busbar in electrical power in distributing refers to thick strips of copper and aluminum and conducts electricity within a switchboard, distributing board, or other electrical apparatus. ELECTRICALBrian Bates, Baron Gould, & MAGNETO & Richard Lynch SYSTEMS FOR SMALL AIRCRAFT The Magnetos • A magneto operates on the principle of electromagnetic induction, is self-contained and engine driven • A magneto provides the electrical power for the ignition system to keep the engine running once the engine has been started. • A magneto is a combination of a low voltage alternating current generator and a high voltage coil and distributor. • Timing of magnetos is • The distributor in the magneto determined in the picks up the high voltage development phase. It is current from the coil and important to prevent pre- delivers it through the coil to ignition and/or detonation. the spark plugs. • Small, general aviation aircraft are usually equipped with two magnetos for efficiency, smoother operation of the engine, and redundancy, to prevent the loss of the system if one magneto were to fail (L & R) Alternator or Generator? • Most small aircraft are equipped with a 28-volt direct current (DC) electrical system, because OR an alternator produces more output for less weight compared to a generator and can produce a specific amount of power at a much lower rotational speed. • An alternator drives the electrical devices and stores energy in the battery. • The battery provides the power to crank the starter. Electrical System, (in a nutshell) • The second electrical system connects the electrical buses and the devices to the battery through a switch, the master switch. • The battery provides the power to crank the starter which will start the engine. Now, since the engine is running, the engine will supply power to the alternator and recharge the battery. • The magnetos continually work to create spark, ignite fuel and crank the engine. • Inside the cockpit, you will find an ammeter • Some instruments require electricity to function Know Your Systems • Read the pilot’s operating manual (POH) and aircraft flight manual (AFM) to learn how to identify and possibly handle any electrical problem in flight. • In the event of a power failure, you should know whether or not an emergency landing is necessary. • Evaluate Conditions •VFR or IFR = Nav equipment? •Retractable Gear = extended? • ER Procedures 101 •Flaps retracted or extended? •Transponder/Comms avail? • Aviate • Best Landing Site • Communicate References Glenn Research Center, http://www.grc.nasa.gov/WWW/K-12/airplane/icengine.html, 1-11-2008 Glenn Research Center, http://www.grc.nasa.gov/WWW/K-12/airplane/elecsys.html, 1-11-2008 Pilot Friend, http://pilotfriend.com/training/flight_training/tech/elec.htm, 1-11-2008 http://selair.selkirk.bc.ca/systems1/Engines/Aircraft%20Magneto%20systems.html, 1-11-2008 Electrical & Magneto Systems Mark Kinder Nathan Williamson Richard Douglas AVIA 112 Outline •Electrical Systems •Alternator •Battery •Ammeter •Master Switch •Circuit Breakers & Fuses •Magnetos Airplane Electrical Systems Battery •Stores Electricity •Powers Engine •Short-term Power Magnetos • Supplies current to plugs • Changes mechanical energy to electrical •Each A/C has 2 magnetos •Provides redundancy •Improves combustion •Magneto is engine-driven Summary •Electrical Systems •Alternator •Battery •Ammeter •Master Switch •Circuit Breakers & Fuses •Magnetos Electrical System Magneto Systems Typical Ignition System aircraft electrical systems generate, regulate and distribute electrical power throughout the aircraft. Many aircraft flight instrument systems use electricity •Aircraft electrical components operate on many different voltages both AC and DC •Most aircraft systems use : •115 Volt Alternating Current (AC) @ 400 Hz •28 Volt Direct Current (DC) Most aircraft engines provide power to generate AC generator (alternator) power. Electrical Systems • The function of the aircraft electrical system is to generate, regulate and distribute electrical power throughout the aircraft. • It is essential for the flight instrument systems. • Aircraft electrical components operate on many different voltages both AC and DC • However, most of the systems use: – 115 VAC @ 400 Hz – 28 VDC • Each of the engines on an aircraft drives an AC generator (alternator). Electrical Power System Components • AC Generator or Alternator • Constant Speed Drive: in this case would be the belt driven by the engine. • Today's modern small aircraft contain all of this inside the alternator: – Integrated Drive Generator – Transformer Rectifier Unit – Generator Control Unit Basic Functions • The basic functions of the electrical system’s components are to: – Generate Power – Control Electrical Power – Protect the Electrical System – Distribute Electrical Power Throughout the Aircraft Magneto How they WoRk! • The ignition magneto combines the functions of a dynamo, contact breaker points, "condenser", and ignition coil. • The engine spins a magnet inside a coil, and also operates a contact breaker, interrupting the current and causing the voltage to be increased sufficiently to jump a small gap. The spark plugs are connected directly from the magneto output. All pilots are… Aircraft Electrical and Magneto Systems Corey Hjalseth Ali Spirggs Fernando Rodriguez Aircraft Magneto Systems • A magneto is a combination of low and high voltage current generator and distributor. • The magnetos ignition coil transforms low voltage to high voltage. • The distributor picks up the high voltage from the coils and delivers it to the spark
Load more

Recommended publications
  • Bibliography on Ignition and Spark-Ignition Systems
    Bibliography on Ignition and Spark-Ignition Systems U.S. Department of Commerce National Bureau of Standards Miscellaneous Publication 251 ; THE NATIONAL BUREAU OF STANDARDS Functions and Activities The functions of the National Bureau of Standards include the developm and maintenance of the national standards of measurement and the provision of means and methods for making measurements consistent with these standards; the determination of physical constants and properties of materials ; the develop- ment of methods and instruments for testing materials, devices, and structures advisory services to government agencies on scientific and technical problems; invention and development of devices to serve special needs of the Government;I and the development of standard practices, codes, and specifications, including assistance to industry, business and consumers in the development and accepi ance of commercial standards and simplified trade practice recommendation!I The work includes basic and applied research, development, engineering, instru- mentation, testing, evaluation, calibration services, and various consultation andd information services. Research projects are also performed for other govern- ment agencies when the work relates to and supplements the basic program of the Bureau or when the Bureau's unique competence is required. The scope of activities is suggested by the listing of divisions and sections on page 26. Publications The results of the Bureau's research are published either in the Burea>au'g own series of publications or in the journals of professional and scientific societies. The Bureau itself publishes three periodicals available from the Gov- ernment Printing Office: The Journal of Research, published in four separai sections, presents complete scientific and technical papers ; the Technical Ne Bulletin presents summary and preliminary reports on work in progress ; a Central Radio Propagation Laboratory Ionospheric Predictions provides da for determining the best frequencies to use for radio communications througho the world.
    [Show full text]
  • Model 162 SERIAL NUMBER
    Model 162 SERIAL NUMBER Serials 16200001 and On REGISTRATION NUMBER This publication includes the material required to be furnished to the pilot by ASTM F2245. COPYRIGHT © 2009 ORIGINAL ISSUE - 22 JULY 2009 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA REVISION 3 - 28 SEPTEMBER 2010 162PHUS-03 U.S. CESSNA INTRODUCTION MODEL 162 GARMIN G300 PILOT’S OPERATING HANDBOOK AND FLIGHT TRAINING SUPPLEMENT CESSNA MODEL 162 SERIALS 16200001 AND ON ORIGINAL ISSUE - 22 JULY 2009 REVISION 3 - 28 SEPTEMBER 2010 PART NUMBER: 162PHUS-03 162PHUS-03 U.S. i/ii CESSNA INTRODUCTION MODEL 162 GARMIN G300 CONGRATULATIONS Congratulations on your purchase and welcome to Cessna ownership! Your Cessna has been designed and constructed to give you the most in performance, value and comfort. This Pilot’s Operating Handbook has been prepared as a guide to help you get the most utility from your airplane. It contains information about your airplane’s equipment, operating procedures, performance and suggested service and care. Please study it carefully and use it as a reference. The worldwide Cessna Organization and Cessna Customer Service are prepared to serve you. The following services are offered by each Cessna Service Station: • THE CESSNA AIRPLANE WARRANTIES, which provide coverage for parts and labor, are upheld through Cessna Service Stations worldwide. Warranty provisions and other important information are contained in the Customer Care Handbook supplied with your airplane. The Customer Care Card assigned to you at delivery will establish your eligibility under warranty and should be presented to your local Cessna Service Station at the time of warranty service. • FACTORY TRAINED PERSONNEL to provide you with courteous, expert service.
    [Show full text]
  • Digital Twin and Triple Spark Ignition in Four- Stroke Internal Combustion Engines of Two- Wheelers
    International Journal of Innovations in Engineering and Technology (IJIET) Digital Twin and Triple Spark Ignition in Four- Stroke Internal Combustion Engines of Two- Wheelers G.V.N.B.Prabhkar Department Of Mechanical Engineering, V.K.R, V.N.B &A.G.K College of Engineering B.Kiran Babu Department Of Mechanical Engineering, V.K.R, V.N.B &A.G.K College of Engineering K.Durga Prasad Department Of Mechanical Engineering, V.K.R, V.N.B &A.G.K College of Engineering Abstract - Today it is a common trend. It has become a fashion for the people especially living in urban areas to ride such vehicles. Now the companies even want to launch such vehicles that attract the younger generation. This can be achieved by technology known as DTSi. Due to DTSi (digital twin spark ignition) system it is possible to combine strong performance and fuel efficiency. The improved engine efficiency modes have also resulted in lowered fuel consumption. The efficiency of these small engines were enhanced with increased power output just by increasing the number of fuel igniting element i.e. Spark Plug. Spark ignition is one of the most vital systems of an engine. Any variation in the spark timing and number of sparks per minute affects the engine performance severely. Thus a good design and control of the system parameters becomes most essential for optimum performance of an engine. Due to Digital Twin Spark Ignition system it is possible to combine strong performance and higher fuel efficiency. DTSi offers many advantages over conventional mechanical spark ignition system.
    [Show full text]
  • Bibliography on Ignition and Spark-Ignition Systems
    NOV - o NBS CIRCULAR 580 Bibliography on Ignition and Spark-Ignition Systems UNITED STATES DEPARTMENT OF COMMERCE NATIONAL BUREAU OF STANDARDS PERIODICALS OF THE NATIONAL BUREAU OF STANDARDS (Published monthly) The National Bureau of Standards is engaged in fundamental and applied re¬ search in physics, chemistry, mathematics, and engineering. Projects are con¬ ducted in fifteen fields: electricity and electronics, optics and metrology, heat and power, atomic and radiation physics, chemistry, mechanics, organic and fibrous materials, metallurgy, mineral products, building technology, applied mathe¬ matics, data processing systems, cryogenic engineering, radio propagation, and radio standards. The Bureau has custody of the national standards of meas¬ urement and conducts research leading to the improvement of scientific and engineering standards and of techniques and methods of measurement. Testing methods and instruments are developed, physical constants and properties of materials are determined, and technical processes are investigated. Journal of Research The Journal presents research papers by authorities in the specialized fields of physics, mathematics, chemistry, and engineering. Complete details of the work are presented, including laboratory data, experimental procedures, and theo¬ retical and mathematical analyses. Annual subscription: domestic, $4.00; $1.25 additional for foreign mailing. Technical News Bulletin Summaries of current research at the National Bureau of Standards are pub¬ lished each month in the Technical News Bulletin. The articles are brief, with emphasis on the results of research, chosen on the basis of their scientific or technologic importance. Lists of all Bureau publications during the preceding month are given, including Research Papers, Handbooks, Applied Mathematics Series, Building Materials and Structures Reports, Miscellaneous Publications, and Circulars.
    [Show full text]
  • Horseless Carriage Club of America
    Horseless Carriage Club of America Founded in Los Angeles Novemb er 14, 1937 A nonprofit corporation founde d by and for automotive antiquarians and dedicated to the prese rvation of motor PLEASE MARK YOUR CALENDAR NOW SO YOU WILL ve hicles of ancient age and historical value, their acces ­ NOT MISS THE MEETINGS YOU WISH TO ATTEND. sories, archives and romantic /ore. OFFICERS March 8-9-10-11-12 I 17th Annual National AUTO­ Joe Straub -------- ----- --- -------·········-·-·······-------···· -···· President RAMA, Conn. State Armory, Hartford, Conn. Dr. E. C. Lawrence ______ _____________ ., ............... Vice President I Roger Ellis _______ ___ ________ _____ ____ ., ..................... ----·--· Secretary March 10 Swap Meet and Flea Market Regions of HCCA, AACA anr MARC, Houston, Texas Roy Davis ................................................ ------ ----- - Treasurer Ken Sorensen ...................................... ---- Board Chairman March 10 I 9th Ann. Swap Meet, Madera Fair­ grounds Central California Region HCCA, Madera, Cal. DIRECTORS AND TERMS OF OFFICE March 10 I Shake-Down Tour 1966-68 1967-69 1968-70 Southern California Region HCCA Peter Bechtel Ralph Cherry Roy Davis March 16 I Dinner Meeting E. R. Bourne Clarence Kay Roger Ellis Canton (Ohio) Region HCCA Cecil Frye Dr. E. C. Lawrence David H. Goerlich March 18-23 I Festival of Classic Motoring Ken Sorensen Herb Schoenfeld Sandy Grover Sporting Car Club of South Australia Les Thomas Joe Straub Edwin N. Saville March 20 I Regular Meet, Randall Jr. Museum San Francisco (Cal.) Region HCCA COMMITTEE CHAIRMEN March 20 I National Meet, South Gate (Cal.) Aud. Vintage Chevrolet Club of America Activities .......................................................... Cecil Frye I & Regional Groups ........................ --------------------- · Les Thomas March 23-24 1 2 Cylinder Tour, Palm Springs Pub lications ____________________________ ...........
    [Show full text]
  • APPLICATION GUIDE for WAUKESHA® VHP Series
    ® APPLICATION GUIDE For WAUKESHA® VHP Series GAS ENGINE TECHNOLOGY reliable ∙ efficient ∙ worldwide Ignition Controllers & Harnesses MIC3+CEC Ignition Controllers ■ High energy retrofit ignition controller 1) ■ More than double the ignition energy (300 mJ) ■ Plug & play solution enables quick conversion without great effort ■ Predefined configuration data can be easily uploaded to the ignition controller ■ For use with VHP F2895, F3521 Equivalent to: P/N 66.00.358-8 WAUKESHA® P/N 740608A, 740608 CEC Models 811/811A MOTORTECH P/N 06.00.515-6/-8 MOTORTECH MIC500 ■ High energy retrofit ignition controller 1) ■ More than double the ignition energy (300 mJ) ■ Plug & play solution enables quick conversion without great effort ■ Predefined configuration data can be easily uploaded to the ignition controller ■ For use with VHP L5108, L5790, L7042 Equivalent to: P/N 66.00.359-12 WAUKESHA® P/N 740609A, 740609 CEC Models 1211/1211A MOTORTECH P/N 06.00.516 MOTORTECH MIC500 1) Patented technology (Patent No. US 8,893,692 BS) 2 ® Ignition Controllers & Harnesses DetCon20 MOTORTECH DETONATION CONTROL SYSTEM 2 1 1 CAN Special bracket kit to mount the igni- PowerView3 tion controller on the position of the MOTORTECH ENGINE INFORMATION MONITOR WAUKESHA® device. 3 0 to 5V/4 to 20 mA/ASO CAN G 24 VDC Power Supply E F A C B Due to the same connector configura- tion, the existing input and output D wiring can be re-used. Additional con- H nectors for CAN Bus (PowerView3) and analog input (DetCon20) connection. Required components 2 The DetCon20 control unit offers 3 Complete visualization of MIC3+, 1 MIC3+CEC ignition controller full protection for gas engines from 2 MIC4 and MIC5 operating data, inclu- to 20 cylinders.
    [Show full text]
  • Airplane Flying Handbook (FAA-H-8083-3B) Chapter 2
    Chapter 2 Ground Operations Introduction All pilots must ensure that they place a strong emphasis on ground operations as this is where safe flight begins and ends. At no time should a pilot hastily consider ground operations without proper and effective thoroughness. This phase of flight provides the first opportunity for a pilot to safely assess the various factors of flight operations including the regulatory requirements, an evaluation of the airplane’s condition, and the pilot’s readiness for their pilot in command (PIC) responsibilities. 2-1 Flying an airplane presents many new responsibilities that are not required for other forms of transportation. Focus is often overly placed on the flying portion itself with less emphasis placed on ground operations; it must be stressed that a pilot should allow themselves adequate time to properly prepare for flight and maintain effective situational awareness at all times until the airplane is safely and securely returned to its tie-down or hangar. This chapter covers the essential elements for the regulatory basis of flight including an airplane’s airworthiness requirements, important inspection items when conducting a Figure 2-2. A visual inspection of the aircraft before flight is an preflight visual inspection, managing risk and resources, and important step in mitigating airplane flight hazards. proper and effective airplane surface movements including the use of the Airplane Flight Manual/Pilot’s Operating Handbook (AFM/POH) and airplane checklists. be kept accurate and secure but available for inspection. Airplane logbooks are not required, nor is it advisable, to be Preflight Assessment of the Aircraft kept in the airplane.
    [Show full text]
  • Unit – I - Rockets System – Sae1402
    SCHOOL OF MECHANICAL ENGINEERING DEPARTMENT OF AERONAUTICAL ENGINEERING UNIT – I - ROCKETS SYSTEM – SAE1402 1 I. Ignition System An ignition system is a system for igniting a fuel-air mixture. Ignition systems are well known in the field of internal combustion engines such as those used in petrol (gasoline) engines used to power the majority of motor vehicles, but they are also used in many other applications such as in oil-fired and gasfired boilers, rocket engines, etc. Diesel engines rely on air compression for ignition, but usually also have glow plugs that preheat the combustion chamber to allow starting of the engine in cold weather. Other engines may use a flame, or a heated tube, for ignition. Types 1. Magneto systems 2. Switchable systems 3. Battery and coil-operated ignition 4. Modern ignition systems 5. Mechanically timed ignition 6. Electronic ignition 7. Digital electronic ignitions Magneto systems Magneto ignition coil. For more details on this topic, see Ignition magneto. The simplest form of spark ignition is that using a magneto. The engine spins a magnet inside a coil, or, in the earlier designs, a coil inside a fixed magnet, and also operates a contact breaker, interrupting the current and causing the voltage to be increased sufficiently to jump a small gap. The spark plugs are connected directly from the magneto output. Early magnetos had one coil, with the contact breaker (sparking plug) inside the combustion chamber. In about 1902, Bosch introduced a double-coil magneto, with a fixed sparking plug, and the contact breaker outside the cylinder. Magnetos are not used in modern cars, but because they generate their own electricity they are often found on piston-engined aircraft engines and small engines such as those found in mopeds, lawnmowers, snowblowers, chainsaws, etc.
    [Show full text]
  • Analysis of Aviation Safety Reporting System Incident Data Associated with the Technical Challenges of the Vehicle Systems Safety Technology Project
    NASA/TM—2014-217900 Analysis of Aviation Safety Reporting System Incident Data Associated With the Technical Challenges of the Vehicle Systems Safety Technology Project Colleen A. Withrow and Mary S. Reveley Glenn Research Center, Cleveland, Ohio October 2014 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the • CONFERENCE PUBLICATION. Collected advancement of aeronautics and space science. The papers from scientific and technical NASA Scientific and Technical Information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or cosponsored by NASA. this important role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program operates under the auspices technical, or historical information from of the Agency Chief Information Officer. It collects, NASA programs, projects, and missions, often organizes, provides for archiving, and disseminates concerned with subjects having substantial NASA’s STI. The NASA STI program provides access public interest. to the NASA Aeronautics and Space Database and its public interface, the NASA Technical Reports • TECHNICAL TRANSLATION. English- Server, thus providing one of the largest collections language translations of foreign scientific and of aeronautical and space science STI in the world. technical material pertinent to NASA’s mission. Results are published in both non-NASA channels and by NASA in the NASA STI Report Series, which Specialized services also include creating custom includes the following report types: thesauri, building customized databases, organizing and publishing research results. • TECHNICAL PUBLICATION. Reports of completed research or a major significant phase For more information about the NASA STI of research that present the results of NASA program, see the following: programs and include extensive data or theoretical analysis.
    [Show full text]
  • Application Guide for CATERPILLAR G3300 Series and Are Used for Reference Purposes Only
    ® APPLICATION GUIDE FOR CATERPILLAR® G3300 SERIES reliable ∙ efficient ∙ worldwide 1 REV. 06/2013 IGNITION CONTROLLERS MIC3+ Series Ignition Controllers ▸ High energy ignition controller for retrofits ▸ Plug & play solution ▸ Patented technology (Patent No. US 8,893,692 BS) ▸ For use with G3304, G3306 P/N 66.00.356-8 Equivalent to: CATERPILLAR® P/N 163-6164 CATERPILLAR® Digital Ignition Controllers – Refurbished ▸ MOTORTECH refurbished ignition controllers ▸ Come with a 1 year warranty ▸ Always consult factory for availability Equivalent to: P/N 163-6164-R CATERPILLAR® P/N 163-6164 As good as new! MOTORTECH Repair and Overhaul Service Based on years of technical experience MOTORTECH offers a comprehensive repair and overhaul service for almost all popular ignition controllers. Our economically remanufacturing process covers intensive inspections, parts replacement, extensive reconditioning and full operational test procedures. Within an average of four weeks (depends on customer location) we return a fully functional product that looks as good as new. Flatrate Overhaul of: • CATERPILLAR® ignition controllers for G3300/G3400 series gas engines • ALTRONIC® DISN series • All MOTORTECH ignition controllers 2 IGNITION COILS Ignition Coils ▸ ALTRONIC® Style ▸ For unshielded applications P/N 06.50.054 Equivalent to: CATERPILLAR® P/N 4W-5439 ALTRONIC® P/N 591010 ▸ ALTRONIC® Style ▸ For unshielded applications P/N 06.50.055 Equivalent to: CATERPILLAR® P/N 2W-3747 ALTRONIC® P/N 501061 Integral Ignition Coils – Slim Design ▸ 6 in. length ▸ 13/16-20 UNEF inner thread ▸ 3 pole primary connector P/N 95.09.222-6 Equivalent to: CATERPILLAR® P/N 107-2400 ALTRONIC® P/N 591011A Grommet for Integral Ignition Coils ▸ Teflon grommet P/N 06.84.116 3 PICKUPS Pickups ▸ Hall effect pickup – Active Low ▸ Thread size 5/8 in.-18 UNF ▸ 2.5 in.
    [Show full text]
  • Service Data
    01-30A-00 CS-310 1 0 SERVICE DATA CHAIN SAW CS-310 (Serial number : 11000001-11999999) (Serial number : 12000001-12999999) INTRODUCTION CONTENTS page We are constantly working on technical im- 1 SERVICE INFORMATION.............................. 2 provement of our products. For this reason, 1-1 Specification ............................................... 2 technical data, equipment and design are 1-2 Technical data............................................. 3 subject to change without notice. All speci- 1-3 Torque limits................................................ 4 1-4 Special repairing materials ......................... 4 fications, illustrations and directions in this 1-5 Service limits............................................... 5 SERVICE DATA are based on the latest 1-6 Special tools ............................................... 6 product information available at the time of publication. 2 CARBURETOR ADJUSTMENT PROCEDURE .... 7 2-1 General adjusting rules............................... 7 2-2 Presetting Idle adjust screw, L mixture needle and H mixture needle ........................................ 7 2-3 Adjusting carburetor.................................... 9 Reference No. 01-30A-00 ISSUED: 20081 1 2 SERVICE INFORMATION CS-310 1 SERVICE INFORMATION 1-1 Specifications Model CS-310 Dimensions Length* mm(in) 396 (15.59) Width mm(in) 232 (9.13) Height mm(in) 268 (10.55) Dry weight* kg(lb) 4.0 (8.8) Engine Type KIORITZ, air-cooled, two-stroke, single cylinder Rotation Clockwise as viewed from the output end Displacement
    [Show full text]
  • 1.3.0.12 ECCAIRS Aviation Data Definition Standard
    ECCAIRS Aviation 1.3.0.12 Data Definition Standard English Attribute Values ECCAIRS Aviation 1.3.0.12 V4 CD Descriptive Factors Aerodrome generally (Aerodrome generally) 40000000 Aerodrome generally: The part played by aerodrome factors in the occurrence. Aerodrome as a structure (Aerodrome as a structure) 41000000 Apron/ramp as an entity (Apron/ramp as an entity) 41300000 N.B. Apron and ramp are synonymous for a defined area, on a land aerodrome, intended to accommodate aircraft for purposes of loading or unloading passengers, mail or cargo, fuelling, parking or maintenance.(Annex 14) Aircraft parking position/gate (Aircraft parking position/gate) 100000118 Apron/ramp congestion (Apron/ramp congestion) 41300200 Apron/ramp obstruction (Apron/ramp obstruction) 41300100 Apron/ramp surface condition (Apron/ramp surface condition) 41300400 Apron/ramp braking action (Apron/ramp braking action) 41300500 Apron/ramp surface state (Apron/ramp surface state) 41300300 Runway as an entity (Runway as an entity) 41100000 Runway. A defined rectangular area on a land aerodrome prepared for the landing and take-off of aircraft. Annex 14. Runway approach obstructions (Approach obstructions) 41100500 All fixed (whether temporary or permanent) and mobile objects that extend above a defined surface intended to protect aircraft in flight. Runway arresting gear (Runway arresting gear) 41100900 Any equipment installed on or after the runway intended to arrest / stop the aircraft. Engineered materials arrestor system (EMAS) (Engineered materials arrestor system 100000120 (EMAS)) An engineered bed of lightweight, crushable concrete built at the end of a runway. Runway safety net (Runway safety net) 100000119 Runway clearway (Runway clearway) 100000056 A defined rectangular area on the ground or water under the control of the appropriate authority, selected or prepared as a suitable area over which an aeroplane may make a portion of its initial climb to a specified height.
    [Show full text]