O-360-A Lycoming Aircraft Engines Parts Catalog
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MGB Alternator Conversion Installation Instructions for MGA & 1962 to 1967 MGB PART# 130-078, 130-088, 130-098 440 Rutherford St
MGB Alternator Conversion Installation Instructions For MGA & 1962 to 1967 MGB PART# 130-078, 130-088, 130-098 440 Rutherford St. Goleta, CA 93117 1-800-642-8295 • FAX 805-692-2525 • www.MossMotors.com Scan the code to watch Moss's Generator to Alternator Conversion Video Or search “Moss TV generator to alternator conversion” on YouTube. Tools required: Vehicle Preparation: Positive Ground to Negative Ground Conversion • Small and medium flat blade screwdriver 1. Remove the battery cover behind the seats using a • Phillips head screwdriver screwdriver to release the dzus fasteners. Disconnect and remove the battery, or both batteries if still • 11/32" wrench, 7/16" wrench, 1/2" wrench, configured for a dual 6 volt set up, using a 1/2" 5/8" wrench wrench. • 7/16" socket with extension, 1/2" socket, 5/8" socket, 22mm socket 2. Disconnect the Yellow/Green and Yellow wires from the generator. If the generator uses ring type • Center punch connectors use a 5/16" and 7/16" wrench. • Hammer 3. For the installation of the Lucas alternator the ignition • 1/4" drill bit, electric drill coil will have to be relocated to the engine bay side • Deadblow hammer of the right fender well. Remove the coil from the generator using a 7/16" socket. Locate a new place • Air impact gun for the coil and mark the hole locations. Using a • Pry bar center punch and hammer, make two dimples at the center of the marks to insure that the drill bit will not • Wire cutters walk around when the holes are being started. -
1. the Future for Automotive Two-Stroke Engines – Part 2
N0.21 THE FUTURE FOR AUTOMOTIVE TWO-STROKE ENGINES (Part 2) CURRENT DEVELOPMENTS Synthetic-based formulation likely to be the preferred option. In the previous issue of Lube, the origins and initial development of the 2T Tendency for combustion chamber deposit formation would have required a engine were described. The earlier engines, characterised by smoky exhausts low ash or ash less lubricant. and poor specific fuel economy, will be remembered by many of the older High temperatures require strong anti-oxidancy. fraternity, as they provided motive power for many commuter lightweight motorcycles, mopeds and scooters in the prewar and postwar years. Many WET SUMP vehicle manufacturers in the UK used proprietary power units manufactured Again, no valve train therefore no requirement for e.g. ZDDP anti-wear by specialist engine manufacturers such as Villiers, who dominated the agent. market, although smaller engine suppliers included companies such as British Diluent unnecessary/undesirable. Anzani. A number of other companies, including Scott, Associated Conventional base oil plus viscosity index-improver is possible (SAE 10/30?). Motorcycles, Excelsior and latterly Ariel also designed their own engines, use Polymer deposits may favour synthetic approach. of which was restricted in the main to vehicles of their own manufacture. However, with the demise of the UK motorcycle industry, 2T engine Tendency for combustion chamber deposits requires a low ash approach. developments, which have progressed steadily during subsequent years, The conclusion was that, in spite of the substantial differences between the have been largely attributable to overseas manufacturers with assistance types of the Orbital engines described above, it may well have been possible from some UK specialist consultancy organizations such as Ricardos at to meet the requirements of both types of engine with a single lubricant, Shoreham. -
Leburg Electronic Ignition System EI10A Installation Manual
Leburg Electronic Ignition System EI10A Installation Manual For Aero VW’s - Or Any 2 Or 4 Cylinder 4 Stroke Engine Skycraft Ltd Telephone: 01406 540777 Riverside House Bloodfold Farm Website: www.skycraft.ltd Ravens Bank Saturday Bridge Email: [email protected] Holbeach Lincolnshire Facebook: @skycraftlimited PE12 8SR © Skycraft Ltd 2013 Leburg EI10A Manual—July 2020 Page 1 Contents 1. Read This First 2. The VW As An Aero Engine 3. Ignition System Performance 4. Principles Of Operation 5. Set Up 6. Power Supplies 7. Fitting A Honda CBR 600 Alternator 8. Manufacture & Assembly Notes 9. Wiring Notes 10. Wiring Up The Spark Plugs 11. Drawings © Skycraft Ltd 2013 Leburg EI10A Manual—July 2020 Page 2 1. Read This First By virtue of the techniques, design, components used and the care taken in building and testing, each ignition controller is believed to be highly reliable. The risk of failure is thus low, but it is finite. Therefore, this system is only made available on the basis that the user agrees to implement a Dual Ignition System. The Leburg system is the dual system, with the power supply system described in this manual. If any change from this is intended, you will need to check with the LAA that they will accept it. If a different alternator or power system is used, again, you will need to check with the LAA that they will accept it. The benefits of smooth running and getting the maximum power are obtained when the system is installed as described in this manual, with dual controllers, dual ignition spark plugs, both firing at the same time at the optimum advance angle. -
Before Endine Start
C-A152 CESSNA – NORMAL PROCEDURES BEFORE ENGINE START THROUGH ENGINE SHUTDOWN – CHECKLIST WILL BE VERBALIZED BEFORE ENGINE START WINDOWS ..................................................................................................................... SECURE CABIN DOORS ............................................................................................................. CLOSED TACH TIME ................................................................................... CHECK TIME REMAINING HOBBS TIME ................................................................................................................ RECORD BEFORE TAKE-OFF BRAKES ....................................................................................... APPLY TOE BRAKES ONLY TYPE OF TAKEOFF .............................................................................................. DETERMINE PASSENGER BRIEF ................................................................................................ COMPLETE FLAPS .................................................................................................................. AS REQUIRED SEATBELTS AND HARNESSES .........................................................FASTEN AND SECURE AIRSPEEDS: ROTATION, CLIMB OUT, CABIN DOOR ......................................................................................... CLOSE AND SECURE AND BEST GLIDE ................................................................... CALCULATE (GUST SPREAD) PRE-TAKEOFF BRIEFING ..................................................................................... -
Wärtsilä 32 PRODUCT GUIDE © Copyright by WÄRTSILÄ FINLAND OY
Wärtsilä 32 PRODUCT GUIDE © Copyright by WÄRTSILÄ FINLAND OY COPYRIGHT © 2021 by WÄRTSILÄ FINLAND OY All rights reserved. No part of this booklet may be reproduced or copied in any form or by any means (electronic, mechanical, graphic, photocopying, recording, taping or other information retrieval systems) without the prior written permission of the copyright owner. THIS PUBLICATION IS DESIGNED TO PROVIDE AN ACCURATE AND AUTHORITATIVE INFORMATION WITH REGARD TO THE SUBJECT-MATTER COVERED AS WAS AVAILABLE AT THE TIME OF PRINTING. HOWEVER, THE PUBLICATION DEALS WITH COMPLICATED TECHNICAL MATTERS SUITED ONLY FOR SPECIALISTS IN THE AREA, AND THE DESIGN OF THE SUBJECT-PRODUCTS IS SUBJECT TO REGULAR IMPROVEMENTS, MODIFICATIONS AND CHANGES. CONSEQUENTLY, THE PUBLISHER AND COPYRIGHT OWNER OF THIS PUBLICATION CAN NOT ACCEPT ANY RESPONSIBILITY OR LIABILITY FOR ANY EVENTUAL ERRORS OR OMISSIONS IN THIS BOOKLET OR FOR DISCREPANCIES ARISING FROM THE FEATURES OF ANY ACTUAL ITEM IN THE RESPECTIVE PRODUCT BEING DIFFERENT FROM THOSE SHOWN IN THIS PUBLICATION. THE PUBLISHER AND COPYRIGHT OWNER SHALL UNDER NO CIRCUMSTANCES BE HELD LIABLE FOR ANY FINANCIAL CONSEQUENTIAL DAMAGES OR OTHER LOSS, OR ANY OTHER DAMAGE OR INJURY, SUFFERED BY ANY PARTY MAKING USE OF THIS PUBLICATION OR THE INFORMATION CONTAINED HEREIN. Wärtsilä 32 Product Guide Introduction Introduction This Product Guide provides data and system proposals for the early design phase of marine engine installations. For contracted projects specific instructions for planning the installation are always delivered. Any data and information herein is subject to revision without notice. This 1/2021 issue replaces all previous issues of the Wärtsilä 32 Project Guides. Issue Published Updates 1/2021 15.03.2021 Technical data updated. -
BOSE , CUTTACK 1. Mist Lubrication System
BOSE , CUTTACK CHAPTER-06 LUBRICATION SYSTEM IN AUTOMOBILE Functions of lubricating oil: A good lubricating oil should perform the following function. · It reduces the friction between the moving parts. · It cools the piston so it also acts as a cooling medium. · It also prevents the leakage of gas between the piston and cylinder because it makes a film of lubricant between them. · It also reduces the noise between the rubbing surfaces. The various lubrication systems used for lubricating the various parts of engine are classified as 1. Mist lubrication system 2. Wet sump lubrication system, and 3. Dry sump lubrication system. 1. Mist lubrication system: Mist lubrication system is a very simple type of lubrication. In this system, the small quantity of lubricating oil (usually 2 to 3%) is mixed with the fuel (preferably gasoline). The oil and fuel mixture is introduced through the carburetor. The gasoline vaporized and oil in the form of mist enters the cylinder via the crank base. The droplets of oil strike the crank base. The droplets of oil strike the crank base, lubricate the main and connecting rod bearings and the rest of the oil lubricates the piston, piston rings and cylinder. The system is preferred in two stroke engines where crank base lubrication is not required. In a two-stroke engine, the charge is partially compressed in a crank base, so it is not possible to have the oil in the crank base. This system is simple, low cost and maintenance free because it does not require any oil pump, filter, etc. However, it has certain serious disadvantages. -
Eaton Aeroquip E-Z Drain Sump Valve
Aeroquip® E-Z Drain® Sump Valve www.herberaircraft.com Eaton’s Aeroquip E-Z Drain Sump Valve makes aircraft oil changes easy. The hand-actuated valve, when attached to the oil drain port, permits aircraft engine oil changes from the ground without removal of the engine cowling. The spring-loaded E-Z Drain Valve is safe for all piston engine applcations because it canot be accidentally opened. Actuation of FEATURES the valve requires a combination push- • Reduces oil changing time twist motion. It also contains a dual seal arrangement which combines • No need to remove engine cowl both an O-ring and a metal-to-metal to change oil seal to prevent accidental leakage of • Easy manual operation – oil through the valve. The seal used on requires no tools the internal valve is replaceable with a • Eliminates messy oil spills standard AS O-ring. The accompanying • Built-in hose line directs old oil hose is furnished in standard 12-inch to container lengths*. • Spring-loaded sleeve prevents accidental oil drainage The FAA has issued a Parts • Dual seal feature guards against Manufacturing Approval to Eaton for O-ring failure use of the E-Z Drain Sump Valve on all of the aircraft engines listed in the • Safety wire holes provided below table. INSTALLATION 1. Simply remove the plug from 2. Take hold of the knurled nut 4. To close, twist the knurled nut. the bottom of the oil sump and and with a combination push- The spring-loaded valve will install the drain valve in the twist motion, open the valve. -
Technical Data Sheet
TECHNICAL DATA SHEET TDS No.: 06-01 Date Issued: 03/28/2006 2100 Mannix | San Antonio, TX 78217 t: 210.820.2450 | f: 210.820.2451 | e: [email protected] Revision: 4 (07/30/2010) AEC is recognized for Quality Management System Compliance to ISO 9001:2000. Page: 1 of 8 Cold Induction System weight and balance could cause instability of the 1.0 Subject: Airmotive Engineering (AE) Cold aircraft. Induction System 5.0 Engine Applications: Call for information 2.0 Availability: The AE Cold Induction Systems regarding other applications are sold through Engine Components Inc. (ECi®) under the TITAN® EXP™ brand. • ECi TITAN® EXP™ IOX-340S (Stroker) Series • ECi TITAN® EXP™ IOX-360 Series 3.0 Part Numbers and Description: AE111-1 (Finned sump) and AE111-2 (Unfinned sump) 6.0 Cold Induction System Schematic: The Cold Induction System components and their 4.0 General Description: An EXPERIMENTAL assembly are shown in Figures 1, 2 and 3 cold induction system for 4 cylinder opposed which are included in Section 13.0 below. engines which are based on the Lycoming 320/360 cu. in. design. The AE Cold Induction System consists of an oil sump assembly with 7.0 Safety Information: The following special “wings” on each side to minimize depth, an attention notices are used in this Technical induction housing with a forward facing Data Sheet to notify and advise the installer mounting pad for the throttle body/servo and and user of the product that certain actions or intake pipe assemblies which together procedures may be dangerous to the user or increase engine horsepower with no weight result in damage to the product. -
Starters & Alternators
Starters & Alternators Technical Manual www.denso-am.eu n UK & IE n RU n DACH n Eastern Europe n Export n Iberia, France, Italy DENSO Europe B.V. After Market and Industrial Solutions Business Unit Sales Representation European Headquarters Albania Hungary Portugal Weesp, Netherlands Austria Ireland Romania Belarus Israel Russia (Moscow) Belgium Italy Russia (Novosibirsk) Distribution warehouses Bosnia and Herzegovina Kaliningrad Slovakia Bulgaria Kazakhstan Slovenia Gennevilliers, France Cyprus Latvia Spain Leipzig, Germany Czech Republic Lithuania Sweden Madrid, Spain Denmark Luxembourg Switzerland Milton Keynes, UK Estonia Macedonia Turkey Moscow, Russia Finland Moldova United Kingdom Polrino, Italy France Montenegro Ukraine Weesp, Netherlands Georgia Netherlands Germany Norway Greece Poland DENSO Starters & Alternators Table of Content DENSO in Europe > The Aftermarket Originals 04 Introduction > About This Publication 04 > Product Range 05 PART 1 – DENSO Starters PART 2 – DENSO Alternators Characteristics Characteristics > System outline 08 > System outline 42 > How Starters work 09 > How Alternators work 43 Types Types > Pinion Shift Type 11 > Conventional Type 45 > Reduction Type 14 > Type III 46 > Planetary Type 17 > SC Type 47 Wall Chart 21 Wall Chart 53 Stop & Start Technology 22 Replacement Guide 54 Replacement Guide 28 Troubleshooting > Diagnostic Chart 55 Troubleshooting > Inspection 56 > Diagnostic Chart 29 > Q&A 58 > Inspection 30 > Q&A 37 Edition: 1, date of publication: August 2016 All rights reserved by DENSO EUROPE B.V. This document may not be reproduced or copied, in Edition: 2, date of publication: October 2016 whole or in part, without the written permission of the publisher. DENSO EUROPE B.V. reserves Editorial dept, staff: DNEU AMIS Technical Service, K. -
Vacuum Pumps Add Easy Horsepower to Any Engine. Here's
The three core components of any vacuum pump system are the pump, drive pulleys, and breather tank. Aerospace Components' billet hardware is too pretty to hide under the hood. The company offers turnkey kits for both small- and big-block Fords. TECH Vacuum Pumps Add Easy Horsepower to Any Engine. BY STEPHEN KIM PHOTOS Here's a Closer Look and How they Work COURTESY OF THE MANUFACTURERS hen a bazillion PSI of cylinder pressure pushes down on the pistons, some of it’s going to leak past the rings and into the crankcase. That’s why old cars have breathers, and newer cars have W PCV systems. While a wee bit of blow-by is completely normal— even in a 100-percent healthy motor—if an engine’s crankcase isn’t ventilated, that wee bit of blow-by is enough to pop oil seals and gaskets in no time. No bueno, homie. So what’s a racer to do? Valve cover breathers are an easy fix for non-emissions engines, but zip-tying rags onto the breathers and using them as disposable “catch cans” is downright ghetto. Instead of venting crankcase fumes into the atmosphere, late-model motors circulate them back into the intake manifold by utilizing a PCV valve. While these closed-loop systems are great for tree-huggers, they also re-circulate tiny oil droplets into the induction tract, which reduces knock resistance and can lead to detonation. Still no bueno, homie. So what’s a racer to do? The ultimate solution is sucking the fumes out of the crankcase with a vacuum pump. -
ROBINSON MODEL R44 II ROBINSON MODEL R44 II SECTION 3 EMERGENCY PROCEDURES FAA APPROVED: 11 MAY 2020 3-I SECTION 3 EMERGENCY PR
ROBINSON SECTION 3 MODEL R44 II EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES CONTENTS Page Definitions . 3-1 Power Failure – General . 3-1 Power Failure Above 500 Feet AGL . 3-2 Power Failure Between 8 Feet and 500 Feet AGL . 3-2 Power Failure Below 8 Feet AGL . 3-3 Maximum Glide Distance Configuration . 3-3 Minimum Rate of Descent Configuration . 3-3 Air Restart Procedure . 3-3 Emergency Water Landing – Power Off . 3-4 Emergency Water Landing – Power On . 3-4 Loss of Tail Rotor Thrust in Forward Flight . 3-5 Loss of Tail Rotor Thrust in Hover . 3-5 Headset Audio Failure . 3-5 Engine Fire During Start on Ground . 3-6 Engine Fire in Flight . 3-6 Electrical Fire in Flight . 3-6 Tachometer Failure . 3-7 Hydraulic System Failure . 3-7 Governor Failure . 3-7 Warning/Caution Lights . 3-8 Audio Alerts . 3-11 FAA APPROVED: 11 MAY 2020 3-i INTENTIONALLY BLANK ROBINSON SECTION 3 MODEL R44 II EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES DEFINITIONS Land Immediately – Land on the nearest clear area where a safe normal landing can be performed. Be prepared to enter autorotation during approach, if required. Land as soon as practical – Landing site is at pilot’s discretion based on nature of problem and available landing areas. Flight beyond nearest airport is not recommended. POWER FAILURE – GENERAL A power failure may be caused by either an engine or drive system failure and will usually be indicated by the low RPM horn. An engine failure may be indicated by a change in noise level, nose left yaw, an oil pressure light, or decreasing engine RPM. -
Altronic® Ignition Systems for Industrial Engines
Ignition Systems for Industrial Engines Altronic Ignition Systems CONTENTS Altronic Ignition Systems Overview and Guide Contents and Introduction ................................................................................ 2 Engine Application Guide ................................................................................. 3 Solid-State/Mechanical Ignition Systems Theory and Overview ........................................................................................ 4 Altronic I, II, III, and V ..................................................................................... 5 Disc-Triggered Digital Ignition Systems Theory and Overview ........................................................................................ 6 CD1, CD200, DISN ......................................................................................... 7 Crankshaft-Referenced Digital Ignition Systems Theory and Overview ........................................................................................ 8 CPU-95, CPU-2000 ......................................................................................... 9 Crankshaft-Referenced, Directed Energy Digital Ignition Systems CPU-XL VariSpark .......................................................................................... 10 Ignition Coils ................................................................................................... 12 Conversion Kits for Caterpillar Engines ......................................................... 14 Flashguard® Spark Plugs & Secondary