DA70 Instruction Manual
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MANUAL REVISION TRANSMITTAL Manual 146 (61-00-46) Propeller Owner's Manual and Logbook
HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. Telephone: 937.778.4200 Fax: 937.778.4391 MANUAL REVISION TRANSMITTAL Manual 146 (61-00-46) Propeller Owner's Manual and Logbook REVISION 3 dated June 2012 Attached is a copy of Revision 3 to Hartzell Propeller Inc. Manual 146. Page Control Chart for Revision 3: Remove Insert Page No. Page No. COVER AND INSIDE COVER COVER AND INSIDE COVER REVISION HIGHLIGHTS REVISION HIGHLIGHTS pages 5 and 6 pages 5 and 6 SERVICE DOCUMENTS LIST SERVICE DOCUMENTS LIST pages 11 and 12 pages 11 and 12 LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES pages 15 and 16 pages 15 and 16 TABLE OF CONTENTS TABLE OF CONTENTS pages 17 thru 24 pages 17 thru 26 INTRODUCTION INTRODUCTION pages 1-1 thru 1-14 pages 1-1 thru 1-16 DESCRIPTION AND DESCRIPTION AND OPERATION OPERATION pages 2-1 thru 2-20 pages 2-1 thru 2-24 INSTALLATION AND INSTALLATION AND REMOVAL REMOVAL pages 3-1 thru 3-22 pages 3-1 thru 3-24 TESTING AND TESTING AND TROUBLESHOOTING TROUBLESHOOTING pages 4-1 thru 4-10 pages 4-1 thru 4-10 continued on next page Page Control Chart for Revision 3 (continued): Remove Insert Page No. Page No. INSPECTION AND INSPECTION AND CHECK CHECK pages 5-1 thru 5-24 pages 5-1 thru 5-26 MAINTENANCE MAINTENANCE PRACTICES PRACTICES pages 6-1 thru 6-36 pages 6-1 thru 6-38 DE-ICE SYSTEMS DE-ICE SYSTEMS pages 7-1 thru 7-6 pages 7-1 thru 7-6 NOTE 1: When the manual revision has been inserted in the manual, record the information required on the Record of Revisions page in this manual. -
DLE-20 Operator’S Manual
DLE-20 Operator’s Manual Specifications Displacement: 20cc [1.2cu. in.] Performance: 2.5HP / 9,000 rpm Idle Speed: 1,700 rpm Ignition Style: Electronic Ignition Recommended Propellers: 14u10, 15 u8, 16u6, 16u8, 17u6 Spark Plug Type: CM6 (Gap) 0.018in.– 0.020 in. [0.45mm –0.51mm] Diameter × Stroke: 1.26in. [32mm] u0.98in. [25 mm] Compression Ratio: 10.5 :1 Carburetor: DLE MP 148 100424 with Manual Choke Weight: Main Engine − 1.43 lb [650g] Muffler − 1.76 oz [50 g] Electronic Ignition − 4.23oz [120 g] ™ Fuel: 87− 93 Octane Gasoline with a 30:1 gas/2-stroke (2-cycle) oil mixture 1 © 2010 Hobbico®, Inc. DLEG0020 Mnl Parts List (1) DLE-20cc Gas Engine w/DLE MP 148 100424 (1) DLE Spark Plug (NGK CM6 size) with additional spring (1) Muffl er with gasket (2) 4 x 14 mm SHCS (muffl er mounting) (1) Electronic Ignition Module with additional tachometer lead (1) Silicone Pick-up Wire Cover / Ignition Wire Cover (1) Red Three Pin Connector Lead with Pig Tail (ignition switch) (1) Long Throttle Arm Extension with installation screw and nut (2) Three Pin Connector Securing Clips (1) DLE Decal (not pictured) Safety Tips and Warnings ● This engine is not a toy. Please place your safety and the safety of others paramount while operating. DLE will not be held responsible for any safety issues or accidents involving this engine. ● Operate the engine in a properly ventilated area. ● Before starting the engine, please make sure all components including the propeller and the engine mount are secure and tight. -
The Starting System Includes the Battery, Starter Motor, Solenoid, Ignition Switch and in Some Cases, a Starter Relay
UNIT II STARTING SYSTEM &CHARGING SYSTEM The starting system: The starting system includes the battery, starter motor, solenoid, ignition switch and in some cases, a starter relay. An inhibitor or a neutral safety switch is included in the starting system circuit to prevent the vehicle from being started while in gear. When the ignition key is turned to the start position, current flows and energizes the starter's solenoid coil. The energized coil becomes an electromagnet which pulls the plunger into the coil. The plunger closes a set of contacts which allow high current to reach the starter motor. The charging system: The charging system consists of an alternator (generator), drive belt, battery, voltage regulator and the associated wiring. The charging system, like the starting system is a series circuit with the battery wired in parallel. After the engine is started and running, the alternator takes over as the source of power and the battery then becomes part of the load on the charging system. The alternator, which is driven by the belt, consists of a rotating coil of laminated wire called the rotor. Surrounding the rotor are more coils of laminated wire that remain stationary (called stator) just inside the alternator case. When current is passed through the rotor via the slip rings and brushes, the rotor becomes a rotating magnet having a magnetic field. When a magnetic field passes through a conductor (the stator), alternating current (A/C) is generated. This A/C current is rectified, turned into direct current (D/C), by the diodes located within the alternator. -
Propeller Operation and Malfunctions Basic Familiarization for Flight Crews
PROPELLER OPERATION AND MALFUNCTIONS BASIC FAMILIARIZATION FOR FLIGHT CREWS INTRODUCTION The following is basic material to help pilots understand how the propellers on turbine engines work, and how they sometimes fail. Some of these failures and malfunctions cannot be duplicated well in the simulator, which can cause recognition difficulties when they happen in actual operation. This text is not meant to replace other instructional texts. However, completion of the material can provide pilots with additional understanding of turbopropeller operation and the handling of malfunctions. GENERAL PROPELLER PRINCIPLES Propeller and engine system designs vary widely. They range from wood propellers on reciprocating engines to fully reversing and feathering constant- speed propellers on turbine engines. Each of these propulsion systems has the similar basic function of producing thrust to propel the airplane, but with different control and operational requirements. Since the full range of combinations is too broad to cover fully in this summary, it will focus on a typical system for transport category airplanes - the constant speed, feathering and reversing propellers on turbine engines. Major propeller components The propeller consists of several blades held in place by a central hub. The propeller hub holds the blades in place and is connected to the engine through a propeller drive shaft and a gearbox. There is also a control system for the propeller, which will be discussed later. Modern propellers on large turboprop airplanes typically have 4 to 6 blades. Other components typically include: The spinner, which creates aerodynamic streamlining over the propeller hub. The bulkhead, which allows the spinner to be attached to the rest of the propeller. -
Ignition System
IGNITION SYSTEM The ignition system of an internal combustion engine is an important part of the overall engine system. All conventional petrol[[1]] (gasoline)[[2]] engines require an ignition system. By contrast, not all engine types need an ignition system - for example, a diesel engine relies on compression-ignition, that is, the rise in temperature that accompanies the rise in pressure within the cylinder is sufficient to ignite the fuel spontaneously. How it helps It provides for the timely burning of the fuel mixture within the engine. How controlled The ignition system is usually switched on/off through a lock switch, operated with a key or code patch. Earlier history The earliest petrol engines used a very crude ignition system. This often took the form of a copper or brass rod which protruded into the cylinder, which was heated using an external source. The fuel would ignite when it came into contact with the rod. Naturally this was very inefficient as the fuel would not be ignited in a controlled manner. This type of arrangement was quickly superseded by spark-ignition, a system which is generally used to this day, albeit with sparks generated by more sophisticated circuitry. Glow plug ignition Glow plug ignition is used on some kinds of simple engines, such as those commonly used for model aircraft. A glow plug is a coil of wire (made from e.g. nichrome[[3]]) that will glow red hot when an electric current is passed through it. This ignites the fuel on contact, once the temperature of the fuel is already raised due to compression. -
Aircraft Service Manual
Propeller Technical Manual Jabiru Aircraft Pty Ltd JPM0001-1 4A482U0D And 4A484E0D Propellers Propeller Technical Manual FOR 4A482U0D and 4A484E0D Propellers DOCUMENT No. JPM0001-1 DATED: 1st Feb 2013 This Manual has been prepared as a guide to correctly operate & maintain Jabiru 4A482U0D and 4A484E0D propellers. It is the owner's responsibility to regularly check the Jabiru web site at www.jabiru.net.au for applicable Service Bulletins and have them implemented as soon as possible. Manuals are also updated periodically with the latest revisions available from the web site. Failure to maintain the propeller, engine or aircraft with current service information may render the aircraft un-airworthy and void Jabiru’s Limited, Express Warranty. This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled. Should you have any questions or doubts about the contents of this manual, please contact Jabiru Aircraft Pty Ltd. This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled. ISSUE 1 Dated : 1st Feb 2013 Issued By: DPS Page: 1 of 32 L:\files\Manuals_For_Products\Propeller_Manuals\JPM0001-1_Prop_Manual (1).doc Propeller Technical Manual Jabiru Aircraft Pty Ltd JPM0001-1 4A482U0D And 4A484E0D Propellers 1.1 TABLE OF FIGURES ............................................................................................................................................. 3 1.2 LIST OF TABLES ................................................................................................................................................. -
Chapter 26: Firewall Forward (Part Ii)
REVISION LIST CHAPTER 26: FIREWALL FORWARD (PART II) The following list of revisions will allow you to update the Legacy construction manual chapter listed above. Under the “Action” column, “R&R” directs you to remove and replace the pages affected by the revision. “Add” directs you to insert the pages shows and “R” to remove the pages. PAGE(S) AFFECTED REVISION # & DATE ACTION DESCRIPTION 26-1 through 26-21 0/02-15-02 None Current revision is correct 26-22 1/09-18-02 R&R Text Correction 26-23 through 26-32 0/02-15-02 None Current revision is correct 26-33 1/09-18-02 R&R Corrected Fig. 26:H:1 26-34 through 26-35 0/02-15-02 None Current revision is correct 26-1 3/12-15-04 R&R Updated table of contents with page numbers and part nbrs. 26-2 through 26-3 3/12-15-04 R&R Updated part nbrs. 26-4 3/12-15-04 R&R Updated engine isolator kit information. 26-6 3/12-15-04 R&R Updated part nbrs. 26-18 3/12-15-04 R&R Updated part nbrs. 26-20 through 26-21 3/12-15-04 R&R Updated part nbrs. 26-26 3/12-15-04 R&R Updated location of bulkhead fitting. 26-3 4/09/30/06 R&R Corrected plug part nbr. 26-26 4/09/30/06 R&R Corrected plug part nbr. 26-27 through 26-33 4/09-30-06 R&R Updated hose numbers and bolded so easier to read. -
Tecumseh V-Twins
TECUMSEH V-TWIN ENGINE TABLE OF CONTENTS CHAPTER 1. GENERAL INFORMATION CHAPTER 2. AIR CLEANERS CHAPTER 3. CARBURETORS AND FUEL SYSTEMS CHAPTER 4. GOVERNORS AND LINKAGE CHAPTER 5. ELECTRICAL SYSTEMS CHAPTER 6. IGNITION CHAPTER 7. INTERNAL ENGINE AND DISASSEMBLY CHAPTER 8. ENGINE ASSEMBLY CHAPTER 9. TROUBLESHOOTING AND TESTING CHAPTER 10. ENGINE SPECIFICATIONS Copyright © 2000 by Tecumseh Products Company All rights reserved. No part of this book may be reproduced or transmitted, in any form or by any means, electronic or mechanical, including photocopying, recording or by any information storage and retrieval system, without permission in writing from Tecumseh Products Company Training Department Manager. i TABLE OF CONTENTS (by subject) GENERAL INFORMATION Page Engine Identification ................................................................................................ 1-1 Interpretation of Engine Identification ...................................................................... 1-1 Short Blocks ............................................................................................................ 1-2 Fuels ........................................................................................................................ 1-2 Engine Oil ................................................................................................................ 1-3 Basic Tune-Up Procedure ....................................................................................... 1-4 Storage ................................................................................................................... -
Diesel Engine Starting Systems Are As Follows: a Diesel Engine Needs to Rotate Between 150 and 250 Rpm
chapter 7 DIESEL ENGINE STARTING SYSTEMS LEARNING OBJECTIVES KEY TERMS After reading this chapter, the student should Armature 220 Hold in 240 be able to: Field coil 220 Starter interlock 234 1. Identify all main components of a diesel engine Brushes 220 Starter relay 225 starting system Commutator 223 Disconnect switch 237 2. Describe the similarities and differences Pull in 240 between air, hydraulic, and electric starting systems 3. Identify all main components of an electric starter motor assembly 4. Describe how electrical current flows through an electric starter motor 5. Explain the purpose of starting systems interlocks 6. Identify the main components of a pneumatic starting system 7. Identify the main components of a hydraulic starting system 8. Describe a step-by-step diagnostic procedure for a slow cranking problem 9. Describe a step-by-step diagnostic procedure for a no crank problem 10. Explain how to test for excessive voltage drop in a starter circuit 216 M07_HEAR3623_01_SE_C07.indd 216 07/01/15 8:26 PM INTRODUCTION able to get the job done. Many large diesel engines will use a 24V starting system for even greater cranking power. ● SEE FIGURE 7–2 for a typical arrangement of a heavy-duty electric SAFETY FIRST Some specific safety concerns related to starter on a diesel engine. diesel engine starting systems are as follows: A diesel engine needs to rotate between 150 and 250 rpm ■ Battery explosion risk to start. The purpose of the starting system is to provide the torque needed to achieve the necessary minimum cranking ■ Burns from high current flow through battery cables speed. -
DESCRIPTION Fokker 50
Fokker 50 - Power Plant DESCRIPTION The aircraft is equipped with two Pratt and Whitney PW 125B turboprop engines, which are enclosed, in wing-mounted nacelles. Each engine drives a Dowty Rotol six-bladed reversible- pitch constant-speed propeller. The engine is essentially a twin-spool turbojet combined with a free power-turbine assembly, which drives the reduction gearbox and propeller via a third concentric shaft. Engine layout Air intake The air intake is located below the propeller spinner. The intake has an anti-icing system. Combustion section The combustion section comprises an annular combustion chamber, fourteen fuel nozzles, and two igniters. Fuel control is through combined mechanical and electronic control systems. High pressure spool This spool comprises a centrifugal compressor and a single stage axial turbine. HP-spool rpm (NH) is governed by fuel metering. The spool drives the HP fuel pump and the lubrication oil pumps. Low pressure spool This spool comprises a centrifugal compressor and a single stage axial turbine. The LP spool is ungoverned; it is free to adapt itself to the operating conditions. LP-spool rpm is designated NL. To ease the gas flow paths and to minimize the gyroscopic moment, the LP spool rotates in a direction opposite to the HP spool and power-turbine shaft. Power turbine The two-stage axial power turbine drives the propeller via the reduction gearbox. The propeller shaft line is set above the engine shaft centerline. Propeller rpm is designated NP. The reduction gearbox also drives an integrated drive generator, a hydraulic pump, a propeller-pitch-control oil pump, a propeller overspeed governor, and the NP indicator. -
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 -
Cummins ISL-G
Cummins ISL-G Webinar Moderator Jerry Guaracino Deputy Chief Engineering Officer Southeastern Pennsylvania Transportation Authority (SEPTA) Philadelphia, PA Presenters Obed Mejia Victoria Chesney Senior Bus Equipment Maintenance Instructor Maintenance Supervisor Los Angeles Metropolitan Transportation Authority Omnitrans Los Angeles, CA San Bernardino, CA Objectives Participants on today’s webinar will learn how to: • Identify Maintenance Procedures • Examine components to meet specifications • Perform maintenance practices to OEM specifications Related APTA Standards • APTA BTS-BMT-RP-008-16: Training Syllabus to Instruct Bus Technicians on EPA Emissions Standards and Treatment Technologies For additional resources visit: http://www.apta.com/resources/standards/bus/ Pages/default.aspx Fleet Facts Metro Omnitrans • 2400+ Buses in service • 187 Fixed Route Coaches • 2300 ISL-G • 22 Cummins 8.3 C+ • 100 L Gas Plus • 43 8.1 John Deere HFN04 • 122 8.9 Cummins ISL G • Revenue Miles ≈ 90 million per year • Service area of 456 sq. miles with just over 9 million miles run per year. Operating Parameters • Maximum Horsepower 320 HP • Peak Torque 1000 LB-FT • Governed Speed 2200 RPM • Engine Displacement 540 CU IN 8.9 LITERS • spark-ignited, in-line 6-cylinder, turbocharged, CAC • Fuel Type CNG/LNG/RNG Methane number75 or greater • Aftertreatment Three-Way Catalyst (TW Engine Management System • The control system for the ISL-G engine is a closed loop control system. The electronic control module controls the throttle plate and fuel control valve to provide the correct fueling and spark timing. • The ISL-G engine through the years has been built with several potential sensor configurations and terminology variances. • Ensure that you are using the latest software version to correctly interact with control system.