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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. -
Service Instruction No
652 Oliver Street SERVICE Williamsport, PA. 17701 U.S.A. Telephone +1 (877) 839-7878 (U.S. and Canada) Telephone +1 (570) 327-7222 (International) Fax +1 (570) 327-7101 Email [email protected] INSTRUCTION www.lycoming.com DATE: April 24, 2020 Service Instruction No. 1009BE (Supersedes Service Instruction No. 1009BD) Engineering Aspects are FAA Approved SUBJECT: Time Between Overhaul (TBO) Schedules MODELS AFFECTED: Lycoming Engine Models Defined Herein REASON FOR REVISION: Added a new paragraph at the end of the Operating Hour Time Period TBO section. Added new engine model IO-390-D to Table 1. Revised Table 2 to include separate listings for engine model O-540-F1B5 for the Robinson R44 and R44 Cadet. Revised Note 10 to include reference to Note 6. Revised the paragraph after the CAUTION in the CALENDAR TIME PERIOD TBO section. Revised Note 15,c. NOTICE: Incomplete review of all the information in this document can cause errors. Read the entire Service Instruction to make sure you have a complete understanding of the requirements. This Service Instruction identifies the Calendar Time Period in years and the Operating Hour Time Period in hours of engine operation for the Time Between Overhaul (TBO) for certified Lycoming engine models operated and maintained in compliance with all applicable Lycoming Technical Publications and FAA Airworthiness Directives. The TBOs stated in this Service Instruction do not apply to engines that: a. Do not conform to the original engine model type certificate configuration; b. Have been assembled, repaired, or overhauled with FAA-PMA parts, where the FAA-PMA parts have not been approved for use by Lycoming (contact Lycoming for information regarding FAA-PMA parts approved for use by Lycoming); c. -
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. -
Service Bulletin P&Wc S.B
Caravan SERVICE LETTER CAL-72-01 TITLE ENGINE - TRANSMITTAL OF P&WC S.B. NO. 1903R2 EFFECTIVITY MODEL SERIAL NUMBERS 208B 208B5000 and On REASON The purpose of this service letter is to transmit P&WC S.B. No. 1903R2, Turboprop Engine Operating Time Between Overhauls and Hot Section Inspection Frequency. DESCRIPTION Pratt & Whitney Canada (P&WC) has issued P&WC S.B. No. 1903R2 to provide information on recommended basic operating Time Between Overhaul (TBO) and to specify a recommended initial Hot Section Inspection (HSI) frequency. The TBO and HSI intervals are the two major scheduled inspections, and are defined in S.B. No. 1903R2. Caravan EX operators should notice that P&WC S.B. No. 1903R2 specifies a life limit for the motive flow shut-off valve, P/N 3076615-04, of 100 hours. P&WC has stated that they will cover the warranty costs to replace the motive flow shut-off valve P/N 3076615-04 until such time as a newly designed valve with a new part number is specified for use by P&WC. Warranty claims for parts and labor should be filed through Cessna Service Parts and Programs in accordance with standard procedures. COMPLIANCE INFORMATIONAL. This service letter is for informational purposes only. MATERIAL AVAILABILITY P&WC S.B. No. 1903R2, Turboprop Engine Operating Time Between Overhauls and Hot Section Inspection Frequency REFERENCES P&WC S.B. No. 1903R2, Turboprop Engine Operating Time Between Overhauls and Hot Section Inspection Frequency CAL-72-01 March 14, 2013 Page1of1 Cessna Aircraft Company, Cessna Customer Service, P.O. -
Epic Performance for Tнe Entire King Air 200 Family
BEECHCRAFT KING AIR B200GT EPIC PERFORMANCE FOR THE B200 ENTIRE KING AIR 200 FAMILY... 200 ...utilizing Swept Blade Technology Simply more of what you bought your King Air for! THE ELEMENTS OF RAISBECK’S 200-SERIES EPIC PERFORMANCE PACKAGE (Elements available separately) SWEPT BLADE TURBOFAN PROPELLERS RAM AIR RECOVERY SYSTEM ENHANCED PERFORMANCE LEADING EDGES DUAL AFT BODY STRAKES HIGH FLOTATION GEAR DOORS OPTIONAL CROWN WING LOCKERS Diaphragm Seal Particle Separator with flap Ice Shedder Turning Vane Flap Bypass Door Seal Benefits Benefits Benefits Benefits Benefits Benefits • Stunning ramp presence • Significantly increases climb and cruise • Cruise speeds and range are increased • Passenger ride quality is improved • Climb and cruise performance of standard- • FAA-certified to carry 600 pounds total cargo in • Quiet and virtually vibrationless operation performance in both normal and anti-ice • Stall speeds and characteristics are improved • Pilot control and handling qualities are gear King Airs is restored 17 cubic feet of luggage space from takeoff to touchdown operating modes • Air conditioning and cooling are more efficient enhanced • Cruise speed is increased 8 to 12 knots • Returns your cabin to your passengers • Certified around the world to meet the most • Protects against FOD—deployable for all • Outboard wing fatigue life is inherently • Air Minimum Control Speed is inherently depending on altitude • Handles skis, snowboards, camping and stringent regulations and noise requirements ground, takeoff and landing operations -
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 ................................................................................................................................................. -
Aeroshell Book
THE AEROSHELL BOOK Twentieth Edition 2021 Issued by: Shell Aviation Shell International Petroleum Co. Ltd. Shell Centre York Road London SE1 7NA www.shell.com/aviation 3 COPYRIGHT STATEMENT All rights reserved. Neither the whole nor any part of this document may be reproduced, stored in any retrieval system or transmitted in any form or by any means (electronic, mechanical, reprographic, recording or otherwise) without the prior written consent of the copyright owner. The companies in which Royal Dutch Shell plc directly and indirectly owns investments are separate entities. In this document the expressions “Shell”, “Group” and “Shell Group” are sometimes used for convenience where references are made to Group companies in general. Likewise, the words “we”, “us” and “our” are also used to refer to Group companies in general or those who work for them. These expressions are also used where there is no purpose in identifying specific companies. © 2021 Shell International Petroleum Company Limited. 4 DEFINITIONS & CAUTIONARY NOTE The companies in which Royal Dutch Shell plc directly and indirectly owns investments are separate legal entities. In this The AeroShell Book, “Shell”, “Shell Group” and “Royal Dutch Shell” are sometimes used for convenience where references are made to Royal Dutch Shell plc and its subsidiaries in general. Likewise, the words “we”, “us” and “our” are also used to refer to Royal Dutch Shell plc and its subsidiaries in general or to those who work for them. These terms are also used where no useful purpose is served by identifying the particular entity or entities. ‘‘Subsidiaries’’, “Shell subsidiaries” and “Shell companies” as used in this The AeroShell Book refer to entities over which Royal Dutch Shell plc either directly or indirectly has control. -
Aa2016-1 Aircraft Accident Investigation Report
AA2016-1 AIRCRAFT ACCIDENT INVESTIGATION REPORT KOREA PILOT SCHOOL N 1 7 6 C D February 25, 2016 The objective of the investigation conducted by the Japan Transport Safety Board in accordance with the Act for Establishment of the Japan Transport Safety Board and with Annex 13 to the Convention on International Civil Aviation is to determine the causes of an accident and damage incidental to such an accident, thereby preventing future accidents and reducing damage. It is not the purpose of the investigation to apportion blame or liability. Norihiro Goto Chairman, Japan Transport Safety Board Note: This report is a translation of the Japanese original investigation report. The text in Japanese shall prevail in the interpretation of the report. AIRCRAFT ACCIDENT INVESTIGATION REPORT AIRCRAFT DAMAGE CAUSED BY FORCED LANDING KOREA PILOT SCHOOL OPERATED BY PRIVATELY CONTRACTED PILOT CIRRUS SR20, N176 CD (THE UNITED STATES) NISHIKATA, IBUSUKI CITY, KAGOSHIMA PREFECTURE, JAPAN At ABOUT 14:30 JST, OCTOBER 12, 2014 February 12, 2016 Adopted by the Japan Transport Safety Board Chairman Norihiro Goto Member Shinsuke Endoh Member Toshiyuki Ishikawa Member Sadao Tamura Member Yuki Shuto Member Keiji Tanaka SYNOPSIS <Summary of the Accident> On Sunday October 12, 2014, around 14:30 Japan Standard Time (JST: UTC + 9 hrs. all times are indicated in JST on a 24-hour clock), the Cirrus SR20, registered N176CD, owned by the KOREA PILOT SCHOOL, was damaged during forced landing in a grass field at Nishikata, Ibusuki city, Kagoshima prefecture, because the engine halted while it was ferried from Saipan International Airport to Gimpo International Airport in the Republic of Korea. -
Heavy-Fueled Intermittent Ignition Engines: Technical Issues
Publications 9-2009 Heavy-Fueled Intermittent Ignition Engines: Technical Issues Jeffrey Arthur Schneider Embry-Riddle Aeronautical University Timothy Wilson Embry-Riddle Aeronautical University, [email protected] Christopher Griffis Peter Pierpont Follow this and additional works at: https://commons.erau.edu/publication Part of the Aeronautical Vehicles Commons, and the Propulsion and Power Commons Scholarly Commons Citation Schneider, J. A., Wilson, T., Griffis, C., & Pierpont,. P (2009). Heavy-Fueled Intermittent Ignition Engines: Technical Issues. , (). Retrieved from https://commons.erau.edu/publication/145 This Report is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Publications by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. DOT/FAA/AR-08/42 Heavy-Fueled Intermittent Air Traffic Organization NextGen & Operations Planning Ignition Engines: Office of Research and Technology Development Technical Issues Washington, DC 20591 September 2009 Final Report This document is available to the U.S. public through the National Technical Information Services (NTIS), Springfield, Virginia 22161. U.S. Department of Transportation Federal Aviation Administration NOTICE This document is disseminated under the sponsorship of the U.S. Department of Transportation in the interest of information exchange. The United States Government assumes no liability for the contents or use thereof. The United States Government does not endorse products or manufacturers. Trade or manufacturer's names appear herein solely because they are considered essential to the objective of this report. This document does not constitute FAA certification policy. Consult your local FAA aircraft certification office as to its use. This report is available at the Federal Aviation Administration William J. -
P180E User Guide IMPORTANT INFORMATION
P180E User Guide IMPORTANT INFORMATION This manual is for flight simulation use only. Do not attempt to use any part for real flight operations. This software is an artistic representation of the subject matter. Military Visualizations Inc. does not endorse, nor in turn, is endorsed by the manufacturer(s) of the depicted subject matter. End User License Agreement By purchasing the Milviz P180E, you are consenting to be bound by and agree to the following: COPYRIGHT: Copyright © 2021 Military Visualizations (Milviz). Milviz retains FULL copyright on the entire P180E package. DISTRIBUTION: You may NOT redistribute the P180E package in whole or in part. Any such distribution is strictly prohibited. GRANT OF LICENSE: A limited license is granted to use the Milviz P180E for personal entertainment purposes only. Commercial, training or any other use without the express permission of Military Visualizations Inc. is expressly prohibited. Any such usage will be litigated to the full extent of the law. This does NOT give you the license to modify in anyway part or whole based on the designers original work except for your own personal use. You MAY of course use the paint kit provided to create new liveries for public distribution, provided no charge is made for them! Any inquiries regarding use of this product in a commercial or training capacity should be directed via e-mail to [email protected]. DISCLAIMER: Milviz and all associates shall NOT be held responsible for any damages arising from the use of the P180E product. Copyright © 2021 Military -
Rotax Service Interval Guide Not New News, but a Very Informative Summary
Rotax Service Interval Guide Not new news, but a very informative summary With growing numbers of 912 & 914 series engines in service these days Rotax have gathered a great deal of field experience and have been continually updating the maintenance procedures. Operators of 912 & 914 series engines can obtain current maintenance manuals free of charge, (yep I did say FREE) from the Rotax aircraft engines web site www.rotax-aircraft-engines.com – just click on the documentation tab & fill in the relevant search boxes to obtain the documents you require. You will find parts lists, line & heavy maintenance manuals, service bulletins, operator’s manuals, installation manuals, and a whole host of information you may not have known about. The system is not perfect, for example parts lists for early engines are not available, but it is pretty good & full of useful documentation. We do find that some Rotax owners find the documentation difficult to interpret and occasionally miss things - agreed it can be difficult to see the wood through the trees, especially after translation. As the maintenance & overhaul information has changed over the last couple of years it’s probably a good time to have a recap on how things are now. So before the flying season gets too busy why not take the opportunity to make sure your engine is ready for the new flying season – I’m assured its going to be a good one this year! Figure 1: Documentation page of the Rotax Aircraft Engines website (www.rotax-aircraft-engines.com) MAINTENANCE SCHEDULES The alterations to the maintenance schedules over the years have mainly been to reduce the work required and the parts replaced, so should you want to save a few pennies in these difficult times you better read on.