Rotax Service Interval Guide Not New News, but a Very Informative Summary
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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. -
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. -
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. -
FLASHBLACK Instruction Manual
Instruction manual Variable pitch propellers in flight FLASHBLACK FLASHBLACK Tractor Pusher BLACK Tractor Aérodrome de Villefranche Tarare (LFHV) 289 Avenue Odette & Edouard DURAND 69620 FRONTENAS - FRANCE Phone: + 33 (0)4 74 72 12 69 - Fax: +33 (0)4 74 72 10 01 ISO 9001:2015 Certified Company E-mail: [email protected] - www.DUC-helices.com for its Quality System Management DH_FSH-PV_BE_02_F Made in France 04/12/2018 Revision update Date Index Object of modification 23/07/2014 A Creation 20/07/2017 F Add SWIRLBLACK-3 & TBO update 11/12/2017 F Minor correction 10/04/2018 F English language correction 04/12/2018 F Minor change in page 42 This instruction manual is to be maintained throughout the life of the propeller. He may have to evolve. The owner must check with the DUC Hélices Company the latest version being valid applicable to the propeller. Identification Date Delivery note n° Engine/Gearbox Owner ratio Aircraft Pitch range Min: Max: Notes: .............................................................................................................................................................................. .......................................................................................................................................................................................... .......................................................................................................................................................................................... ......................................................................................................................................................................................... -
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. -
Looking After Your Rotax 912 Series Engine
LOOKING AFTER YOUR ROTAX 912 SERIES ENGINE Most of the things you wanted to know about servicing a Rotax 912/914 series aircraft engine but were afraid to ask…. By Conrad Beale Copyright ConAir Sports Ltd. All rights reserved. Page 1 of 20 Most of the things you wanted to know about servicing a Rotax 912/914 series aircraft engine but were afraid to ask…. By Conrad Beale This article has been written by Conrad Beale of ConAir Sports Ltd. It is intended to help you look after your 912 series engine. It is in no way endorsed by Rotax. All information contained here in may be subject to change without notice. It does not substitute, override or in any way replace the information given in the Installation / Maintenance or Operators Manuals or any subsequent documentation issued by Rotax. The intention of this article is to assist the many Rotax 4 stroke engine owners, operators and engineers to carry out the work necessary to prolong the life of their Rotax 912/914 series aircraft engines. This article will touch on a number of subjects and will hopefully clear up some of the common questions we get asked. Some areas will be covered in detail, others less so. I hope it covers everything sufficiently. I have been involved with Rotax engines for 25+ years, 18 of which have been working commercially on Rotax aircraft engines. 8 years ago I set up ConAir Sports Ltd with my wife Louise and we are the only UK Skydrive appointed Service Centre for Rotax Aircraft Engines. -
Carburetor Synchronization
Carburetor Synchronization With the proliferation of the Rotax 912 80 hp and the Rotax 912S 100 hp engines, the topic of carburetor synchronization has come to the forefront. Until about the 1980s, the popularity of Continental and Lycoming engines dominated the general aviation market, these engines used a single carburetor providing for a single source of air and fuel to the cylinders. The use of dual carburetors was primarily relegated to the area of the two-stroke ultralight market. And, even with these engines, the process of carburetor synchronization was quite simple and reliable. How- ever, with the popularity of the Rotax 9 series engines, it has become import- ant to under- stand a little bit more about how the induc- tion system works on this amazing little powerhouse. This understand- ing is important not only from a maintenance standpoint, but from a pilot’s per- spective as well. The Rotax 912 is essentially two engines connected to a single crankshaft and gearbox with both Figure: 1 The Rotax 912 is two separate engines connected to a common crankshaft the left and right sides of the engine having their own independent carburetor, ignition, and exhaust sys- tem Figure: 1. As you might well imagine, having two engines trying to run a single propeller requires a bit of choreography between the right and left side of the en- gine in order to make things run smoothly. Most of us, who have spent a consider- able amount of time in the air, can remember a time when one of the cylinders on a four-cylinder engine just quit firing, maybe from fouled spark plugs, or a plugged fuel Figure: 2 Clamping off the crossover (Balance) hose injector. -
European Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : E.121 Issue : 06 Date : 17.06.2014 Type : Rotax 912 series engines Models Rotax 912 A1 Rotax 912 A2 Rotax 912 A3 Rotax 912 A4 Rotax 912 F2 Rotax 912 F3 Rotax 912 F4 Rotax 912 S2 Rotax 912 S3 Rotax 912 S4 Rotax 912 iSc2 Sport Rotax 912 iSc3 Sport List of effective Pages: Page 1 2 3 4 5 6 7 8 9 10 11 12 13 Issue 6 6 6 6 6 6 6 6 6 6 6 6 6 TCDS EASA.E.121 Rotax 912 series engines page 2/13 Issue 06, 17 June 2014, models: 912 A1, A2, A3, A4, F2, F3, F4, S2, S3, S4, iSc2 Sport, iSc3 Sport Intentionally left blank TCDS EASA.E.121 Rotax 912 series engines page 3/13 Issue 06, 17 June 2014, models: 912 A1, A2, A3, A4, F2, F3, F4, S2, S3, S4, iSc2 Sport, iSc3 Sport I - General 1. Type / Models: Rotax 912/ Rotax 912 A1, Rotax 912 A2, Rotax 912 A3, Rotax 912 A4, Rotax 912 F2, Rotax 912 F3, Rotax 912 F4, Rotax 912 S2, Rotax 912 S3, Rotax 912 S4, Rotax 912 iSc2 Sport, Rotax 912 iSc3 Sport 2. Type Certificate Holder: Since March 15, 2014 BRP-Powertrain GmbH & Co KG Rotaxstraße 1 A-4623 Gunskirchen, Austria DOA EASA.21J.048 Before March 15, 2014 BRP-Powertrain GmbH & Co KG Welser Straße 32 A-4623 Gunskirchen, Austria DOA EASA.21J.048 Before February 3, 2009 BRP-Rotax GmbH & Co KG Welser Straße 32 A-4623 Gunskirchen, Austria DOA EASA.21J.048 Before June 16, 2004 Bombardier-Rotax GmbH & Co KG Welser Straße 32 A-4623 Gunskirchen, Austria Before December 29, 2001 Bombardier-Rotax Gesellschaft mbH Welser Straße 32 A-4623 Gunskirchen, Austria 3. -
Pratt & Whitney's R-4360
The Piston Engine Revolution Pratt & Whitney’s R-4360 Graham White Pratt & Whitney’s 28-cylinder, four-row radial, the R-4360, was the largest and most complex aircraft piston engine to enter production in the West. After cancellation of P & W’s liquid cooled sleeve valve efforts, the R-4360 was rushed into development with an initial rating of over 3000 hp. Although too late for WWII, it played a significant part in postwar military aviation and to a lesser degree, in commercial aviation. Topics covered are: cooling, vibration, bearings, superchargers (including turbocharging and variable discharge turbines), etc. Questions such as how to mount such a behemoth, cowl designs, nacelle design, cooling flow, oil cooling, propellers (including dual rotation) etc., will be addressed. Finally, how many R-4360s are still in service? KEYWORDS: Large aero-engines. Introduction If big is good, then bigger is better, right? Wrong!! The Pratt & Whitney R-4360 was the only aircraft piston engine displacing over 4,000 cubic inches that entered into series production. However, the landscape is littered with attempts at producing a large displacement, high horsepower aircraft engine. This includes air- cooled radials, liquid-cooled in-lines and even liquid-cooled radials. History has indicated that doubling the displacement of an engine causes the development problems to go up exponentially. These problems are associated with cooling, mechanical design, lubrication and weight control. Of course, engines were developed that could produce in excess of 4,000 horsepower, but for how long would they stay together? There is little point in developing a hot-rod that lasts 200 hours between overhauls. -
Manual 154 Revision 4 October 2013
Manual 154 Revision 4 October 2013 Propeller Owner's Manual & Log Book Series HC-A6( )-3( )( ) Six-Blade Lightweight Turbine Propeller Hartzell Propeller Inc. One Propeller Place Piqua, OH 45356 - 2634 U.S.A. Ph: 937-778-4200 (Hartzell Propeller Inc.) Ph: 937-778-4379 (Product Support) Product Support Fax: 937-778-4391 Propeller Owner's Manual 154 © 1987, 1992, 1994, 2013 - Hartzell Propeller Inc. - All rights reserved Inside Cover COVER Rev. 4 Oct/13 Propeller Owner's Manual 154 REVISION HIGHLIGHTS Revision 4, dated October 2013, incorporates the following: • Revised Cover for Revision 4 • Revised Revision Highlights section • Revised Record of Revisions section • Added Airworthiness Limitations Section • Revised List of Effective Pages section Page 1 REVISION HIGHLIGHTS Rev. 4 Oct/13 Propeller Owner's Manual 154 (This page is intentionally blank.) Page 2 REVISION HIGHLIGHTS Rev. 4 Oct/13 Propeller Owner's Manual 154 RECORD OF REVISIONS Rev. No. Issue Date Date Inserted Inserted By Rev 1 5/87 5/87 HPI Rev. 2 5/92 5/92 HPI Rev. 3 1/94 1/94 HPI Rev. 4 10/13 10/13 HPI Page 1 RECORD OF REVISIONS Rev. 4 Oct/13 Propeller Owner's Manual 154 RECORD OF REVISIONS Rev. No. Issue Date Date Inserted Inserted By Page 2 RECORD OF REVISIONS Rev. 4 Oct/13 Propeller Owner's Manual 154 AIRWORTHINESS LIMITATIONS The Airworthiness Limitations section is FAA approved and specifies maintenance required under 14 CFR §§ 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA approved. FAA APPROVED by: ______________________________ date: ____________ Manager, Chicago Aircraft Certification Office, ACE-115C Federal Aviation Administration Rev. -
Methodology to Evaluate Aircraft Piston Engine Durability
METHODOLOGY TO EVALUATE AIRCRAFT PISTON ENGINE DURABILITY Luca Piancastelli, Leonardo Frizziero, Simone Marcoppido DIEM, University of Bologna viale Risorgimento, 2 - 40136 Bologna, Italy e-mail: [email protected] Eugenio Pezzuti University of Rome Tor Vergata Faculty of Engineering via del Politecnico, 1 – 00133 Rome, Italy e-mail: [email protected] ABSTRACT A main problem in aircraft engines is the evaluation of residual life to TBO. The algorithm described in this paper calculates with good reliability the residual life to TBO of a petrol piston engine. The method was tested on small last-generation naturally-aspirated-avio piston engine, and has demonstrated to be effective in several experimental tests. This method is implemented directly in the FADEC or ECU of the engine with very few lines of C-Code. The method can be used also in many industrial engines. This innovative method assumes that only two main factors (load and wear) affect engine durability or Time Between Overhauls (TBO). These two factors are considered as separate and combined with the worst case criteria. The load is assumed to follow a logarithmic law and a formula similar to the Miner‟s law for material fatigue is used, making possible to calculate the “load curve” with the knowledge of only two points. The “wear” curve is related to elapsed engine cycles, and is easy to implement since it is related to technological. The resulting algorithm is very simple and can be implemented in very few software lines with data collected from the already existing sensors. 1. 1. INTRODUCTION speed. In some modern automotive engine some sensors 2. -
Revised Listing of Amateur Built Aircraft Kits
REVISED LISTING OF AMATEUR-BUILT AIRCRAFT KITS Updated on: June 22, 2021 The following is a revised listing of aircraft kits that have been evaluated and found eligible in meeting the “major portion” requirement of Title 14, Code of Federal Regulations (14 CFR) Part 21, Certification Procedures for Products and Parts, specifically, § 21.191(g). • This listing is only representative of those kits where the kit manufacturer or distributor requested an evaluation by the Federal Aviation Administration (FAA) for eligibility and should not be construed as meaning the kit(s) are FAA “certified,” “certificated,” or “approved.” • There are other aircraft kits that may allow a builder to meet the “major portion” requirement of § 21.191(g), but those manufacturers or distributors have not requested an FAA evaluation. • The placement of an aircraft kit on this list is not a prerequisite for airworthiness certification. • The primary purpose of this listing is to assist FAA Inspectors/Designees and other interested individuals by eliminating the duplication of evaluations for “major portion” determination when the aircraft is presented for airworthiness certification as an “Amateur-Built Experimental.” • Kit manufacturers or distributors whose status is unknown are identified with a question (?) mark and their address has been deleted. Additional Information and Guidance • Advisory Circular (AC) 20-27G, Certification and Operation of Amateur-Built Aircraft. • FAA Order 8130.35B, Amateur-Built Aircraft National Kit Evaluation Team • Contact your local FAA Flight Standards District Office (FSDO) or Manufacturing Inspection District Office (MIDO). Those publications and other information pertaining to amateur-built experimental aircraft are available online at http://www.faa.gov/aircraft.