Aviation Investigation Report A10h0004
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FAA Advisory Circular 20-97B
Subject: AIRCRAFT TIRE MAINTENANCE Date: 4/18/05 AC No.: 20-97B AND OPERATIONAL PRACTICES Initiated by: AFS-306 Change: 1. PURPOSE. This advisory circular (AC) provides recommended tire care and maintenance practices needed to assure the safety of support personnel and the continued airworthiness of aircraft. Specifically, this AC provides guidance on the installation, inflation, maintenance, and removal of aircraft tires. In addition, this AC provides guidance on those operational practices necessary to maintain safe aircraft operations. This AC is not mandatory and does not constitute a regulation. It is issued for guidance purposes and to outline acceptable tire maintenance and operational practices. In lieu of following this method without deviation, operators may elect to follow an alternative method that has also been found acceptable by the Federal Aviation Administration (FAA). 2. CANCELLATION. AC 20-97A, High-Speed Tire Maintenance and Operational Practices, dated May 13, 1987, is cancelled. 3. RELATED REGULATIONS AND DOCUMENTS. a. Title 14 of the Code of Federal Regulations (14 CFR): (1) Part 21, subpart O, Technical Standard Order Authorizations. (2) Part 23, Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes. (3) Part 25, Airworthiness Standards: Transport Category Airplanes. (4) Part 27, Airworthiness Standards: Normal Category Rotorcraft. (5) Part 29, Airworthiness Standards: Transport Category Rotorcraft. (6) Part 43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration. (7) Part 145, Repair Stations. b. FAA ACs. Copies of the following ACs may be obtained from the U.S. Department of Transportation, Subsequent Distribution Center, Ardmore East Business Center, 3341 Q 75th Avenue, Landover, MD 20785, and may be downloaded at the following Web site: http://www.faa.gov/avr/afs/acs/ac-idx.htm. -
Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed
International Journal of Aviation, Aeronautics, and Aerospace Volume 2 Issue 1 Article 2 3-2-2015 Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed Abdurrhman A. Alroqi University of Sussex, [email protected] Weiji Wang University of Sussex, [email protected] Follow this and additional works at: https://commons.erau.edu/ijaaa Part of the Aeronautical Vehicles Commons Scholarly Commons Citation Alroqi, A. A., & Wang, W. (2015). Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed. International Journal of Aviation, Aeronautics, and Aerospace, 2(1). https://doi.org/10.15394/ ijaaa.2015.1043 This Article is brought to you for free and open access by the Journals at Scholarly Commons. It has been accepted for inclusion in International Journal of Aviation, Aeronautics, and Aerospace by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed Cover Page Footnote The authors would like to acknowledge University of Sussex for its support with the literature and related resources. This article is available in International Journal of Aviation, Aeronautics, and Aerospace: https://commons.erau.edu/ ijaaa/vol2/iss1/2 Alroqi and Wang: Comparison of Aircraft Tire Wear with Initial Wheel Rotational Speed In this paper, the landing impact of an aircraft is described using a physical model of a single wheel in the main landing gear. The purpose of this study is to understand potential tire-life improvements that could be made by reducing abrasive skidding between aircraft tires and runway surfaces immediately after touchdown. -
Program Schedule
Program Schedule AIAA Science and Technology Forum and Exposition 2015 January 05 - 09, 2015 The Program Report was last updated December 18, 2014 at 04:16 PM EST. To view the most recent meeting schedule online, visit https://aiaa-mst15.abstractcentral.com/planner.jsp Monday, January 05, 2015 Time Session or Event Info 8:00 AM-9:00 AM, Osceola Ballroom CD, PLNRY-01. Opening Keynote , Plenary, Forum 9:00 AM-12:30 PM, St. George 112, ISC-01. International Student Conference (Undergraduate Category), Technical Paper, 53rd AIAA Aerospace Sciences Meeting, Chair: Chris Tavares, The Boeing Company Martian RHOVER Feasibility Study J. Fuentes; R. Pankaja 9:00-9:30 AM Kaluarachchi Satellite Formation Control using Differential Drag S.R. Omar; J.M. 9:30-10:00 AM Wersinger Manufacturing of Triaxial Quasi-three-dimensional Composite 10:00-10:30 AM Materials G. Peterson; D. Liu The Design, Fabrication, and Evaluation of Millimeter Wave Lenses 10:30-11:00 AM for Beamed Energy Applications S.E. Sloan Colorimetric hydrogel-based microfluidic assay system to monitor 11:00-11:30 AM malnutrition in a microgravity environment J.K. Tsosie Significance of Constituent Chemical age on Solid Rocket Propellant 11:30-12:00 PM Regression Rates D.J. Dulin; G.S. Gibson 12:00-12:30 PM Aerodynamic Testing and Development of Sunswift eVe S. Ambrose 9:30 AM-12:30 PM, Miami 2, AA-01. Computational Aeroacoustics I, Technical Paper, 53rd AIAA Aerospace Sciences Meeting, Chair: Walter Eversman, Missouri University of Science and Technology A Computational Study of Flow Within Cavities with Complex 9:30-10:00 AM Geometric Features M.F. -
Aircraft Tire Data
Aircraft tire Engineering Data Introduction Michelin manufactures a wide variety of sizes and types of tires to the exacting standards of the aircraft industry. The information included in this Data Book has been put together as an engineering and technical reference to support the users of Michelin tires. The data is, to the best of our knowledge, accurate and complete at the time of publication. To be as useful a reference tool as possible, we have chosen to include data on as many industry tire sizes as possible. Particular sizes may not be currently available from Michelin. It is advised that all critical data be verified with your Michelin representative prior to making final tire selections. The data contained herein should be used in conjunction with the various standards ; T&RA1, ETRTO2, MIL-PRF- 50413, AIR 8505 - A4 or with the airframer specifications or military design drawings. For those instances where a contradiction exists between T&RA and ETRTO, the T&RA standard has been referenced. In some cases, a tire is used for both civil and military applications. In most cases they follow the same standard. Where they do not, data for both tires are listed and identified. The aircraft application information provided in the tables is based on the most current information supplied by airframe manufacturers and/or contained in published documents. It is intended for use as general reference only. Your requirements may vary depending on the actual configuration of your aircraft. Accordingly, inquiries regarding specific models of aircraft should be directed to the applicable airframe manufacturer. -
Qtr 02 09 a Quarterly Publication Boeing.Com/Commercial/ Aeromagazine
Qtr_02 09 A QUarterlY PUBLIcatION BOEING.COM/COMMERCIAL/ AEROMAGAZINE Material Management: Providing Customer Solutions 777 Freighter: Greater Efficiency for Long-Haul Operators Landing Gear Program Provides Overhaul Alternative Exceeding Tire Speed Rating During Takeoff Contribution of Flight Systems to Performance-Based Navigation AERO Cover photo: 777 in factory AERO Contents 03 Material Management: Providing Customer Solutions Our services are designed to help airlines operate more efficiently while reducing costs. 05 777 Freighter: Greater Efficiency for Long-Haul Operators The Boeing 777 Freighter is an efficient, long-range, high-capacity freighter offering the advanced features of the 05 777 family. 11 Landing Gear Program Provides Overhaul Alternative Boeing’s overhaul and exchange program offers operators additional options for 11 servicing landing gear. 15 Exceeding Tire Speed Rating During Takeoff Boeing offers guidance to help prevent 15 tire overspeed events during takeoff. 21 Contribution of Flight Systems to Performance-Based Navigation The evolution of flight management systems has led the way for performance- based navigation and the Next Generation 21 Air Transportation System. 01 WWW.boeIng.com/commercIal/aeromagaZIne Issue 34_Quarter 02 | 2009 AERO Publisher Design Cover photography Editorial Board Shannon Frew Methodologie Jeff Corwin Gary Bartz, Frank Billand, Richard Breuhaus, Darrell Hokuf, Al John, Doug Lane, Jill Langer, Mick Pegg, Wade Price, Bob Rakestraw, Editorial director Writer Printer Frank Santoni, Jerome -
Aircraft Accident at Kajaani Airport, Finland, 3. November 1994
Aircraft accident at Kajaani Airport, Finland, 3. November 1994 Micro-summary: This McDonnell Douglas MD-83 left the runway on landing. Event Date: 1994-11-03 at 0657 local Investigative Body: Finland Accident Investigation Board (AIB), Finland Investigative Body's Web Site: http://www.onnettomuustutkinta.fi/ Cautions: 1. Accident reports can be and sometimes are revised. Be sure to consult the investigative agency for the latest version before basing anything significant on content (e.g., thesis, research, etc). 2. Readers are advised that each report is a glimpse of events at specific points in time. While broad themes permeate the causal events leading up to crashes, and we can learn from those, the specific regulatory and technological environments can and do change. Your company's flight operations manual is the final authority as to the safe operation of your aircraft! 3. Reports may or may not represent reality. Many many non-scientific factors go into an investigation, including the magnitude of the event, the experience of the investigator, the political climate, relationship with the regulatory authority, technological and recovery capabilities, etc. It is recommended that the reader review all reports analytically. Even a "bad" report can be a very useful launching point for learning. 4. Contact us before reproducing or redistributing a report from this anthology. Individual countries have very differing views on copyright! We can advise you on the steps to follow. Aircraft Accident Reports on DVD, Copyright © 2006 by Flight Simulation Systems, LLC All rights reserved. www.fss.aero Major Accident Report Nr 2/1994 Translation of the Finnish original report Aircraft accident at Kajaani Airport, Finland, 3. -
FINAL PROGRAM #Aiaascitech
4–8 JANUARY 2016 SAN DIEGO, CA The Largest Event for Aerospace Research, Development, and Technology FINAL PROGRAM www.aiaa-SciTech.org #aiaaSciTech 16-928 WHAT’S IMPOSSIBLE TODAY WON’T BE TOMORROW. AT LOCKHEED MARTIN, WE’RE ENGINEERING A BETTER TOMORROW. We are partnering with our customers to accelerate manufacturing innovation from the laboratory to production. We push the limits in additive manufacturing, advanced materials, digital manufacturing and next generation electronics. Whether it is solving a global crisis like the need for clean drinking water or travelling even deeper into space, advanced manufacturing is opening the doors to the next great human revolution. Learn more at lockheedmartin.com © 2014 LOCKHEED MARTIN CORPORATION VC377_164 Executive Steering Committee AIAA SciTech 2016 2O16 Welcome Welcome to the AIAA Science and Technology Forum and Exposition 2016 (AIAA SciTech 2016) – the world’s largest event for aerospace research, development, and technology. We are confident that you will come away from San Diego inspired and with the tools necessary to continue shaping the future of aerospace in new and exciting ways. From hearing preeminent industry thought leaders, to attending sessions where cutting- edge research will be unveiled, to interacting with peers – this will be a most fulfilling week! Our organizing committee has worked hard over the past year to ensure that our plenary sessions examine the most critical issues facing aerospace today, such as aerospace science and Richard George Lesieutre technology policy, lessons learned from a half century of aerospace innovation, resilient design, Christiansen The Pennsylvania and unmanned aerial systems. We will also focus on how AIAA and other stakeholders in State University Sierra Lobo, Inc. -
On the Modeling of Light Aircraft Landing Gears Nadia Arif, Iulian Rosu, Frédéric Lebon, Hélène Elias-Birembaux
On the modeling of light aircraft landing gears Nadia Arif, Iulian Rosu, Frédéric Lebon, Hélène Elias-Birembaux To cite this version: Nadia Arif, Iulian Rosu, Frédéric Lebon, Hélène Elias-Birembaux. On the modeling of light aircraft landing gears. Journal of Aeronautics and Aerospace Engineering, 2019, 23 (3), pp.1-9. 10.4172/2168- 9792.1000213. hal-02336636 HAL Id: hal-02336636 https://hal.archives-ouvertes.fr/hal-02336636 Submitted on 21 Nov 2019 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. cs & Aero ti sp au a n c o e Nadia et al., J Aeronaut Aerospace Eng 2018, 7:3 r E e n A g f Journal of Aeronautics & Aerospace DOI: 10.4172/2168-9792.1000213 i o n l e a e r n i r n u g o J Engineering ISSN: 2168-9792 Research Article Open Access On the Modeling of Light Aircraft Landing Gears Arif Nadia*, Rosu Iulian, Lebon Fred´eric and Elias-Birembaux Hel`ene Aix-Marseille University, CNRS, Centrale Marseille, LMA, Marseille, France *Corresponding author: Nadia A, Aix-Marseille University, CNRS, Centrale Marseille, LMA, Marseille, France, Tel: +33 491 396 500; E-mail: [email protected] Received: August 29, 2018; Accepted: October 28, 2018; Published: November 09, 2018 Copyright: © 2018 Nadia A, et al. -
Program Schedule
Program Schedule SciTech 2016 January 03 - 08, 2016 The Program Report was last updated December 11, 2015 at 01:06 AM EST. To view the most recent meeting schedule online, visit https://aiaa-mst16.abstractcentral.com/planner.jsp Sunday, January 03, 2016 Time Session or Event Info 6:00 PM-7:30 PM, Seaport H, NW-01. Student Welcome Reception, Networking, Forum Event Monday, January 04, 2016 Time Session or Event Info 7:00 AM-7:30 AM, Session Room Foyers, NW-02. Monday Early Morning Networking Coffee Break, Networking, Forum Event 7:30 AM-8:00 AM, Session Rooms, SB-01. Monday Morning Speakers' Briefing, Speakers' Briefing, Forum Event 8:00 AM-9:00 AM, Seaport A-E, PLNRY-01. Monday Morning Plenary Panel Aerospace S&T Policy in the 2016 Political Arena , Plenary, Forum Event 9:00 AM-12:30 PM, Nautical, AA-01. Aeroacoustics - Jet Noise I, Technical Paper, 54th AIAA Aerospace Sciences Meeting, Chair: Krishan Ahuja, [email protected], Georgia Institute of Technology; Co-Chair: Douglas Nark, [email protected], NASA Langley Research Center Mean Velocity and Turbulence Measurements of Supersonic Jets with 9:00-9:30 AM Fluidic Inserts R.W. Powers; S. Hromisin; D.K. McLaughlin; P.J. Morris Numerical Investigation of Supersonic Jet Noise Suppression via 9:30-10:00 AM Downstream Microjet Fluidic Injection H. Pourhashem; I. Kalkhoran Fluctuating Pressure Gradients in Heated Supersonic Jets K.T. Lowe; 10:00-10:30 AM C.C. Nelson Extracting Near-Field Structures Related to Noise Production in High 10:30-11:00 AM Speed Jets P. -
Cleveland Wheels & Brakes
CLEVELAND WHEELS & BRAKES CLEVELAND WHEELS CLEVELAND HOMEBUILDERS SPECIAL & BRAKES FOR WHEEL & BRAKE SET PACKAGES CM HOMEBUILTS Wheels with matching hydraulic disc brakes are made from mag ne sium alloy castings to give a light weight, durable unit. Wheels com plete with bearings and wheel covers. Brake assembly has lin ings installed. Sold in pairs only. WP 500 x 5, Wt. 5.75 Lbs. Each (Wheel P/N 40-78B, Brake P/N 30-9) Kit P/N 199-102 (Std. Disc)................................... $1,767.00 /Pr Kit P/N 199-102C (Chrome Disc).......................... $2,983.00 /Pr Use Lining P/N 66-106. Fits 1-1/4” dia. axles. 600 x 6, Wt. 7-3/4 Lbs. Each (Wheel P/N 40-59A, Brake P/N 30-59A) ME Kit P/N 199-104 (Std. Disc)................................... $3,559.00 /Pr Kit P/N 199-104C (Chrome Disc).......................... $3,126.00 /Pr Use Lining P/N 66-112. Fits 1-1/2” dia. axles. 600 x 6, with Master Cylinders for Defiant HA Special set consists of (2) P/N 40-75B wheels, (2) P/N 30-52 brake assemblies and (2) P/N 10-34 master cylinders. P/N 199-133X ............ $5,017.00 500 x 5 NOSE WHEEL - Magnesium, with bearings. PACKAGE NO. 1 - For 1-1/4” dia. axle. ................. P/N 40-77C ................ $1,026.00 Includes 2 Cleveland 5.00-5 magnesium wheels & brakes plus (2) 6 ply AP tires & tubes. (Wt. approx. 28 lbs.) 600 x 6 NOSE WHEEL - Anodized aluminum, with bearings. For 1-1/2” dia. -
Tor RMT.0586 Issue 1
European Aviation Safety Agency Terms of Reference for rulemaking task RMT.0586 Tyre pressure monitoring system ISSUE 1 Issue/rationale Improper tyre pressure, in particular underinflation, remains a major contributing factor to tyre- and wheel- failure-related accidents or incidents. These kinds of occurrences continue to occur regularly despite a number of regulatory changes established over the last 40 years. It is widely recognised that ensuring correct aircraft tyre inflation pressure is the most important factor for safe tyre operations. The specific objective of this rulemaking task is to propose a regulatory change to ensure that the tyres’ inflation pressures of large aeroplanes remain within the pressure specifications defined by the aircraft manufacturer. Action area: Design and maintenance improvements Affected rules: CS-25; Part-26; CS-26; Part-M; AMC & GM to Part-M Affected stakeholders: Design organisations manufacturing large aeroplanes and their suppliers; operators of large aeroplanes; maintenance organisations Driver: Safety Rulemaking group: Yes Impact assessment: Full Rulemaking Procedure: Standard 30.5.2017 2018/Q3 2019/Q3 2020/Q3 2020/Q3 (Part-26, Part-M) (Part-26, Part-M) (CS-26, AMC & GM to Part-M) (CS-25) TE.RPRO.00037-007 © European Aviation Safety Agency. All rights reserved. ISO 9001 certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA intranet/internet. Page 1 of 9 An agency of the European Union European Aviation Safety Agency RMT.0586 ToR Issue 1 1. Why we need to change the rules — issue/rationale 1.1. General Improper tyre pressure, in particular underinflation, remains a major contributing factor to tyre- and wheel-failure-related accidents or incidents. -
Ep 1 892 129 A2
(19) & (11) EP 1 892 129 A2 (12) EUROPEAN PATENT APPLICATION (43) Date of publication: (51) Int Cl.: 27.02.2008 Bulletin 2008/09 B60C 23/04 (2006.01) (21) Application number: 07114932.2 (22) Date of filing: 24.08.2007 (84) Designated Contracting States: (72) Inventor: Logan, Brian Matthew AT BE BG CH CY CZ DE DK EE ES FI FR GB GR Akron, OH 44302 (US) HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR (74) Representative: Kutsch, Bernd Designated Extension States: Goodyear S.A., AL BA HR MK YU Patent Department, Avenue Gordon Smith (30) Priority: 25.08.2006 US 467405 7750 Colmar-Berg (LU) (71) Applicant: THE GOODYEAR TIRE & RUBBER COMPANY Akron, OH 44316-0001 (US) (54) Aircraft tire condition monitoring system and method (57) An aircraft tire condition monitoring system in- the aircraft. The antenna (16) is electrically coupled to cludes a reader (20) mounted in the fuselage (32) of an the reader (20) to facilitate the communication of signals aircraft and an antenna (16) that defines a peripheral from a transponder (14) located within the tire (12). The boundary proximate the circumference of a tire (12) of antenna (16) may be located within the tire (12), or it may be located on the aircraft fuselage (32). EP 1 892 129 A2 Printed by Jouve, 75001 PARIS (FR) 1 EP 1 892 129 A2 2 Description comings and drawbacks of tire condition monitoring sys- tems heretofore known for use in vehicles. Dependent Technical Field claims refer to preferred embodiments of the invention.